WO2023174161A1 - 一种消息传输的方法及相应终端 - Google Patents

一种消息传输的方法及相应终端 Download PDF

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Publication number
WO2023174161A1
WO2023174161A1 PCT/CN2023/080660 CN2023080660W WO2023174161A1 WO 2023174161 A1 WO2023174161 A1 WO 2023174161A1 CN 2023080660 W CN2023080660 W CN 2023080660W WO 2023174161 A1 WO2023174161 A1 WO 2023174161A1
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WO
WIPO (PCT)
Prior art keywords
satellite
terminal
message
guidance interface
interface
Prior art date
Application number
PCT/CN2023/080660
Other languages
English (en)
French (fr)
Inventor
林子杰
张若兰
钱锋
周道洋
Original Assignee
华为技术有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 华为技术有限公司 filed Critical 华为技术有限公司
Priority to EP23736591.1A priority Critical patent/EP4274270A4/en
Priority to US18/552,285 priority patent/US20240048651A1/en
Priority to CN202380020549.4A priority patent/CN118872298A/zh
Publication of WO2023174161A1 publication Critical patent/WO2023174161A1/zh

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851—Systems using a satellite or space-based relay
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/1853—Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/72—Mobile telephones; Cordless telephones, i.e. devices for establishing wireless links to base stations without route selection
    • H04M1/724—User interfaces specially adapted for cordless or mobile telephones
    • H04M1/72403—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality
    • H04M1/7243—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality with interactive means for internal management of messages
    • H04M1/72436—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality with interactive means for internal management of messages for text messaging, e.g. short messaging services [SMS] or e-mails
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
    • H04W4/12—Messaging; Mailboxes; Announcements
    • H04W4/14—Short messaging services, e.g. short message services [SMS] or unstructured supplementary service data [USSD]
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W64/00—Locating users or terminals or network equipment for network management purposes, e.g. mobility management
    • H04W64/003—Locating users or terminals or network equipment for network management purposes, e.g. mobility management locating network equipment
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/72—Mobile telephones; Cordless telephones, i.e. devices for establishing wireless links to base stations without route selection
    • H04M1/724—User interfaces specially adapted for cordless or mobile telephones
    • H04M1/72448—User interfaces specially adapted for cordless or mobile telephones with means for adapting the functionality of the device according to specific conditions
    • H04M1/72457—User interfaces specially adapted for cordless or mobile telephones with means for adapting the functionality of the device according to specific conditions according to geographic location
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W84/00—Network topologies
    • H04W84/02—Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
    • H04W84/04—Large scale networks; Deep hierarchical networks
    • H04W84/06—Airborne or Satellite Networks

Definitions

  • the present application relates to the field of communication technology, and specifically to a message transmission method and a corresponding terminal.
  • Short message is a basic service for terminal (such as mobile phone) communication.
  • a sending terminal can send a short message through an access network device (such as the first base station), and the short message is forwarded to the receiving terminal through the network.
  • the access network device (such as a second base station) then sends the short message to the receiving terminal through the second base station.
  • This application provides a message transmission method for guiding the user to adjust the positional relationship between the terminal and the target satellite through the satellite search guidance interface, thereby enabling the terminal to quickly send or receive satellite messages.
  • This application also provides corresponding terminals, computer-readable storage media, computer program products, etc.
  • the first aspect of the present application provides a message transmission method, applied to a terminal, including: displaying a satellite search guidance interface, the satellite search guidance interface includes a satellite identifier, and the display position of the satellite identifier on the satellite search guidance interface is used to indicate the terminal and The position relationship of the target satellite; in response to the user's movement operation of the terminal, the display position of the satellite identification is updated; if the position relationship between the moved terminal and the target satellite satisfies the message transmission conditions, the first satellite message is sent to the target satellite or from the target satellite. The satellite receives the first satellite message.
  • the star finding guidance interface is used to guide the user to adjust the position of the terminal.
  • the user can determine the positional relationship between the terminal and the target satellite through the display position of the satellite logo in the satellite search guidance interface, and then move the terminal (such as moving the terminal left or right, moving the terminal up or down), and the terminal will respond to the Move and adjust the display position of the satellite logo on the satellite search guidance interface.
  • the positional relationship between the moved terminal and the target satellite satisfies the message transmission condition, the positional relationship between the moved terminal and the target satellite can enable the terminal to establish a communication connection with the target satellite.
  • satellite messages refer to messages directly sent by the terminal to the satellite, or messages directly sent by the satellite to the terminal, without being forwarded by the base station.
  • the terminal can guide the user to adjust the positional relationship between the terminal and the target satellite through the satellite guidance interface, so that the terminal can quickly establish a communication connection with the satellite, so that the terminal can quickly send or receive satellite messages.
  • the star-finding guidance interface further includes star-finding prompt information, and the star-finding prompt information is used to prompt the user in the direction of the mobile terminal.
  • the star finding prompt information is used to prompt the user for the direction of the mobile terminal.
  • the star search prompt information is to move the terminal to the left, move the terminal to the right, move the terminal up or move the terminal down.
  • the star finding prompt information is usually It is a prompt given by the terminal according to the shortest moving path. In this way, the user moves the terminal according to the star finding prompt information, and can quickly move the terminal to a position suitable for establishing a communication connection with the target satellite, thereby speeding up the terminal to send satellite messages to the target satellite or The speed at which satellite messages are received.
  • the star finding guidance interface includes a first star finding guidance interface and a second star finding guidance interface.
  • the first satellite search guidance interface includes a first satellite identification and a first alignment area.
  • the first satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the azimuth angle. When the positional relationship between the terminal and the target satellite in the azimuth angle satisfies During the message transmission condition, the first satellite identifier is located in the first alignment area.
  • the second satellite search guidance interface includes a second satellite identification and a second alignment area. The second satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle. When the positional relationship between the terminal and the target satellite in the pitch angle satisfies During the message transmission condition, the second satellite identification is located in the second alignment area.
  • the satellite identification and alignment area are set from two dimensions: the azimuth angle and the pitch angle between the terminal and the target satellite.
  • the first satellite search guidance interface and the alignment area can be adjusted respectively.
  • the satellite identification and alignment area on the second satellite search guidance interface adjust the positional relationship between the terminal and the target satellite in azimuth and elevation angles, thereby speeding up the speed of establishing a communication connection between the terminal and the target satellite.
  • the above steps display the satellite search guidance interface; and, in response to the user's mobile operation of the terminal, update the display position of the satellite identification, specifically including: displaying the first satellite search guidance interface , in response to the user's leftward movement operation or rightward movement operation on the terminal, update the display position of the first satellite identification; when the first satellite identification is located in the first alignment area, display the second satellite search guidance interface; in response to the user
  • the display position of the second satellite logo is updated by an upward movement operation or a downward movement operation of the terminal.
  • the first satellite search guidance interface will be displayed first.
  • the first satellite logo is located in the first alignment area, that is, the terminal is aligned with the target satellite in the azimuth angle.
  • the second satellite search guidance interface is displayed.
  • the second satellite search guidance interface may not include the first satellite identification and the first alignment area, or may include the first satellite identification and the first alignment area. It can be seen from this implementation method that this application provides diversified presentation methods for the star search guidance interface.
  • the above steps display a satellite search guidance interface; and, in response to the user's mobile operation of the terminal, update the display position of the satellite identification, specifically including: displaying a second satellite search guidance interface , in response to the user's upward movement operation or downward movement operation on the terminal, the display position of the second satellite identification is updated; when the second satellite identification is located in the second alignment area, the first satellite search guidance interface is displayed; in response to the user's operation on the terminal, The leftward or rightward moving operation of the terminal updates the display position of the first satellite logo.
  • the second satellite search guidance interface will be displayed first.
  • the second satellite logo is located in the second alignment area, that is, the terminal is aligned with the target satellite at the pitch angle.
  • the first satellite search guidance interface is displayed.
  • the first satellite search guidance interface may not include the second satellite identification and the second alignment area, or may include the second satellite identification and the second alignment area. It can be seen from this implementation method that this application provides diversified presentation methods for the star search guidance interface.
  • the satellite search guidance interface includes a first satellite identification and a first alignment area, a second satellite identification and a second alignment area; the first satellite identification is used to indicate the terminal and the target The positional relationship of the satellite in the azimuth angle.
  • the first satellite identification is located in the first alignment area; the second satellite identification is used to indicate that the terminal and the target satellite are in the same position.
  • the positional relationship in the pitch angle when the final When the positional relationship between the terminal and the target satellite in pitch angle meets the message transmission conditions, the second satellite identifier is located in the second alignment area.
  • the satellite identification and alignment area are set from the two dimensions of the azimuth angle and pitch angle between the terminal and the target satellite, so that when adjusting the position of the terminal, the satellites on the star search guidance interface can be adjusted respectively.
  • the identification and alignment area adjusts the positional relationship between the terminal and the target satellite in azimuth and elevation angles, thereby speeding up the establishment of a communication connection between the terminal and the target satellite.
  • the above step: updating the display position of the satellite logo in response to the user's movement operation on the terminal specifically includes: responding to the user's leftward movement operation or rightward movement operation on the terminal. , update the display position of the first satellite logo; in response to the user's upward movement operation or downward movement operation on the terminal, update the display position of the second satellite logo.
  • the star search guidance interface includes the first satellite identification and the first alignment area.
  • the user can first move the terminal to the left or right, and first adjust the The positional relationship between the terminal and the target satellite in the direction angle, and then move the terminal upward or downward first to adjust the positional relationship between the terminal and the target satellite in the pitch angle.
  • the user adjusts the positional relationship in the azimuth angle and the pitch angle at the same time, such as: moving the terminal upward to the left or downward to the left, or moving the terminal upward to the right or moving the terminal downward to the right.
  • the user can move the terminal according to the guidance of the star finding prompt information displayed on the terminal. It can be seen from this implementation method that this application provides diversified presentation methods for the star search guidance interface.
  • the first alignment area when the display position of the first satellite logo is located outside the first alignment area, the first alignment area is displayed in the first color; the display position of the first satellite logo is located in the first alignment area.
  • the first alignment area is displayed in a second color, and the first color and the second color are different.
  • color changes can be used to indicate that the positions of the terminal and the target satellite in the azimuth angle have been adjusted, which can better prompt the user that the terminal has moved to the appropriate position in the left or right direction.
  • the second alignment area when the display position of the second satellite logo is located outside the second alignment area, the second alignment area is displayed in a third color; the display position of the second satellite logo is located in the third color.
  • the second alignment area is displayed in the fourth color, and the third color is different from the fourth color.
  • color changes can be used to indicate that the positions of the terminal and the target satellite in the pitch angle have been adjusted, which can better prompt the user that the terminal has moved to the appropriate position in the upward or downward direction.
  • the method when the terminal is used to send the first satellite message, before displaying the satellite search guidance interface, the method further includes: responding to the user's operation of creating a new satellite message or replying to the satellite message. Operation, display the satellite message editing interface, and the satellite message editing interface is used for the user to input the content of the first satellite message.
  • the terminal can configure the satellite message function in a short message application or other communication application, and then send the satellite message.
  • the above step: displaying a satellite search guidance interface specifically includes: displaying a satellite search guidance interface in response to a user's operation of sending the first satellite message.
  • the terminal responds to the user's operation of sending the first satellite message and displays a satellite search guidance interface for the user to perform the satellite search guidance process in the various implementation methods described above.
  • the above step: displaying the satellite search guidance interface specifically includes: in response to the user's operation of receiving the satellite message, displaying the satellite search guidance interface. .
  • the terminal when receiving a satellite message, responds to the user's operation of receiving the satellite message and displays a satellite search guidance interface for the user to perform the satellite search guidance process in the various implementation methods described above.
  • the method when the terminal is used to send the first satellite message, before displaying the satellite search guidance interface, the method further includes: sending an ordinary message to the base station; receiving a failure to send the ordinary message. Response message; the above steps: display the star search guidance interface, specifically including: in response to the response message that the ordinary message fails to be sent, display the star search guidance interface.
  • ordinary messages refer to messages sent through the base station. After the ordinary message fails to be sent, the content of the ordinary message can be transferred to the satellite message editing interface, and the content of the ordinary message can be sent through the satellite message. In this way, the success rate of message sending can be improved.
  • the method further includes: in response to the user's sending operation of the second satellite message, determining the position change after the terminal sends the first satellite message; If the position change after the terminal sends the first satellite message is less than the first threshold, the second satellite message is sent to the target satellite without displaying the satellite search guidance interface.
  • the first threshold may be preconfigured.
  • the user adjusts the positional relationship between the terminal and the target satellite and establishes a communication connection between the terminal and the target satellite.
  • the user can remain in At this position, when sending a second satellite message to the same recipient or a different recipient, there is no need to display the satellite search guidance interface. In this way, the speed of sending satellite messages can be increased.
  • the method after sending the first satellite message, also includes: in response to the user's sending operation of the second satellite message, determining the time when the terminal sends the first satellite message; if the terminal sends the second satellite message, If the time difference between the first satellite message and the user triggering the sending operation of the second satellite message is less than the second threshold, the second satellite message is sent to the target satellite without displaying the satellite search guidance interface.
  • the method after sending the first satellite message to the target satellite, the method further includes: receiving a response message indicating a failure to send the first satellite message; and receiving a response message indicating a failure to send the first satellite message. message to display the star finding guidance interface.
  • the first satellite message fails to be sent, it means that the communication connection between the terminal and the target satellite is disconnected or the signal is poor, and the positional relationship between the terminal and the target satellite needs to be adjusted again.
  • a second aspect of this application provides a terminal, including:
  • the display unit is used to display the satellite search guidance interface.
  • the satellite search guidance interface includes a satellite identifier.
  • the display position of the satellite identifier on the satellite search guidance interface is used to indicate the positional relationship between the terminal and the target satellite.
  • the processing unit is configured to update the display position of the satellite identification displayed by the display unit in response to the user's movement operation on the terminal.
  • the transceiver unit is used to send the first satellite message to the target satellite or receive the first satellite message from the target satellite if the positional relationship between the moved terminal and the target satellite satisfies the message transmission condition.
  • the star-finding guidance interface also includes star-finding prompt information, and the star-finding prompt information is used to prompt the user for the direction of the mobile terminal.
  • the star finding guidance interface includes a first star finding guidance interface and a second star finding guidance interface;
  • the first star finding guidance interface includes a first satellite identification and a first alignment area,
  • the first satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the azimuth angle.
  • the first satellite identification is located in the first alignment area;
  • the second The satellite search guidance interface includes a second satellite identification and a second alignment area.
  • the second satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle.
  • the second satellite identifier is located in the second alignment area.
  • the display unit is specifically configured to display the first star finding guidance interface.
  • the processing unit is specifically configured to update the display position of the first satellite logo in response to the user's leftward movement operation or rightward movement operation on the terminal.
  • the display unit is specifically configured to display the second satellite search guidance interface when the first satellite identifier is located in the first alignment area.
  • the processing unit is specifically configured to update the display position of the second satellite logo in response to the user's upward movement operation or downward movement operation on the terminal.
  • the display unit is specifically configured to display the second star finding guidance interface.
  • the processing unit is specifically configured to update the display position of the second satellite logo in response to the user's upward movement operation or downward movement operation on the terminal.
  • the display unit is specifically configured to display the first satellite search guidance interface when the second satellite identifier is located in the second alignment area.
  • the processing unit is specifically configured to update the display position of the first satellite logo in response to the user's leftward or rightward movement operation of the terminal.
  • the satellite search guidance interface includes a first satellite identification and a first alignment area, a second satellite identification and a second alignment area; the first satellite identification is used to indicate the terminal and the target The positional relationship of the satellite in the azimuth angle.
  • the first satellite identification is located in the first alignment area; the second satellite identification is used to indicate that the terminal and the target satellite are in the same position.
  • the positional relationship in the pitch angle When the positional relationship between the terminal and the target satellite in the pitch angle satisfies the message transmission condition, the second satellite identifier is located in the second alignment area.
  • the processing unit is specifically configured to update the display position of the first satellite logo in response to the user's leftward movement operation or rightward movement operation on the terminal; in response to the user's leftward movement operation or rightward movement operation on the terminal; Move up or move down to update the display position of the second satellite logo.
  • the first alignment area when the display position of the first satellite logo is located outside the first alignment area, the first alignment area is displayed in the first color; the display position of the first satellite logo is located in the first alignment area.
  • the first alignment area is displayed in a second color, and the first color and the second color are different.
  • the second alignment area when the display position of the second satellite logo is located outside the second alignment area, the second alignment area is displayed in a third color; the display position of the second satellite logo is located in the third color.
  • the second alignment area is displayed in the fourth color, and the third color is different from the fourth color.
  • the display unit is also configured to respond to the user's operation of creating a new satellite message or reply to the satellite message before displaying the satellite search guidance interface when the terminal is used to send the first satellite message.
  • the operation displays the satellite message editing interface.
  • the satellite message editing interface is used for the user to input the content of the first satellite message.
  • the display unit is specifically configured to respond to the user's response to the first satellite message. Send the message and display the star search guidance interface.
  • the display unit is specifically configured to display a star finding guidance interface in response to a user's operation of receiving satellite messages.
  • the transceiver unit is also configured to send an ordinary message to the base station; and receive a response message indicating that the ordinary message fails to be sent.
  • the display unit is specifically used to display the star finding guidance interface in response to a response message that fails to send an ordinary message.
  • the processing unit is further configured to determine the position change after the terminal sends the first satellite message in response to the user's operation of sending the second satellite message.
  • the transceiver unit is also used to send a second satellite message to the target satellite without displaying the satellite search guidance interface if the position change after the terminal sends the first satellite message is less than the first threshold.
  • the transceiver unit is also configured to receive a response message indicating that the first satellite message fails to be sent.
  • the display unit is also used to display the satellite search guidance interface according to the response message of failure to send the first satellite message.
  • a third aspect of the present application provides a terminal, which is used to perform the method in the foregoing first aspect or any possible implementation of the first aspect.
  • the fourth aspect of this application provides a chip system.
  • the chip system includes one or more interface circuits and one or more processors; the interface circuit and the processor are interconnected through lines; the interface circuit is used to receive signals from the memory of the terminal, and sends a signal to the processor, where the signal includes computer instructions stored in the memory; when the processor executes the computer instructions, the terminal executes the method in the aforementioned first aspect or any possible implementation of the first aspect.
  • the fifth aspect of the present application provides a computer-readable storage medium on which a computer program or instructions are stored.
  • the computer program or instructions When the computer program or instructions are run on a computer, the computer is caused to execute the aforementioned first aspect or any possible method of the first aspect. Methods in the implementation.
  • a sixth aspect of the present application provides a computer program product.
  • the computer program product includes computer program code.
  • the computer program code When executed on a computer, it causes the computer to execute the aforementioned first aspect or any possible implementation of the first aspect. Methods.
  • Figure 1A is a schematic diagram of an application scenario provided by an embodiment of the present application.
  • Figure 1B is another schematic diagram of an application scenario provided by an embodiment of the present application.
  • Figure 1C is another schematic diagram of an application scenario provided by an embodiment of the present application.
  • Figure 1D is another schematic diagram of an application scenario provided by an embodiment of the present application.
  • Figure 1E is another schematic diagram of an application scenario provided by an embodiment of the present application.
  • Figure 2 is a schematic structural diagram of a terminal provided by an embodiment of the present application.
  • Figure 3 is a schematic diagram of an embodiment of a message sending method provided by an embodiment of the present application.
  • Figure 4A is a schematic diagram of an interface provided by an embodiment of the present application.
  • Figure 4B is a schematic interface diagram of the information provided by the embodiment of the present application.
  • Figure 4C is a schematic interface diagram of a satellite short message provided by an embodiment of the present application.
  • Figure 4D is a schematic interface diagram of a new satellite short message provided by an embodiment of the present application.
  • Figure 5A is a schematic diagram of a loading interface for star finding guidance provided by an embodiment of the present application.
  • Figure 5B is a schematic diagram of the three-dimensional coordinate system provided by the embodiment of the present application.
  • 5C to 5F are multiple schematic diagrams of the star finding guidance interface provided by the embodiment of the present application.
  • FIGS 6A to 6D are multiple schematic diagrams of the star finding guidance interface provided by embodiments of the present application.
  • FIG. 7A to 7C are multiple schematic diagrams of the star finding guidance interface provided by the embodiment of the present application.
  • FIGS. 8A to 8C are multiple schematic diagrams of the star finding guidance interface provided by the embodiment of the present application.
  • Figure 9 is another schematic diagram of the star finding guidance interface provided by the embodiment of the present application.
  • FIGS. 10A to 10D are multiple schematic diagrams of the star finding guidance interface provided by embodiments of the present application.
  • Figure 11A is a schematic diagram of the satellite message editing interface provided by the embodiment of the present application.
  • Figure 11B is another schematic diagram of the satellite message editing interface provided by the embodiment of the present application.
  • Figure 11C is another schematic diagram of the satellite message editing interface provided by the embodiment of the present application.
  • Figure 11D is another schematic diagram of the satellite message editing interface provided by the embodiment of the present application.
  • Figure 11E is another schematic diagram of the satellite message editing interface provided by the embodiment of the present application.
  • Figure 12 is a schematic diagram of an embodiment of a message receiving method provided by an embodiment of the present application.
  • Figure 13A is another schematic interface diagram of a satellite short message provided by an embodiment of the present application.
  • Figure 13B is another schematic interface diagram of a satellite short message provided by an embodiment of the present application.
  • Figure 14 is another schematic structural diagram of a terminal provided by an embodiment of the present application.
  • Embodiments of the present application provide a message transmission method for guiding a user to adjust the positional relationship between a terminal and a target satellite through a satellite search guidance interface, thereby enabling the terminal to quickly send or receive satellite messages.
  • This application also provides corresponding terminals, computer-readable storage media, computer program products, etc. Each is explained in detail below.
  • Figures 1A to 1E show the application scenario of sending satellite messages
  • Figure 1C, Figure 1D and Figure 1E show the application scenario of receiving satellite messages.
  • satellite messages refer to messages directly sent by the terminal to the satellite, or messages directly received by the terminal from the satellite. Messages that need to be transferred between the terminal and the satellite through other devices (such as base stations or cloud networks) are called ordinary messages.
  • the message application or other communication applications of the terminal can be configured with a satellite message function item.
  • the user can edit the satellite message through the satellite message function item on the terminal, and click the send operation, and then the terminal sends the satellite message to the satellite. information.
  • the user can click the satellite message receiving operation on the terminal through the satellite message function item, and then the terminal receives the satellite message from the satellite.
  • a messaging application refers to an application used to send or receive messages (short messages, SM).
  • Other communication applications may be instant messaging applications or other applications that can receive or send messages.
  • the application scenario of sending satellite messages may include: a first terminal, a satellite, a base station and a second terminal.
  • the first terminal sends a satellite message to the satellite.
  • the satellite After receiving the satellite message, the satellite sends the content of the satellite message to the base station.
  • the base station sends the content of the satellite message to the second terminal.
  • the second terminal After receiving the content of the satellite message, the second terminal Displayed as a normal message.
  • the application scenario of sending satellite messages is shown in Figure 1B.
  • the application scenario may include: a first terminal, a satellite, a cloud network and a second terminal.
  • the first terminal sends a satellite message to the satellite.
  • the satellite After receiving the satellite message, the satellite sends the content of the satellite message to the cloud network.
  • the cloud network sends the content of the satellite message to the second terminal, and the second terminal receives the content of the satellite message through the cloud network.
  • the content of the satellite message can be displayed in the ordinary message of the corresponding application (App).
  • the application scenario may include: a first terminal, a satellite and a second terminal.
  • the first terminal sends satellite messages to the satellite, and the satellite receives the satellite message. After receiving the message, the satellite message is sent to the second terminal. After receiving the satellite message from the satellite, the second terminal displays the satellite message.
  • the application scenario of receiving satellite messages may include: a first terminal, a base station, a satellite, and a second terminal.
  • the first terminal sends a common message to the base station, and the base station sends the common message to the satellite.
  • the satellite After receiving the common message, the satellite sends the content of the common message to the second terminal.
  • the second terminal After receiving the content of the common message, the second terminal The content of the ordinary message is displayed in the form of satellite message in the satellite message function item.
  • the application scenario may include: a first terminal, a satellite, a cloud network and a second terminal.
  • the first terminal sends an ordinary message to the cloud network.
  • the cloud network sends the ordinary message to the satellite.
  • the satellite After receiving the ordinary message, the content of the ordinary message is sent to the second terminal.
  • the second terminal After receiving the content of the ordinary message, the second terminal displays the content of the ordinary message in the form of a satellite message in the satellite message function item.
  • the above process can also involve multiple satellites. Taking two satellites as an example, one of the satellites receives the signal from the first terminal. After receiving the satellite message, the satellite message can be sent to another satellite, and the other satellite sends the satellite message to a second terminal or other device (such as a base station or cloud network).
  • a second terminal or other device such as a base station or cloud network
  • Both the first terminal and the second terminal described above can be a mobile phone, a tablet computer (pad), a portable game console, a handheld computer (personal digital assistant, PDA), a notebook computer, or an ultra mobile personal computer (UMPC). ), handheld computers, netbooks, vehicle-mounted media playback equipment, wearable electronic devices, virtual reality (VR) terminal equipment, augmented reality (AR) terminal equipment and other digital display products.
  • the embodiments of this application are only described taking the example that the first terminal and the second terminal are mobile phones.
  • the terminal may include a processor 210, an external memory interface 220, an internal memory 221, a universal serial bus (USB) interface 230, a charging management module 240, a power management module 241, a battery 242, and an antenna.
  • a processor 210 an external memory interface 220, an internal memory 221, a universal serial bus (USB) interface 230, a charging management module 240, a power management module 241, a battery 242, and an antenna.
  • Antenna 2 antenna 3 mobile communication module 250, satellite communication module 251, wireless communication module 260, audio module 270, speaker 270A, receiver 270B, microphone 270C, headphone interface 270D, sensor module 280, button 290, motor 291, Indicator 292, camera 293, display screen 294, and subscriber identification module (subscriber identification module, SIM) card interface 295, etc.
  • SIM subscriber identification module
  • the sensor module 280 may include a pressure sensor 280A, a gyro sensor 280B, an air pressure sensor 280C, a magnetic sensor 280D, an acceleration sensor 280E, a distance sensor 280F, a proximity light sensor 280G, a fingerprint sensor 280H, a temperature sensor 280J, a touch sensor 280K, and an environment.
  • the structure illustrated in this embodiment does not constitute a specific limitation on the terminal.
  • the terminal may include more or fewer components than shown, or some components may be combined, or some components may be separated, or may be arranged differently.
  • the components illustrated may be implemented in hardware, software, or a combination of software and hardware.
  • the processor 210 may include one or more processing units.
  • the processor 210 may include an application processor (application processor, AP), a modem processor, a graphics processing unit (GPU), and an image signal processor. (image signal processor, ISP), controller, memory, video codec, digital signal processor (digital signal processor, DSP), baseband processor, and/or neural-network processing unit (NPU) wait.
  • application processor application processor, AP
  • modem processor graphics processing unit
  • GPU graphics processing unit
  • image signal processor image signal processor
  • ISP image signal processor
  • controller memory
  • video codec digital signal processor
  • DSP digital signal processor
  • NPU neural-network processing unit
  • different processing units can be independent devices or integrated in one or more processors.
  • the controller can be the nerve center and command center of the terminal.
  • the controller can generate operation control signals based on the instruction operation code and timing signals to complete the control of fetching and executing instructions.
  • the processor 210 may also be provided with a memory for storing instructions and data.
  • the memory in processor 210 is cache memory. This memory may hold instructions or data that have been recently used or recycled by processor 210 . If the processor 210 needs to use the instructions or data again, it can be called directly from the memory. Repeated access is avoided and the waiting time of the processor 210 is reduced, thus improving the efficiency of the system.
  • processor 210 may include one or more interfaces. Interfaces may include integrated circuit (inter-integrated circuit, I2C) interface, integrated circuit built-in audio (inter-integrated circuit sound, I2S) interface, pulse code modulation (PCM) interface, universal asynchronous receiver and transmitter (universal asynchronous receiver/transmitter (UART) interface, mobile industry processor interface (MIPI), general-purpose input/output (GPIO) interface, subscriber identity module (SIM) interface, and /or universal serial bus (USB) interface, etc.
  • I2C integrated circuit
  • I2S integrated circuit built-in audio
  • PCM pulse code modulation
  • UART universal asynchronous receiver and transmitter
  • MIPI mobile industry processor interface
  • GPIO general-purpose input/output
  • SIM subscriber identity module
  • USB universal serial bus
  • the interface connection relationships between the modules illustrated in this embodiment are only schematic illustrations and do not constitute structural limitations on the terminal.
  • the terminal may also adopt different interface connection methods in the above embodiments, or a combination of multiple interface connection methods.
  • the charge management module 240 is used to receive charging input from the charger.
  • the charger can be a wireless charger or a wired charger.
  • the charging management module 240 may receive charging input from the wired charger through the USB interface 230 .
  • the charging management module 240 may receive wireless charging input through the wireless charging coil of the terminal. While charging the battery 242, the charging management module 240 can also provide power to the terminal through the power management module 241.
  • the power management module 241 is used to connect the battery 242, the charging management module 240 and the processor 210.
  • the power management module 241 receives input from the battery 242 and/or the charging management module 240 and supplies power to the processor 210, internal memory 221, external memory, display screen 294, camera 293, wireless communication module 260, etc.
  • the power management module 241 can also be used to monitor battery capacity, battery cycle times, battery health status (leakage, impedance) and other parameters.
  • the power management module 241 may also be provided in the processor 210 .
  • the power management module 241 and the charging management module 240 may also be provided in the same device.
  • the wireless communication function of the terminal can be implemented through antenna 1, antenna 2, antenna 3, mobile communication module 250, satellite communication module 251, wireless communication module 260, modem processor and baseband processor, etc.
  • Antenna 1, Antenna 2 and Antenna 3 are used to transmit and receive electromagnetic wave signals.
  • Each antenna in a terminal can be used to cover a single or multiple communication bands. Different antennas can also be reused to improve antenna utilization.
  • Antenna 1 can be reused as a diversity antenna for a wireless LAN. In other embodiments, antennas may be used in conjunction with tuning switches.
  • Antenna 3 may be used to transmit signals to and/or receive signals from satellites.
  • the mobile communication module 250 can provide wireless communication solutions including 2G/3G/4G/5G applied on the terminal.
  • the mobile communication module 250 may include at least one filter, switch, power amplifier, low noise amplifier (LNA), etc.
  • the mobile communication module 250 can receive electromagnetic waves from the antenna 1, perform filtering, amplification and other processing on the received electromagnetic waves, and transmit them to the modem processor for demodulation.
  • the mobile communication module 250 can also amplify the signal modulated by the modem processor and convert it into electromagnetic waves through the antenna 1 for radiation.
  • at least part of the functional modules of the mobile communication module 250 may be disposed in the processor 210 .
  • at least part of the functional modules of the mobile communication module 250 and at least part of the modules of the processor 210 may be provided in the same device.
  • the satellite communication module 251 can provide a solution for communicating with satellites on the terminal.
  • the satellite communication module 251 may be one or more devices integrating at least one communication processing module.
  • the satellite communication module 251 receives electromagnetic waves through the antenna 3 , frequency modulates and filters the electromagnetic wave signals, and sends the processed signals to the processor 210 .
  • the satellite communication module 251 can also receive the signal to be sent from the processor 210, frequency modulate it, amplify it, and convert it into electromagnetic waves through the antenna 3 for radiation.
  • a modem processor may include a modulator and a demodulator.
  • the modulator is used to modulate the low-frequency baseband signal to be sent into a medium-high frequency signal.
  • the demodulator is used to demodulate the received electromagnetic wave signal into a low-frequency baseband signal.
  • the demodulator then transmits the demodulated low-frequency baseband signal to the baseband processor for processing.
  • the application processor outputs sound signals through audio devices (not limited to speaker 270A, receiver 270B, etc.), or displays images or videos through display screen 294.
  • the modem processor may It is an independent device.
  • the modem processor may be independent of the processor 210 and may be provided in the same device as the mobile communication module 250 or other functional modules.
  • the wireless communication module 260 can provide applications on the terminal including wireless local area networks (WLAN) (such as wireless fidelity (Wi-Fi) network), Bluetooth (bluetooth, BT), global navigation satellite system (global navigation satellite system) Navigation satellite system, GNSS), frequency modulation (FM), near field communication technology (near field communication, NFC), infrared technology (infrared, IR) and other wireless communication solutions.
  • WLAN wireless local area networks
  • Bluetooth blue, BT
  • global navigation satellite system global navigation satellite system
  • GNSS global navigation satellite system
  • FM frequency modulation
  • NFC near field communication technology
  • infrared technology infrared, IR
  • the wireless communication module 260 may be one or more devices integrating at least one communication processing module.
  • the wireless communication module 260 receives electromagnetic waves via the antenna 2 , frequency modulates and filters the electromagnetic wave signals, and sends the processed signals to the processor 210 .
  • the wireless communication module 260 can also receive the signal to be sent from the processor 210, frequency modulate it
  • the antenna 1 of the terminal is coupled to the mobile communication module 250, and the antenna 2 is coupled to the wireless communication module 260, so that the terminal can communicate with the network and other devices through wireless communication technology.
  • the wireless communication technology may include global system for mobile communications (GSM), general packet radio service (GPRS), code division multiple access (codedivision multiple access, CDMA), broadband code Wideband code division multiple access (WCDMA), time-division code division multiple access (TDSCDMA), long term evolution (LTE), BT, GNSS, WLAN, NFC, FM, and /or IR technology, etc.
  • the GNSS may include global positioning system (GPS), global navigation satellite system (GLONASS), Beidou satellite navigation system (beidounavigation satellite system, BDS), quasi-zenith satellite system (quasi- zenith satellitesystem (QZSS) and/or satellite based augmentation systems (SBAS).
  • GPS global positioning system
  • GLONASS global navigation satellite system
  • Beidou satellite navigation system beidounavigation satellite system, BDS
  • quasi-zenith satellite system quasi-zenith satellite system
  • QZSS quasi-zenith satellite system
  • SBAS satellite based augmentation systems
  • the terminal implements display functions through the GPU, display screen 294, and application processor.
  • the GPU is an image processing microprocessor and is connected to the display screen 294 and the application processor. GPUs are used to perform mathematical and geometric calculations for graphics rendering.
  • Processor 210 may include one or more GPUs that execute program instructions to generate or alter display information.
  • the display screen 294 is used to display images, videos, etc.
  • the display screen 294 includes a display panel.
  • the display panel can use a liquid crystal display (LCD), an organic light-emitting diode (OLED), an active matrix organic light emitting diode or an active matrix organic light emitting diode (active-matrix organic light emitting diode).
  • diode, AMOLED organic light-emitting diode
  • flexible light-emitting diode flexible light-emitting diode (flex light-emitting diode, FLED), Miniled, MicroLed, Micro-oLed, quantum dot light emitting diode (quantum dot light emitting diode, QLED), etc.
  • the terminal can realize the shooting function through the ISP, camera 293, video codec, GPU, display screen 294 and application processor.
  • the ISP is used to process the data fed back by the camera 293. For example, when taking a photo, the shutter is opened, the light is transmitted to the camera sensor through the lens, the optical signal is converted into an electrical signal, and the camera sensor passes the electrical signal to the ISP for processing, and converts it into an image visible to the naked eye. ISP can also perform algorithm optimization on image noise, brightness, and skin color. ISP can also optimize the exposure, color temperature and other parameters of the shooting scene. In some embodiments, the ISP may be provided in the camera 293.
  • Camera 293 is used to capture still images or video.
  • the object passes through the lens to produce an optical image that is projected onto the photosensitive element.
  • the photosensitive element can be a charge coupled device (CCD) or a complementary metal-oxide-semiconductor (CMOS) phototransistor.
  • CMOS complementary metal-oxide-semiconductor
  • the photosensitive element converts the optical signal into an electrical signal, and then passes the electrical signal to the ISP to convert it into a digital image signal.
  • ISP outputs digital image signals to DSP for processing.
  • DSP converts digital image signals into standard RGB, YUV and other format image signals.
  • the terminal may include 1 or N cameras 293, where N is a positive integer greater than 1.
  • the camera 293 can also be used to provide the terminal with a personalized and contextualized service experience to the user based on the perceived external environment and user actions. Among them, the camera 293 can obtain rich and accurate information so that the terminal can perceive the external environment and user's actions. Specifically, in this embodiment of the present application, the camera 293 can be used to identify whether the user of the terminal is the first user or the second user.
  • Digital signal processors are used to process digital signals. In addition to digital image signals, they can also process other digital signals. For example, when the terminal selects a frequency point, the digital signal processor is used to perform Fourier transform on the frequency point energy.
  • Video codecs are used to compress or decompress digital video.
  • the terminal can support one or more video codecs.
  • the terminal can play or record videos in multiple encoding formats, such as: moving picture experts group (MPEG)1, MPEG2, MPEG3, MPEG4, etc.
  • MPEG moving picture experts group
  • NPU is a neural network (NN) computing processor.
  • NN neural network
  • NPU can realize terminal intelligent cognitive applications, such as image recognition, face recognition, speech recognition, text understanding, etc.
  • the external memory interface 220 can be used to connect an external memory card, such as a Micro SD card, to expand the storage capacity of the terminal.
  • the external memory card communicates with the processor 210 through the external memory interface 220 to implement the data storage function. Such as saving music, videos, etc. files in external memory card.
  • Internal memory 221 may be used to store computer executable program code, which includes instructions.
  • the processor 210 executes instructions stored in the internal memory 221 to execute various functional applications and data processing of the terminal. For example, in this embodiment of the present application, the processor 210 can respond to the user's operation on the display screen 294 by executing instructions stored in the internal memory 221 to display corresponding display content on the display screen.
  • the internal memory 221 may include a program storage area and a data storage area. Among them, the stored program area can store an operating system, at least one application program required for a function (such as a sound playback function, an image playback function, etc.). The storage data area can store data created during the use of the terminal (such as audio data, phone book, etc.).
  • the internal memory 221 may include high-speed random access memory, and may also include non-volatile memory, such as at least one disk storage device, a flash memory device, universal flash storage (UFS), etc.
  • the terminal can implement audio functions through the audio module 270, the speaker 270A, the receiver 270B, the microphone 270C, the headphone interface 270D, and the application processor. Such as music playback, recording, etc.
  • the audio module 270 is used to convert digital audio information into analog audio signal output, and is also used to convert analog audio input into digital audio signals. Audio module 270 may also be used to encode and decode audio signals. In some embodiments, the audio module 270 may be provided in the processor 210 , or some functional modules of the audio module 270 may be provided in the processor 210 . Speaker 270A, also called “speaker”, is used to convert audio electrical signals into sound signals. The terminal can listen to music through the speaker 270A, or listen to hands-free calls. Receiver 270B, also known as "earpiece”, is used to convert audio electrical signals to Replace it with an audio signal. When the terminal answers a call or voice message, the voice can be heard by bringing the receiver 270B close to the human ear.
  • Microphone 270C also called “microphone” or “microphone” is used to convert sound signals into electrical signals.
  • the user can speak by approaching the microphone 270C with the human mouth and input the sound signal to the microphone 270C.
  • the terminal can be provided with at least one microphone 270C.
  • the terminal may be provided with two microphones 270C, which in addition to collecting sound signals, may also implement a noise reduction function.
  • the terminal can also be equipped with three, four or more microphones 270C to collect sound signals, reduce noise, identify sound sources, and implement directional recording functions, etc.
  • the headphone interface 270D is used to connect wired headphones.
  • the headphone interface 270D can be a USB interface 230, or a 3.5mm open mobile terminal platform (OMTP) standard interface, or a cellular telecommunications industry association of the USA (CTIA) standard interface.
  • OMTP open mobile terminal platform
  • CTIA cellular telecommunications industry association of the USA
  • the pressure sensor 280A is used to sense pressure signals and can convert the pressure signals into electrical signals.
  • pressure sensor 280A may be disposed on display screen 294.
  • pressure sensors 280A such as resistive pressure sensors, inductive pressure sensors, capacitive pressure sensors, etc.
  • a capacitive pressure sensor may include at least two parallel plates of conductive material. When a force is applied to pressure sensor 280A, the capacitance between the electrodes changes. The terminal determines the intensity of the pressure based on changes in capacitance. When a touch operation is performed on the display screen 294, the terminal detects the strength of the touch operation according to the pressure sensor 280A. The terminal may also calculate the touched position based on the detection signal of the pressure sensor 280A.
  • touch operations acting on the same touch location but with different touch operation intensities may correspond to different operation instructions. For example: when a touch operation with an intensity less than the pressure threshold is applied to the short message application icon, the instruction to view the short message is executed. When a touch operation with a touch operation intensity greater than or equal to the pressure threshold is applied to the short message application icon, the instruction to create a new short message is executed.
  • the gyro sensor 280B can be used to determine the movement posture of the terminal.
  • the angular velocity of the terminal about three axes may be determined by gyro sensor 280B.
  • the gyro sensor 280B can be used for image stabilization. For example, when the shutter is pressed, the gyro sensor 280B detects the angle of the terminal shake, calculates the distance that the lens module needs to compensate based on the angle, and allows the lens to offset the terminal shake through reverse movement to achieve anti-shake.
  • the gyro sensor 280B can also be used for navigation and somatosensory gaming scenarios.
  • the gyro sensor 280B can also be used to measure the rotation amplitude or movement distance of the terminal.
  • Air pressure sensor 280C is used to measure air pressure. In some embodiments, the terminal calculates the altitude through the air pressure value measured by the air pressure sensor 280C to assist positioning and navigation.
  • Magnetic sensor 280D includes a Hall sensor.
  • the terminal can use the magnetic sensor 280D to detect the opening and closing of the flip leather case.
  • the terminal may detect opening and closing of the flip according to the magnetic sensor 280D. Then, based on the detected opening and closing status of the leather case or the opening and closing status of the flip cover, features such as automatic unlocking of the flip cover are set.
  • the acceleration sensor 280E can detect the acceleration of the terminal in various directions (generally three axes). When the terminal is stationary, the magnitude and direction of gravity can be detected. It can also be used to identify terminal gestures and be used in horizontal and vertical screen switching, pedometer and other applications. In addition, the acceleration sensor 280E can also be used to measure the orientation of the terminal (ie, the direction vector of the orientation).
  • the terminal can measure distance via infrared or laser. In some embodiments, when shooting a scene, the terminal can use the distance sensor 280F to measure distance to achieve fast focusing.
  • Proximity light sensor 280G may include, for example, a light emitting diode (LED) and a light detector, such as a photodiode.
  • the light emitting diode may be an infrared light emitting diode.
  • the terminal emits infrared light through a light-emitting diode.
  • the terminal uses photodiodes to detect infrared reflected light from nearby objects. When sufficient reflected light is detected, it can be determined that there is an object near the terminal. When insufficient reflected light is detected, the terminal can determine that there is no object near the terminal.
  • the terminal can use the proximity light sensor 280G to detect when the user holds the terminal close to the ear to talk, so that the screen can be automatically turned off to save power.
  • the proximity light sensor 280G can also be used in holster mode, and pocket mode automatically unlocks and locks the screen.
  • the ambient light sensor 280L is used to sense ambient light brightness.
  • the terminal can adaptively adjust the brightness of the display screen 294 according to the perceived ambient light brightness.
  • the ambient light sensor 280L can also be used to automatically adjust the white balance when taking pictures.
  • the ambient light sensor 280L can also cooperate with the proximity light sensor 280G to detect whether the terminal is in a pocket to prevent accidental touches.
  • Fingerprint sensor 280H is used to collect fingerprints.
  • the terminal can use the collected fingerprint characteristics to realize fingerprint unlocking, access application lock, fingerprint photo taking, fingerprint answering incoming calls, etc.
  • Temperature sensor 280J is used to detect temperature.
  • the terminal uses the temperature detected by the temperature sensor 280J to execute the temperature processing policy. For example, when the temperature reported by the temperature sensor 280J exceeds a threshold, the terminal reduces the performance of a processor located near the temperature sensor 280J in order to reduce power consumption and implement thermal protection.
  • the terminal when the temperature is lower than another threshold, the terminal heats the battery 242 to avoid abnormal shutdown of the terminal due to low temperature.
  • the terminal when the temperature is lower than another threshold, the terminal performs boosting on the output voltage of the battery 242 to avoid abnormal shutdown caused by low temperature.
  • Touch sensor 280K also called “touch panel”.
  • the touch sensor 280K can be disposed on the display screen 294.
  • the touch sensor 280K and the display screen 294 form a touch screen, which is also called a "touch screen”.
  • the touch sensor 280K is used to detect a touch operation on or near the touch sensor 280K.
  • the touch sensor can pass the detected touch operation to the application processor to determine the touch event type.
  • Visual output related to the touch operation may be provided through display screen 294.
  • the touch sensor 280K may also be disposed on the surface of the terminal, at a location different from that of the display screen 294 .
  • Bone conduction sensor 280M can acquire vibration signals.
  • the bone conduction sensor 280M can acquire the vibration signal of the vibrating bone mass of the human body's vocal part.
  • the bone conduction sensor 280M can also contact the human body's pulse and receive blood pressure beating signals.
  • the bone conduction sensor 280M can also be provided in the earphone and combined into a bone conduction earphone.
  • the audio module 270 can analyze the voice signal based on the vibration signal of the vocal vibrating bone obtained by the bone conduction sensor 280M to implement the voice function.
  • the application processor can analyze the heart rate information based on the blood pressure beat signal obtained by the bone conduction sensor 280M to implement the heart rate detection function.
  • Motion sensor 280N can acquire motion data.
  • the buttons 290 include a power button, a volume button, etc.
  • Key 290 may be a mechanical key. It can also be a touch button.
  • the terminal can receive key input and generate key signal input related to user settings and function control of the terminal.
  • the terminal identifies the operations (including the first operation, the second operation, the third operation, etc.) mentioned in the embodiments of this application through various sensors, buttons 290, and/or cameras 293 in the sensor module 280 .
  • the motor 291 can generate vibration prompts.
  • the motor 291 can be used for vibration prompts for incoming calls and can also be used for touch vibration feedback.
  • touch operations for different applications can correspond to different vibration feedback effects.
  • Acting on touch operations in different areas of the display screen 294, the motor 291 can also correspond to different vibration feedback effects.
  • Different application scenarios (such as time reminders, receiving messages, alarm clocks, games, etc.) can also correspond to different vibrations feedback effect.
  • the touch vibration feedback effect can also be customized.
  • the indicator 292 may be an indicator light, which may be used to indicate charging status, power changes, or may be used to indicate messages, missed calls, notifications, etc.
  • the SIM card interface 295 is used to connect a SIM card.
  • the SIM card can be inserted into the SIM card interface 295 or pulled out from the SIM card interface 295 to achieve contact and separation from the terminal.
  • the terminal can support 1 or N SIM card interfaces, where N is a positive integer greater than 1.
  • SIM card interface 295 can support Nano SIM card, Micro SIM card, SIM card, etc. Multiple cards can be inserted into the same SIM card interface 295 at the same time. The types of the plurality of cards may be the same or different.
  • the SIM card interface 295 is also compatible with different types of SIM cards.
  • the SIM card interface 295 is also compatible with external memory cards.
  • the terminal interacts with the network through the SIM card to implement functions such as calls and data communications.
  • the terminal uses eSIM, that is, an embedded SIM card.
  • the eSIM card can be embedded in the terminal and cannot be separated from the terminal.
  • the following describes the satellite short message sending method and receiving method of the terminal provided by the embodiment of the present application, taking the following terminal as a mobile phone as an example.
  • the method may be executed by the terminal or by components of the terminal (such as a processor, a chip, or a chip system, etc.).
  • the message transmission method provided by the embodiment of the present application can be applied to the terminal introduced previously.
  • the message transmission method may include a message sending method and a message receiving method, which are introduced separately below.
  • an embodiment of the message sending method provided by the embodiment of the present application may include:
  • the terminal displays the star finding guidance interface.
  • the satellite search guidance interface includes a satellite identifier, and the display position of the satellite identifier on the satellite search guidance interface is used to indicate the positional relationship between the terminal and the target satellite.
  • the terminal may display a satellite message editing interface in response to the user's operation of creating a new satellite message or replying to a satellite message, and the satellite message editing interface is used for the user to input the content of the first satellite message. Then, the terminal may display a satellite search guidance interface in response to the user's operation of sending the first satellite message.
  • operations related to satellite messages can be completed in the satellite message function item, and the satellite message function item can be set in the information application, such as : Short message application or other communication application.
  • a satellite message application can also be designed for satellite messages to realize the function of the satellite message function item. If the satellite message function item is set in a short message application, the short message application has the function of a normal short message + the function of a satellite short message. If the satellite message function item is set in an instant messaging application, the instant messaging application has the function of instant messaging function + satellite message. If a satellite messaging application is designed for satellite messaging, the satellite messaging application must at least have the functionality of satellite messaging.
  • Satellite messaging function Users can usually use the satellite messaging function when the signal is poor or there is no mobile communication service.
  • a short message application is used as an example for explanation.
  • the satellite message involved in the short message application may be called a satellite short message.
  • the terminal displays the information interface as shown in Figure 4B in response to the user's click operation on the information application (short message application) 401 on the main interface of the mobile phone.
  • the information interface includes satellite short message function item 402.
  • the terminal displays the satellite short message interface shown in Figure 4C.
  • the satellite short message interface includes an identification 403 of "Create a new satellite short message" and may also include an identification 404 of "Receive a satellite short message".
  • the terminal displays a new satellite short message interface as shown in Figure 4D in response to the user's click operation on the logo 403 of "New Satellite Short Message".
  • the user can select the recipient in the recipient box, such as the recipient "Mary” as shown in Figure 4D, and then edit the content of the first satellite message in the edit box, as shown in Figure 4D "Everything is fine, don't worry” as shown in 4D.
  • the new satellite short message interface provided by the embodiment of the present application will include a "carry location" identifier 405. This identifier is usually in a default selected state.
  • the terminal When the terminal sends the content of the first satellite message to the target satellite, it will automatically carry the current terminal location. location information. Of course, the user can also cancel the function of carrying the location by clicking the " ⁇ " location. If the function of carrying the location is not checked, the location information of the current terminal location will not be carried when the content of the first satellite message is sent.
  • the terminal may display a loading interface as shown in Figure 5A in response to the user's click operation on the send button 406 in Figure 4D.
  • the loading interface can display prompt information such as "Please stay in an open area as much as possible to avoid foreign objects blocking signals in the line of sight", and can also display the loading progress.
  • the terminal may not display the loading interface as shown in Figure 5A, but may directly display the loaded result interface.
  • the loaded result interface may be called a star search guide. interface.
  • the terminal updates the display position of the satellite logo in response to the user's mobile operation on the terminal.
  • the star finding guidance interface is used to guide the user to adjust the position of the terminal.
  • the user can determine the positional relationship between the terminal and the target satellite through the display position of the satellite logo in the satellite search guidance interface, and then move the terminal (such as moving the terminal left or right, moving the terminal up or down), and the terminal will respond to the Move and adjust the display position of the satellite logo on the satellite search guidance interface.
  • the terminal sends the first satellite message to the target satellite.
  • the positional relationship between the moved terminal and the target satellite satisfies the message transmission condition, the positional relationship between the moved terminal and the target satellite can enable the terminal to establish a communication connection with the target satellite.
  • the terminal can guide the user to adjust the positional relationship between the terminal and the target satellite through the satellite search guidance interface, so that the terminal can quickly establish a communication connection with the satellite, so that the terminal can quickly send satellite messages.
  • the star-finding guidance interface may also include star-finding prompt information, and the star-finding prompt information is used to prompt the user for the direction of the mobile terminal.
  • the star search prompt information is to move the terminal to the left, move the terminal to the right, move the terminal up or move the terminal down.
  • the star-finding prompt information is usually a prompt given by the terminal according to the shortest movement path. In this way, the user moves the terminal according to the star-finding prompt information and can quickly move the terminal to a position suitable for establishing a communication connection with the target satellite. This in turn speeds up the terminal's ability to send or receive satellite messages to the target satellite.
  • the satellite search guidance interface and the interface for sending satellite messages in the embodiment of the present application can have multiple expressions, and the expressions are related to the order of adjusting the azimuth and pitch angles of the terminal and the target satellite.
  • the azimuth angle and pitch angle you can refer to the three-dimensional coordinate system (xyz) shown in Figure 5B for understanding.
  • the terminal is located at the center of the three-dimensional coordinate system.
  • the antenna on the terminal that communicates with the satellite is in the y-axis direction.
  • the angle is the y-axis and the projection point C of the satellite on the xy plane and
  • the angle between the line connecting the center of the circle and the pitch angle is the angle between the line connecting the satellite’s projection point C on the xy plane and the center of the circle, and the angle between the line connecting the satellite and the center of the circle.
  • the star finding guidance interface may include a first star finding guidance interface and a second star finding guidance interface.
  • the first satellite search guidance interface includes a first satellite identification and a first alignment area.
  • the first satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the azimuth angle. When the positional relationship between the terminal and the target satellite in the azimuth angle satisfies During the message transmission condition, the first satellite identifier is located in the first alignment area.
  • the second satellite search guidance interface includes a second satellite identification and a second alignment area. The second satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle. When the positional relationship between the terminal and the target satellite in the pitch angle satisfies During the message transmission condition, the second satellite identification is located in the second alignment area.
  • the star finding guidance interface may not be divided into a first star finding guidance interface and a second star finding guidance interface.
  • the star finding guidance interface includes a first satellite identification and a first alignment area, a second satellite logo and the second alignment area; the first satellite logo is used to indicate the positional relationship between the terminal and the target satellite in the azimuth angle.
  • the first satellite logo is located The first alignment area; the second satellite identifier is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle.
  • the second satellite identifier is located in the second Aim the area.
  • the expression form of the star search guidance interface is related to the sequence of adjusting the azimuth angle and pitch angle between the terminal and the target satellite.
  • the following is a description of the search results in different expression forms according to the sequence of adjusting the azimuth angle and pitch angle between the terminal and the target satellite.
  • Star guide interface is introduced.
  • a star-finding guidance interface when adjusting the azimuth angle can be understood with reference to FIG. 5C.
  • the star search guidance interface will display the message "Searching" 501, and the "Signal Status" logo 502 will also be displayed.
  • the four signal grids are in a blank state, indicating that there is no signal yet. signal
  • the area used to adjust the positional relationship between the terminal and the target satellite in Figure 5C is represented by the disk area 503
  • the first satellite identification 504 will be displayed in the disk area 503
  • the area covered by the antenna communicating with the target satellite is represented by a sector. means, usually a range of plus or minus 15° from the center line of the disc area 503.
  • the center line is a line passing through the center of the disc 503 and parallel to the y-axis.
  • This sector-shaped area can be called the first alignment area 505.
  • the star-finding guidance interface can also display star-finding prompt information, such as the words "turn the phone to the right" 506 in Figure 5C, which is a star-finding prompt message for adjusting the azimuth angle.
  • the positions of the first satellite identifier 504 and the first alignment area 505 in the disk area 505 are based on the position of the antenna in the terminal that communicates with the target satellite as a reference to determine the relative position of the target satellite. in the horizontal orientation of the terminal, and display the first satellite logo 504 in the corresponding position of the disk area 503.
  • the position of the first satellite identifier 504 may be determined by reverse calculation using the target satellite for positioning the mobile phone.
  • the specific content of the star finding prompt information displayed on the star finding guidance interface is related to the location of the first satellite identification 504.
  • the first satellite identification 504 is located on the right side of the first alignment area 505. side, that is, the range from 0° to 180° on the right side of the center line of the first alignment area 505, in order to enable the first satellite mark 504 to enter the first pair of satellites in a shorter path or at a smaller rotation angle.
  • the terminal usually gives a star-finding prompt message of “turn the phone to the right”.
  • the terminal will usually give a "turn the phone to the left" message.
  • Star search prompt information Although the embodiment of the present application does not provide a schematic diagram showing that the first satellite identifier 504 is located on the left side of the first alignment area 505, it is easy to understand based on the text description here and in conjunction with Figure 5C that the first satellite identifier 504 is located on the left side of the first alignment area 505. A plan aligned to the left of area 505.
  • the star-finding guidance interface shown in Figure 5C if the user operates according to the star-finding prompt information of "turn the phone to the right", or the degree of the user turning the phone to the left is the difference between 360° and the degree of turning the phone to the right. value, the first satellite logo 504 can be rotated to the first alignment area 505, and the interface of the terminal will be refreshed accordingly, displaying the satellite search guidance interface as shown in Figure 5D.
  • the first satellite logo 504 is located at the center line of the first alignment area 505, indicating that the azimuth angle has been adjusted. Because the pitch angle has not been adjusted yet, as shown in Figure 5D
  • the four signal grids of the "signal status" mark 502 in the star search guidance interface are still blank.
  • the first alignment area when the display position of the first satellite logo is located outside the first alignment area, the first alignment area is displayed in the first color; the display position of the first satellite logo is located in the first pair of When the first alignment area is within the alignment area, the first alignment area is displayed in a second color, and the first color and the second color are different.
  • the first alignment area 505 can be displayed in the first color before the azimuth angle is adjusted.
  • the first satellite The logo 504 is located behind the first alignment area 505.
  • the first alignment area 505 may be displayed in a second color.
  • the first color is different from the second color. In this way, the color change can better remind the user that the azimuth alignment has been completed.
  • a star-finding guidance interface for adjusting the pitch angle (second star-finding guidance interface).
  • a star-finding guidance interface when adjusting the pitch angle can be understood with reference to FIG. 6A.
  • the star finding guidance interface will display the message "Searching" and the "Signal Status" logo.
  • the four signal grids are blank, indicating that there is no signal yet.
  • the area used to adjust the positional relationship between the terminal and the target satellite in FIG. 6A is represented by a disk area.
  • the second satellite identification 601 will be displayed in the disk area, and the second alignment area 602 is a small disk in communication with the disk area.
  • the star-finding guidance interface can also display star-finding prompt information, such as the words "Lift the phone up" 603 in Figure 6A, which is a star-finding prompt message for adjusting the pitch angle.
  • the positions of the second satellite identifier 601 and the second alignment area 602 in the disk area are based on the position of the antenna in the terminal that communicates with the target satellite as a reference to determine the relative position of the target satellite.
  • the elevation position of the terminal is determined, and the second satellite identification 601 is displayed in the corresponding position of the disk area.
  • the specific content of the star finding prompt information displayed on the star finding guidance interface is related to the location of the second satellite identification 601.
  • the second satellite identification 601 is located in the center of the second alignment area 602.
  • the terminal will give a star-finding prompt message of "lift the phone upwards". If the second satellite mark 601 is located directly above the second alignment area 602, the terminal will give a star search prompt message of "press down on the mobile phone".
  • the embodiment of the present application does not provide a schematic diagram showing that the second satellite identification 601 is located directly above the second alignment area 602, it is easy to understand based on the text description here and in conjunction with FIG. 6A that the second satellite identification 601 is located at the second alignment area 602.
  • the second solution is to align directly above the area 602.
  • the terminal interface will be refreshed accordingly.
  • display the star finding guidance interface as shown in Figure 6B.
  • the second satellite identification 601 is located in the second alignment area.
  • the center position of 602 indicates that the pitch angle has been adjusted.
  • the second alignment area is displayed in the third color; when the display position of the second satellite logo is within the second alignment area, The second alignment area is displayed in a fourth color, the third color being different from the fourth color.
  • the second alignment area 602 can be displayed in the third color before the azimuth angle is adjusted. After the azimuth angle is adjusted, the second satellite logo 601 is located in the second alignment After the area 602, the second alignment area 602 can also be displayed in a fourth color, and the third color is different from the fourth color.
  • the color change process of the second alignment area 602 is not shown through a schematic diagram, it can also be displayed in conjunction with Figure 5E and understand the color change process in Figure 5F. In this way, the color change can better remind the user that the pitch angle alignment has been completed.
  • Option 3 A star-finding guidance interface that first adjusts the azimuth angle and then the elevation angle.
  • the solution 3 is to first display the first star finding guidance interface, and then display the second star finding guidance interface, corresponding to the previous steps 301 and 302.
  • This process may specifically include: displaying the first star finding guidance interface, in response to the user's input to the terminal. Move operation to the left or move to the right to update the display position of the first satellite identification; when the first satellite identification is located in the first alignment area, display the second satellite search guidance interface; in response to the user's upward movement operation on the terminal or Move downward to update the display position of the second satellite logo.
  • the terminal will successively display Figure 5C, Figure 5D, and Figure 5C. 6A and 6B, and then you can get the interface for sending satellite messages as shown in Figure 6C.
  • the interface for sending satellite short messages can only display the second satellite logo 601 and the second alignment area 602 of the interface for adjusting the pitch angle, and not display the first Satellite identification 504 and first alignment area 505 .
  • three of the four signals in the "signal status" mark 604 on the interface for sending satellite short messages are in a full state, indicating that a connection has been established with the satellite.
  • the interface for sending satellite short messages can also display The words "Sending” 605, and the words "Please keep holding the posture” 606 can also be displayed.
  • Option 4 A star-finding guidance interface that adjusts the pitch angle first and then the azimuth angle.
  • Solution 4 is to first display the second star finding guidance interface, and then display the first star finding guidance interface, corresponding to the previous steps 301 and 302.
  • This process may specifically include: displaying the second star finding guidance interface, in response to the user's input to the terminal.
  • the upward movement operation or the downward movement operation updates the display position of the second satellite identification; when the second satellite identification is located in the second alignment area, the first satellite search guidance interface is displayed; in response to the user moving the terminal to the left or to the Move right to update the display position of the first satellite logo.
  • the terminal will display Figure 6A, Figure 6B, and Figure 5C successively. and Figure 5D, and then you can get the interface for sending satellite short messages as shown in Figure 6D.
  • the interface for sending satellite short messages can only display the first satellite identification 504 and the first alignment area 505 of the interface for adjusting the azimuth angle, and not display the second Satellite identification 601 and second alignment area 602.
  • three of the four signals in the "signal status" mark 604 on the interface for sending satellite short messages are in a full state, indicating that a connection has been established with the satellite.
  • the interface for sending satellite short messages can also display The words "Sending” 605, and the words "Please keep holding the posture” 606 can also be displayed.
  • This solution 5 displays the first satellite search guidance interface first, and then displays the second satellite search guidance interface. What is different from the second satellite search guidance interface in Solution 3 is that the first satellite identification and the first alignment area are not displayed: The second satellite search guidance interface in Solution 5 also displays the first satellite identification and the first alignment area.
  • the terminal will successively display Figure 5C, Figure 5D, and then display the star search shown in Figure 7A Boot interface.
  • the star-finding guidance interface shown in Figure 7A can also display star-finding prompt information such as "lift the phone upwards", “signal status”, and "star-finding in progress”. These contents have been introduced in the previous part of Figure 6A and will not be repeated here.
  • the terminal interface will be refreshed accordingly.
  • the second satellite identification 601 is located in the center of the second alignment area 602, indicating that the pitch angle has been adjusted. It also displays that the first satellite identification 504 is located in the first alignment area. 505.
  • first satellite mark 504 deviates from the first alignment area 505 during the process of adjusting the pitch angle, the first satellite mark 504 can be adjusted back again using the principle of adjusting the azimuth angle introduced earlier. First alignment area 505.
  • the terminal will refresh the interface for sending satellite short messages as shown in Figure 7C.
  • the interface for sending satellite short messages can display both the second satellite logo 601 and the second alignment area 602 of the interface for adjusting the pitch angle, as well as the first Satellite identification 504 and first alignment area 505 .
  • three of the four signals in the "signal status" mark 604 on the interface for sending satellite short messages are in a full state, indicating that a connection has been established with the satellite.
  • the interface for sending satellite short messages can also display The words "Sending" 605, and the words "Please keep holding the posture" 606 can also be displayed.
  • Option 6 Another star-finding guidance interface that adjusts the elevation angle first and then the azimuth angle.
  • This solution 6 first displays the second satellite search guidance interface, and then displays the first satellite search guidance interface. What is different from the first satellite search guidance interface in Solution 4 is that the second satellite identification and the second alignment area are not displayed: The first satellite search guidance interface in Solution 6 also displays the second satellite identification and the second alignment area.
  • the terminal will successively display Figure 6A, Figure 6B, and then display the star search shown in Figure 8A Boot interface.
  • the star-finding guidance interface shown in Figure 8A can also display star-finding prompt information such as "turn the phone to the right", “signal status”, and "star-finding in progress”. These contents have been introduced in the previous part of Figure 5C and will not be repeated here.
  • the terminal interface will follow. Refresh to display the star finding guidance interface as shown in Figure 7B.
  • the first satellite identifier 504 is located in the first alignment area. 505, indicating that the azimuth angle has been adjusted, and it will also display that the second satellite identifier 601 is located in the second alignment area 602.
  • the terminal will refresh the interface for sending satellite short messages as shown in Figure 7C.
  • the interface for sending satellite short messages can display both the first satellite identification 504 and the first alignment area 505 of the interface for adjusting the azimuth angle, and also display the second Satellite identification 601 and second alignment area 602.
  • three of the four signals in the "signal status" mark 604 on the interface for sending satellite short messages are in a full state, indicating that a connection has been established with the satellite.
  • the interface for sending satellite short messages can also display The words "Sending" 605, and the words "Please keep holding the posture" 606 can also be displayed.
  • Option 7 Another star-finding guidance interface that adjusts the azimuth angle first and then the elevation angle.
  • the satellite search guidance interface of Solution 7 includes a first satellite identification and a first alignment area, a second satellite identification and a second alignment area.
  • Step 302 in the previous embodiment specifically includes: in response to the user's leftward movement operation or rightward movement operation on the terminal, updating the display position of the first satellite logo; in response to the user's upward movement operation or downward movement operation on the terminal, Update the display position of the second satellite logo.
  • the terminal can display the satellite search guidance interface as shown in Figure 8B in sequence.
  • the star finding guidance interface when adjusting the azimuth angle, not only the first satellite identification 504 and the first alignment area 505 are displayed, but also the second satellite identification 601 and the first alignment area 505 are displayed. Two alignment areas 602.
  • the star-finding guidance interface shown in Figure 8B can also display star-finding prompt information such as "turn the phone to the right", “signal status", and "star-finding in progress”. These contents have been introduced in the previous part of Figure 5C and will not be repeated here.
  • the terminal interface On the star-finding guidance interface shown in Figure 8B, if the user operates according to the star-finding prompt information of "turn the phone to the right" and turns the first satellite logo 504 to the first alignment area 505, the terminal interface will follow. Refresh to display the star finding guidance interface as shown in Figure 7A. Then, on the basis of the satellite search guidance interface shown in Figure 7A, the pitch angle is adjusted to refresh the satellite search guidance interface shown in Figure 7B, and then the interface for sending satellite short messages as shown in Figure 7C is refreshed.
  • Option 8 Another star finding guidance interface that adjusts the elevation angle first and then the azimuth angle.
  • the terminal can display the satellite search guidance interface as shown in Figure 8C in sequence.
  • the star finding guidance interface when adjusting the azimuth angle, not only the first satellite identification 504 and the first alignment area 505 are displayed, but also the second satellite identification 601 and the first alignment area 505 are displayed. Two alignment areas 602.
  • the star-finding guidance interface shown in Figure 8C can also display the star-finding prompt information of "lift the phone upwards", “signal status", and "star-finding in progress". These contents have been introduced in the previous part of Figure 5C and will not be repeated here.
  • the terminal interface On the star-finding guidance interface shown in Figure 8C, if the user operates according to the star-finding prompt information of "lift the phone up" and moves the second satellite identification 601 to the second alignment area 602, the terminal interface will be refreshed accordingly. , display the star finding guidance interface as shown in Figure 8A. Then adjust the azimuth angle based on the star finding guidance interface shown in Figure 8A and refresh the image as shown in Figure 7B In the satellite search guidance interface shown, the interface for sending satellite short messages as shown in Figure 7C is refreshed.
  • Solution 9 A star-finding guidance interface that simultaneously adjusts the azimuth and elevation angles.
  • the terminal can directly display the star-finding guidance interface as shown in Figure 9.
  • the star-finding prompt message in Figure 9 is "Turn the phone to the right. + Lift the phone up".
  • the satellite search guidance interface and the interface for sending satellite short messages only display the satellite identification of one satellite.
  • this application does not limit the satellite search guidance interface and the interface for sending satellite short messages.
  • the satellite identifications of multiple satellites can be displayed on the satellite search guidance interface and the interface for sending satellite short messages. The following shows two satellites. Taking the satellite identification of a satellite as an example, we will introduce option 10 in combination with the previous option 7 when displaying a satellite.
  • the satellite search guidance interface When displaying the satellite identifications of multiple satellites, the satellite search guidance interface first adjusts the azimuth angle and then the elevation angle.
  • the satellite search guidance interface shown in Figure 10A includes the satellite identifications of two satellites.
  • the first satellite identification 504 and the second satellite identification 601 of the first satellite (target satellite) have been introduced before.
  • the first satellite identification of the second satellite The satellite identification is represented by 1001, and the second satellite identification is represented by 1002.
  • the terminal provides "turn right" on the satellite search guidance interface shown in Figure 10A. "Mobile phone" star finding prompt information.
  • FIG. 10B displays the star-finding prompt information of "lifting the mobile phone upwards". If the user operates according to the star-finding prompt information of "lifting the mobile phone upwards", the second satellite identification 601 will be moved to In the second alignment area 602, the interface of the terminal will be refreshed accordingly, displaying the satellite search guidance interface as shown in Figure 10C, and then refreshing the interface for sending satellite short messages as shown in Figure 10D.
  • the first satellite identification 1001 and the second satellite identification 1002 of the second satellite are added on the basis of the above Solution 7.
  • options 8 and 9 you can add a satellite identification similar to that of another satellite introduced in option 10.
  • the terminal will determine the displayed star finding prompt information based on the relationship between another satellite and the first alignment area. It can be seen that there can be multiple star finding guidance interfaces and interfaces for sending satellite short messages when there are multiple satellites. This will not be introduced one by one in the embodiments of this application.
  • the first satellite message after sending the first satellite message, it is also possible to: in response to the user's sending operation of the second satellite message, determine the position change after the terminal sends the first satellite message; if the position change after the terminal sends the first satellite message If the position change is less than the first threshold, a second satellite message is sent to the target satellite without displaying the satellite search guidance interface.
  • the second satellite message may also be: in response to the user's sending operation of the second satellite message, determine the time when the terminal sends the first satellite message; if the time when the terminal sends the first satellite message is far from the user If the time difference between triggering the sending operations of the second satellite message is less than the second threshold, the second satellite message is sent to the target satellite without displaying the satellite search guidance interface.
  • the terminal after the terminal sends the first satellite short message, it can receive feedback from the satellite that the transmission is successful. For the previous message sent to the recipient "Mary", it can display The interface shown in Figure 11A. If the user is worried that the second terminal cannot successfully receive the message, he or she can keep the terminal in the posture of adjusting the azimuth and elevation angles and send the second satellite short message to the same recipient again. Because the time interval from the last satellite short message sent is very small or the position of the mobile phone has changed very little, there is no need to enter the satellite search guidance interface again when sending the satellite short message again. If the second satellite short message is also sent successfully, the terminal The interface shown in Figure 11B will be displayed.
  • the terminal after the terminal sends the first satellite short message, the terminal can also keep the posture of the terminal to adjust the azimuth and pitch angles, and send the second satellite short message to another recipient, as shown in Figure 11C.
  • the recipient "Lucy” sends the second satellite short message. Because the time interval between sending the second satellite short message to the recipient "Lucy” and the last time sending the satellite short message to the recipient "Mary” is very small or the location of the mobile phone has changed very little, so the time interval between sending the second satellite short message to the recipient "Lucy" and There is no need to enter the satellite search guidance interface again when sending the second satellite short message. If the second satellite short message sent to the recipient "Lucy" is also sent successfully, the terminal will display the interface shown in Figure 11D.
  • Figures 11A to 11D all describe the situation in which the satellite short message is successfully sent.
  • the method After sending the first satellite message to the target satellite, the method also includes: receiving a response message that the first satellite message fails to be sent; according to the first satellite message Send a failed response message and display the star search guidance interface.
  • the terminal will display the interface shown in Figure 11E.
  • the terminal can display the star finding guidance interface again to facilitate the user to perform star finding and alignment again.
  • a prompt message "Whether to change a satellite" can also pop up in the terminal's display interface.
  • ordinary messages that have not been successfully sent can also be converted into satellite messages for transmission. This process can be: before displaying the satellite search guidance interface, sending an ordinary message to the base station; receiving a response that the ordinary message fails to be sent. Message; in response to a response message that fails to send an ordinary message, the star finding guidance interface is displayed.
  • the terminal can automatically switch to satellite short message sending, automatically fill in the content of the ordinary short message into the editing area of the satellite short message, and activate the previous embodiment. Describe the star-finding process. It can also be that when the ordinary short message fails to be sent, the user is prompted whether to switch to satellite short message sending. If the user selects "Yes", the user agrees to switch to satellite short message sending, and the terminal automatically fills in the content of the ordinary short message into Editing area for satellite short messages, and start the satellite search process described in the previous embodiment.
  • an embodiment of the message receiving method provided by the embodiment of the present application may include:
  • the terminal displays the star finding guidance interface.
  • the satellite search guidance interface includes a satellite identifier, and the display position of the satellite identifier on the satellite search guidance interface is used to indicate the positional relationship between the terminal and the target satellite.
  • the terminal updates the display position of the satellite logo in response to the user's mobile operation on the terminal.
  • the terminal receives the first satellite message from the target satellite.
  • the terminal can guide the user to adjust the positional relationship between the terminal and the target satellite through the satellite search guidance interface, so that the terminal can quickly establish a communication connection with the satellite, so that the terminal can quickly receive satellite messages.
  • both steps 1201 and 1202 can be understood by referring to the corresponding content of the previous message receiving method. The introduction will not be repeated here. The difference is that step 1203 is to receive the first satellite message from the target satellite, and step 303 is to send the first satellite message to the target satellite.
  • the operation of receiving the satellite short message may be operated in the interface as shown in Figure 13A, such as responding to the user's identification of receiving the satellite short message in Figure 13A.
  • 404 click operation start the loading interface as shown in Figure 5A, or display other star finding guidance interfaces introduced in the process of receiving satellite short messages, and then follow the steps 1 to 10 introduced in the process of receiving satellite short messages or other feasible
  • the solution performs satellite search guidance, allowing the terminal to establish a communication connection with the satellite, and then receive satellite short messages through the satellite.
  • FIG. 13B An interface for the terminal to receive satellite short messages can be understood with reference to Figure 13B. As shown in Figure 13B, the terminal receives the satellite short message "Drive to pick me up at this location" sent by Peter, which also carries location information.
  • messages can be sent or received through satellites, and the terminal can also be aligned with the target satellite, improving the success of message sending. Especially in areas where mobile communication signals are weak or have no mobile communication signal service, the success rate of message sending is improved.
  • the terminal 140 provided by the embodiment of the present application includes:
  • the display unit 1401 is used to display a satellite search guidance interface.
  • the satellite search guidance interface includes a satellite identifier.
  • the display position of the satellite identifier on the satellite search guidance interface is used to indicate the positional relationship between the terminal and the target satellite.
  • the processing unit 1402 is configured to update the display position of the satellite identification displayed by the display unit 1401 in response to the user's movement operation on the terminal.
  • the transceiver unit 1403 is configured to send the first satellite message to the target satellite or receive the first satellite message from the target satellite if the processing unit 1402 responds to the position relationship between the terminal and the target satellite after the user moves and satisfies the message transmission condition.
  • the terminal can guide the user to adjust the positional relationship between the terminal and the target satellite through the satellite search guidance interface, so that the terminal can quickly establish a communication connection with the satellite, so that the terminal can quickly send or receive satellite messages.
  • the star-finding guidance interface also includes star-finding prompt information, and the star-finding prompt information is used to prompt the user in the direction of the mobile terminal.
  • the satellite search guidance interface includes a first satellite search guidance interface and a second satellite search guidance interface; the first satellite search guidance interface includes a first satellite identification and a first alignment area, and the first satellite identification is used to instruct the terminal and The positional relationship of the target satellite in the azimuth angle.
  • the first satellite identification is located in the first alignment area;
  • the second satellite search guidance interface includes the second satellite identification and the second alignment area, the second satellite mark The identification is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle.
  • the second satellite identifier is located in the second alignment area.
  • the display unit 1401 is specifically used to display the first star finding guidance interface.
  • the processing unit 1402 is specifically configured to update the display position of the first satellite logo in response to the user's leftward movement operation or rightward movement operation on the terminal.
  • the display unit 1401 is specifically configured to display the second satellite search guidance interface when the first satellite identifier is located in the first alignment area.
  • the processing unit 1402 is specifically configured to update the display position of the second satellite logo in response to the user's upward movement operation or downward movement operation on the terminal.
  • the display unit 1401 is specifically used to display the second star finding guidance interface.
  • the processing unit 1402 is specifically configured to update the display position of the second satellite logo in response to the user's upward movement operation or downward movement operation on the terminal.
  • the display unit 1401 is specifically configured to display the first satellite search guidance interface when the second satellite identifier is located in the second alignment area.
  • the processing unit 1402 is specifically configured to update the display position of the first satellite logo in response to the user's leftward or rightward movement operation of the terminal.
  • the star search guidance interface includes a first satellite identification and a first alignment area, a second satellite identification and a second alignment area;
  • the first satellite identification is used to indicate the positional relationship between the terminal and the target satellite in azimuth, When the positional relationship between the terminal and the target satellite in the azimuth angle meets the message transmission conditions, the first satellite identification is located in the first alignment area;
  • the second satellite identification is used to indicate the positional relationship between the terminal and the target satellite in the pitch angle.
  • the second satellite identifier is located in the second alignment area.
  • the processing unit 1402 is specifically configured to update the display position of the first satellite logo in response to the user's leftward movement operation or rightward movement operation on the terminal; in response to the user's upward movement operation or downward movement operation on the terminal , update the display position of the second satellite logo.
  • the first alignment area is displayed in the first color; when the display position of the first satellite logo is within the first alignment area, the first alignment area is displayed in the first alignment area.
  • An aligned area is displayed in a second color, the first color being different from the second color.
  • the second alignment area is displayed in a third color; when the display position of the second satellite logo is within the second alignment area, the second alignment area is displayed in the third color.
  • the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
  • the display unit 1401 is also configured to display a satellite message editing interface in response to the user's operation of creating a new satellite message or the operation of replying to a satellite message before displaying the satellite search guidance interface when the terminal is used to send the first satellite message.
  • the satellite message editing interface is used for the user to input the content of the first satellite message.
  • the display unit 1401 is specifically configured to display a star finding guidance interface in response to the user's operation of sending the first satellite message.
  • the display unit 1401 is specifically configured to display a star finding guidance interface in response to the user's operation of receiving satellite messages.
  • the transceiver unit 1403 is also configured to send an ordinary message to the base station; and receive a response message indicating that the ordinary message has failed to be sent.
  • the display unit 1401 is specifically configured to display a star finding guidance interface in response to a response message indicating that the ordinary message fails to be sent.
  • the processing unit 1402 is also configured to determine the location change after the terminal sends the first satellite message in response to the user's sending operation of the second satellite message.
  • the transceiver unit 1403 is also configured to send a second satellite message to the target satellite without displaying the satellite search guidance interface if the position change after the terminal sends the first satellite message is less than the first threshold.
  • the transceiver unit 1403 is also configured to receive a response message indicating that the first satellite message fails to be sent.
  • the display unit 1401 is also configured to display a satellite search guidance interface according to the response message indicating that the first satellite message fails to be sent.
  • each unit in the terminal is similar to those described in the aforementioned embodiments shown in FIGS. 3 to 13B and will not be described again here.
  • a computer-readable storage medium is also provided.
  • Computer-executable instructions are stored in the computer-readable storage medium.
  • the processor of the terminal executes the computer-executed instructions
  • the terminal executes the above-mentioned Figure 3 to Steps performed by the terminal device in Figure 13B.
  • a computer program product is also provided.
  • the computer program product includes a computer program code.
  • the computer program code is executed on a computer, the computer device executes what the terminal in FIGS. 3 to 13B above executes. A step of.
  • a chip system in another embodiment, is also provided.
  • the chip system includes one or more interface circuits and one or more processors; the interface circuits and the processors are interconnected through lines; the interface circuit is used to slave the terminal.
  • the memory receives the signal and sends the signal to the processor, and the signal includes the computer instructions stored in the memory; when the processor executes the computer instructions, the terminal performs the aforementioned steps performed by the terminal device in Figure 3 to Figure 13B.
  • the chip system may also include a memory for storing necessary program instructions and data for controlling the device.
  • the chip system may be composed of chips, or may include chips and other discrete devices.
  • the disclosed systems, devices and methods can be implemented in other ways.
  • the device embodiments described above are only illustrative.
  • the division of units is only a logical function division. In actual implementation, there may be other division methods.
  • multiple units or components may be combined or integrated. to another system, or some features can be ignored, or not implemented.
  • the coupling or direct coupling or communication connection between each other shown or discussed may be through some interfaces, and the indirect coupling or communication connection of the devices or units may be in electrical, mechanical or other forms.
  • the units described as separate components may or may not be physically separated, and the components shown as units may or may not be physical units, that is, they may be located in one place, or they may be distributed to multiple network units. Some or all of the units can be selected according to actual needs to achieve the purpose of the solution of this embodiment.
  • each functional unit in each embodiment of the present application can be integrated into one processing unit, each unit can exist physically alone, or two or more units can be integrated into one unit.
  • the above-mentioned integrated units can be implemented in whole or in part through software, hardware, firmware, or any combination thereof.
  • the integrated unit When the integrated unit is implemented using software, it may be implemented in whole or in part in the form of a computer program product.
  • the computer program product includes one or more computer instructions. Load and execute said computer program on a computer When instructions are given, the processes or functions described in the embodiments of this application are produced in whole or in part.
  • the computer may be a general-purpose computer, a special-purpose computer, a computer network, or other programmable device.
  • the computer instructions may be stored in or transmitted from one computer-readable storage medium to another, e.g., the computer instructions may be transferred from a website, computer, server, or data center Transmission to another website, computer, server or data center through wired (such as coaxial cable, optical fiber, digital subscriber line (DSL)) or wireless (such as infrared, wireless, microwave, etc.) means.
  • the computer-readable storage medium may be any available medium that can be accessed by a computer or a data storage device such as a server, data center, etc. that contains one or more available media integrated.
  • the available media may be magnetic media (eg, floppy disk, hard disk, magnetic tape), optical media (eg, DVD), or semiconductor media (eg, solid state disk (SSD)), etc.

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Abstract

本申请公开了一种消息传输的方法，应用于终端。该方法包括：终端可以显示寻星引导界面，该寻星引导界面包括卫星标识，该卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系，该终端可以响应用户对终端的移动操作，更新卫星标识的显示位置，若移动后的终端与目标卫星的位置关系满足消息传输条件，则终端向目标卫星发送卫星消息或者从目标卫星接收卫星消息。本申请提供的方案可以通过寻星引导界面引导用户调整终端与目标卫星之间的位置，进而可以使终端快速进行卫星消息的发送或接收。

Description

一种消息传输的方法及相应终端
本申请要求于2022年03月18日提交中国专利局、申请号为202210270407.0、发明名称为“一种消息传输的方法及相应终端”的中国专利申请的优先权，其全部内容通过引用结合在本申请中。
技术领域
本申请涉及通信技术领域，具体涉及一种消息传输的方法及相应终端。
背景技术
短消息(short message)是终端(如：手机)通信的一种基础业务，通常一个发送终端可以通过接入网络设备(如：第一基站)发送短消息，该短消息经过网络转发到接收终端所接入的接入网络设备(如：第二基站)，然后通过第二基站将该短消息发送给接收终端。
发明内容
本申请提供一种消息传输的方法，用于通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，进而可以使终端快速进行卫星消息的发送或接收。本申请还提供了相应的终端、计算机可读存储介质以及计算机程序产品等。
本申请第一方面提供一种消息传输的方法，应用于终端，包括：显示寻星引导界面，该寻星引导界面包括卫星标识，卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系；响应于用户对终端的移动操作，更新卫星标识的显示位置；若移动后的终端与目标卫星的位置关系满足消息传输条件，则向目标卫星发送第一卫星消息或从目标卫星接收第一卫星消息。
本申请中，寻星引导界面用于引导用户调整终端的位置。用户可以通过卫星标识在寻星引导界面中的显示位置来确定终端与目标卫星的位置关系，进而移动终端(如：向左或向右移动终端，向上或向下移动终端)，终端会响应该移动，调整卫星标识在寻星引导界面上的显示位置。
本申请中，移动后的终端与目标卫星的位置关系满足消息传输条件可以是移动后的终端与目标卫星的位置关系可以使终端与目标卫星建立通信连接。
本申请中，卫星消息指的是终端直接向卫星发送的消息，或者卫星直接发送给终端的消息,不需要经过基站转发。
上述第一方面中，终端可以通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，使终端可以快速与卫星建立通信连接，从而可以使终端快速进行卫星消息的发送或接收。
在第一方面的一种可能的实现方式中，寻星引导界面还包括寻星提示信息，寻星提示信息用于提示用户移动终端的方向。
该种可能的实现方式中，寻星提示信息用于提示用户移动终端的方向。如:寻星提示信息为向左移动终端、向右移动终端、向上移动终端或向下移动终端。该寻星提示信息通常 是终端按照最短移动路径给出的提示，这样，用户按照寻星提示信息移动终端，可以快速的将终端移动到适合与目标卫星建立通信连接的位置，进而加快了终端向目标卫星发送卫星消息或接收卫星消息的速度。
在第一方面的一种可能的实现方式中，寻星引导界面包括第一寻星引导界面和第二寻星引导界面。第一寻星引导界面包括第一卫星标识和第一对准区域，第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域。第二寻星引导界面包括第二卫星标识和第二对准区域，第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
该种可能的实现方式中，从终端与目标卫星的方位角和俯仰角两个维度设置了卫星标识和对准区域，这样在调整终端的位置时，就可以分别根据第一寻星引导界面和第二寻星引导界面上的卫星标识和对准区域调整方位角上和俯仰角上终端与目标卫星的位置关系，从而可以加快终端与目标卫星建立通信连接的速度。
在第一方面的一种可能的实现方式中，上述步骤：显示寻星引导界面；以及，响应于用户对终端的移动操作，更新卫星标识的显示位置，具体包括：显示第一寻星引导界面，响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；当第一卫星标识位于第一对准区域时，显示第二寻星引导界面；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
该种可能的实现方式中，按照终端显示的先后顺序，会先显示第一寻星引导界面，当第一卫星标识位于第一对准区域时，也就是在方位角上终端与目标卫星对准后，再显示第二寻星引导界面，该第二寻星引导界面可以不包括第一卫星标识和第一对准区域，也可以包括第一卫星标识和第一对准区域。由该种实现方式可知，针对寻星引导界面，本申请提供了多样化的呈现方式。
在第一方面的一种可能的实现方式中，上述步骤：显示寻星引导界面；以及，响应于用户对终端的移动操作，更新卫星标识的显示位置，具体包括：显示第二寻星引导界面，响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置；当第二卫星标识位于第二对准区域时，显示第一寻星引导界面；响应于用户对终端的向左移动或向右移动操作，更新第一卫星标识的显示位置。
该种可能的实现方式中，按照终端显示的先后顺序，会先显示第二寻星引导界面，当第二卫星标识位于第二对准区域时，也就是在俯仰角上终端与目标卫星对准后，再显示第一寻星引导界面，该第一寻星引导界面可以不包括第二卫星标识和第二对准区域，也可以包括第二卫星标识和第二对准区域。由该种实现方式可知，针对寻星引导界面，本申请提供了多样化的呈现方式。
在第一方面的一种可能的实现方式中，寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域；第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终 端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
该种可能的实现方式中，从终端与目标卫星的方位角和俯仰角两个维度设置了卫星标识和对准区域，这样在调整终端的位置时，就可以分别根据寻星引导界面上的卫星标识和对准区域调整方位角上和俯仰角上终端与目标卫星的位置关系，从而可以加快终端与目标卫星建立通信连接的速度。
在第一方面的一种可能的实现方式中，上述步骤：响应于用户对终端的移动操作，更新卫星标识的显示位置，具体包括：响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
该种可能的实现方式中，寻星引导界面上包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域时，用户可以先向左或向右移动终端，先调整终端与目标卫星在方向角上的位置关系，再先向上或向下移动终端，调整终端与目标卫星在俯仰角上的位置关系。也可以是先向上或向下移动终端，先调整终端与目标卫星在俯仰角上的位置关系，再先向左或向右移动终端，调整终端与目标卫星在方位角上的位置关系。还可以是，用户同时调整方位角和俯仰角上的位置关系，如：向左上移动终端或者向左下移动终端，或者向右上移动终端或者向右下移动终端。用户可以根据终端上显示的寻星提示信息的指引移动终端。由该种实现方式可知，针对寻星引导界面，本申请提供了多样化的呈现方式。
在第一方面的一种可能的实现方式中，第一卫星标识的显示位置位于第一对准区域之外时，第一对准区域以第一颜色显示；第一卫星标识的显示位置位于第一对准区域之内时，第一对准区域以第二颜色显示，第一颜色与第二颜色不同。
该种可能的实现方式中，可以通过颜色变化来表示方位角上终端与目标卫星的位置已经调整好，这样可以更好的提示用户在向左或向右的方向上终端已经移动到合适的位置。
在第一方面的一种可能的实现方式中，第二卫星标识的显示位置位于第二对准区域之外时，第二对准区域以第三颜色显示；第二卫星标识的显示位置位于第二对准区域之内时，第二对准区域以第四颜色显示，第三颜色与第四颜色不同。
该种可能的实现方式中，可以通过颜色变化来表示俯仰角上终端与目标卫星的位置已经调整好，这样可以更好的提示用户在向上或向下的方向上终端已经移动到合适的位置。
在第一方面的一种可能的实现方式中，当终端用于发送第一卫星消息时，在显示寻星引导界面之前，该方法还包括：响应于用户新建卫星消息的操作或者回复卫星消息的操作，显示卫星消息编辑界面，卫星消息编辑界面用于用户输入第一卫星消息的内容。
该种可能的实现方式中，终端上可以在短消息应用或者其他通信应用上配置卫星消息的功能，进而进行卫星消息的发送。
在第一方面的一种可能的实现方式中，上述步骤：显示寻星引导界面，具体包括：响应于用户对第一卫星消息的发送操作，显示寻星引导界面。
该种可能的实现方式中，终端响应于用户对第一卫星消息的发送操作，显示寻星引导界面，供用户进行前面所介绍的多种实现方式中的寻星引导过程。
在第一方面的一种可能的实现方式中，当终端用于接收第一卫星消息时，上述步骤：显示寻星引导界面，具体包括：响应于用户接收卫星消息的操作，显示寻星引导界面。
该种可能的实现方式中，接收卫星消息时，终端响应于用户接收卫星消息的操作，显示寻星引导界面，供用户进行前面所介绍的多种实现方式中的寻星引导过程。
在第一方面的一种可能的实现方式中，当终端用于发送第一卫星消息时，在显示寻星引导界面之前，该方法还包括：向基站发送普通消息；接收到普通消息发送失败的响应消息；上述步骤：显示寻星引导界面，具体包括：响应于普通消息发送失败的响应消息，显示寻星引导界面。
该种可能的实现方式中，普通消息指的是通过基站发送的消息。普通消息发送失败后，可以将普通消息的内容转移到卫星消息编辑界面，通过卫星消息发送该普通消息的内容。这样，可以提高消息发送的成功率。
在第一方面的一种可能的实现方式中，在发送第一卫星消息之后，该方法还包括：响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息之后的位置变化；若终端发送第一卫星消息之后的位置变化小于第一阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
该种可能的实现方式中，第一阈值可以是预先配置好的，发送第一卫星消息时，用户调整了终端与目标卫星的位置关系，建立了终端与目标卫星的通信连接，用户可以保持在该位置，向同一收件人或者不同收件人发送第二卫星消息，不需要再显示寻星引导界面，这样，可以提高卫星消息发送的速度。
另外，作为一种可能的实现方式，在发送第一卫星消息之后，该方法还包括：响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息时的时间；若终端发送第一卫星消息时的时间距离用户触发第二卫星消息的发送操作之间的时间差小于第二阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
在第一方面的一种可能的实现方式中，在向目标卫星发送第一卫星消息之后，该方法还包括：接收到第一卫星消息发送失败的响应消息；根据第一卫星消息发送失败的响应消息，显示寻星引导界面。
该种可能的实现方式中，如果第一卫星消息发送失败，则表示终端与目标卫星之间的通信连接断开或者信号较差，需要再次调整终端与目标卫星之间的位置关系。
本申请第二方面提供一种终端，包括：
显示单元，用于显示寻星引导界面，寻星引导界面包括卫星标识，卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系。
处理单元，用于响应于用户对终端的移动操作，更新显示单元显示的卫星标识的显示位置。
收发单元，用于若移动后的终端与目标卫星的位置关系满足消息传输条件，则向目标卫星发送第一卫星消息或从目标卫星接收第一卫星消息。
在第二方面的一种可能的实现方式中，寻星引导界面还包括寻星提示信息，寻星提示信息用于提示用户移动终端的方向。
在第二方面的一种可能的实现方式中，寻星引导界面包括第一寻星引导界面和第二寻星引导界面；第一寻星引导界面包括第一卫星标识和第一对准区域，第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二寻星引导界面包括第二卫星标识和第二对准区域，第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
在第二方面的一种可能的实现方式中，显示单元，具体用于显示第一寻星引导界面。
处理单元，具体用于响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置。
显示单元，具体用于当第一卫星标识位于第一对准区域时，显示第二寻星引导界面。
处理单元，具体用于响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
在第二方面的一种可能的实现方式中，显示单元，具体用于显示第二寻星引导界面。
处理单元，具体用于响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
显示单元，具体用于当第二卫星标识位于第二对准区域时，显示第一寻星引导界面。
处理单元，具体用于响应于用户对终端的向左移动或向右移动操作，更新第一卫星标识的显示位置。
在第二方面的一种可能的实现方式中，寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域；第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
在第二方面的一种可能的实现方式中，处理单元，具体用于响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
在第二方面的一种可能的实现方式中，第一卫星标识的显示位置位于第一对准区域之外时，第一对准区域以第一颜色显示；第一卫星标识的显示位置位于第一对准区域之内时，第一对准区域以第二颜色显示，第一颜色与第二颜色不同。
在第二方面的一种可能的实现方式中，第二卫星标识的显示位置位于第二对准区域之外时，第二对准区域以第三颜色显示；第二卫星标识的显示位置位于第二对准区域之内时，第二对准区域以第四颜色显示，第三颜色与第四颜色不同。
在第二方面的一种可能的实现方式中，显示单元，还用于当终端用于发送第一卫星消息时，在显示寻星引导界面之前，响应于用户新建卫星消息的操作或者回复卫星消息的操作，显示卫星消息编辑界面，卫星消息编辑界面用于用户输入第一卫星消息的内容。
在第二方面的一种可能的实现方式中，显示单元，具体用于响应于用户对第一卫星消 息的发送操作，显示寻星引导界面。
在第二方面的一种可能的实现方式中，显示单元，具体用于响应于用户接收卫星消息的操作，显示寻星引导界面。
在第二方面的一种可能的实现方式中，收发单元，还用于向基站发送普通消息；以及接收到普通消息发送失败的响应消息。
显示单元，具体用于响应于普通消息发送失败的响应消息，显示寻星引导界面。
在第二方面的一种可能的实现方式中，处理单元，还用于响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息之后的位置变化。
收发单元，还用于若终端发送第一卫星消息之后的位置变化小于第一阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
在第二方面的一种可能的实现方式中，收发单元，还用于接收到第一卫星消息发送失败的响应消息。
显示单元，还用于根据第一卫星消息发送失败的响应消息，显示寻星引导界面。
本申请第三方面提供了一种终端，该终端用于执行前述第一方面或第一方面的任意可能的实现方式中的方法。
本申请第四方面提供了一种芯片系统，该芯片系统包括一个或多个接口电路和一个或多个处理器；接口电路和处理器通过线路互联；接口电路用于从终端的存储器接收信号，并向处理器发送信号，信号包括存储器中存储的计算机指令；当处理器执行计算机指令时，终端执行前述第一方面或第一方面的任意可能的实现方式中的方法。
本申请第五方面提供了一种计算机可读存储介质，其上存储有计算机程序或指令，当计算机程序或指令在计算机上运行时，使得计算机执行前述第一方面或第一方面的任意可能的实现方式中的方法。
本申请第六方面提供了一种计算机程序产品，该计算机程序产品包括计算机程序代码，当计算机程序代码在计算机上执行时，使得计算机执行前述第一方面或第一方面的任意可能的实现方式中的方法。
其中，第二、第三、第四、第五、第六方面或者其中任一种可能实现方式所带来的技术效果可参见第一方面或第一方面不同可能实现方式所带来的技术效果，此处不再赘述。
附图说明
图1A是本申请实施例提供的应用场景的一示意图；
图1B是本申请实施例提供的应用场景的另一示意图；
图1C是本申请实施例提供的应用场景的另一示意图；
图1D是本申请实施例提供的应用场景的另一示意图；
图1E是本申请实施例提供的应用场景的另一示意图；
图2是本申请实施例提供的终端的结构示意图；
图3是本申请实施例提供的消息发送的方法的一实施例示意图；
图4A是本申请实施例提供的一界面示意图；
图4B是本申请实施例提供的信息的一界面示意图；
图4C是本申请实施例提供的卫星短消息的一界面示意图；
图4D是本申请实施例提供的新建卫星短消息的一界面示意图；
图5A是本申请实施例提供的寻星引导的一加载界面示意图；
图5B是本申请实施例提供的三维坐标系示意图；
图5C至图5F是本申请实施例提供的寻星引导界面的多个示意图；
图6A至图6D是本申请实施例提供的寻星引导界面的多个示意图；
图7A至图7C是本申请实施例提供的寻星引导界面的多个示意图；
图8A至图8C是本申请实施例提供的寻星引导界面的多个示意图；
图9是本申请实施例提供的寻星引导界面的另一示意图；
图10A至图10D是本申请实施例提供的寻星引导界面的多个示意图；
图11A是本申请实施例提供的卫星消息编辑界面的一示意图；
图11B是本申请实施例提供的卫星消息编辑界面的另一示意图；
图11C是本申请实施例提供的卫星消息编辑界面的另一示意图；
图11D是本申请实施例提供的卫星消息编辑界面的另一示意图；
图11E是本申请实施例提供的卫星消息编辑界面的另一示意图；
图12是本申请实施例提供的消息接收的方法的一实施例示意图；
图13A是本申请实施例提供的卫星短消息的另一界面示意图；
图13B是本申请实施例提供的卫星短消息的另一界面示意图；
图14是本申请实施例提供的终端的另一结构示意图。
具体实施方式
下面结合附图，对本申请的实施例进行描述，显然，所描述的实施例仅仅是本申请一部分的实施例，而不是全部的实施例。本领域普通技术人员可知，随着技术发展和新场景的出现，本申请实施例提供的技术方案对于类似的技术问题，同样适用。
本申请的说明书和权利要求书及上述附图中的术语“第一”、“第二”等是用于区别类似的对象，而不必用于描述特定的顺序或先后次序。应该理解这样使用的数据在适当情况下可以互换，以便这里描述的实施例能够以除了在这里图示或描述的内容以外的顺序实施。此外，术语“包括”和“具有”以及他们的任何变形，意图在于覆盖不排他的包含，例如，包含了一系列步骤或单元的过程、方法、系统、产品或设备不必限于清楚地列出的那些步骤或单元，而是可包括没有清楚地列出的或对于这些过程、方法、产品或设备固有的其它步骤或单元。
本申请实施例提供一种消息传输的方法，用于通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，进而可以使终端快速进行卫星消息的发送或接收。本申请还提供了相应的终端、计算机可读存储介质以及计算机程序产品等。以下分别进行详细说明。
在对本申请实施例所提供的方法进行描述之前，先对本申请实施例所提供的方法的应用场景进行描述。本申请实施例提供的方法的应用场景可以如图1A至图1E所示。其中，图 1A、图1B和图1C表示发送卫星消息的应用场景，图1C、图1D和图1E表示接收卫星消息的应用场景。
本申请实施例中，卫星消息指的是终端直接向卫星发送的消息，或者，终端直接从卫星接收的消息。若终端与卫星之间还需要通过其他设备(如：基站或云网络)中转的消息称为普通消息。
本申请实施例中，终端的消息应用或者其他通信应用中可以配置有卫星消息功能项，用户可以在终端上通过该卫星消息功能项编辑卫星消息，以及点击发送操作，进而终端向卫星发送该卫星消息。或者，用户可以在终端上通过该卫星消息功能项点击卫星消息的接收操作，进而终端从卫星接收卫星消息。
需要说明的是，消息应用指的是用于发送或接收消息(short message，SM)的应用，其他通信应用可以是即时通信应用或者其他能够接收或发送消息的应用。
如图1A所示的发送卫星消息的应用场景，该应用场景(或架构)可以包括：第一终端、卫星、基站和第二终端。第一终端向卫星发送卫星消息，卫星接收到卫星消息后，将该卫星消息的内容发送给基站，基站将该卫星消息的内容发送给第二终端，第二终端接收到该卫星消息的内容后以普通消息显示。
如图1B所示通发送卫星消息的应用场景。该应用场景(或架构)可以包括：第一终端、卫星、云网络和第二终端，第一终端向卫星发送卫星消息，卫星接收到卫星消息后，将该卫星消息的内容发送给云网络，云网络将该卫星消息的内容发送给第二终端，第二终端通过云网络接收该卫星消息的内容，该卫星消息的内容可以在相应应用(App)的普通消息中显示。
如图1C所示的发送卫星消息以及接收卫星消息的应用场景，该应用场景(或架构)可以包括：第一终端、卫星和第二终端，第一终端向卫星发送卫星消息，卫星接收到卫星消息后，将该卫星消息发送给第二终端，第二终端从卫星接收到卫星消息后，显示该卫星消息。
如图1D所示的接收卫星消息的应用场景，该应用场景(或架构)可以包括：第一终端、基站、卫星和第二终端。第一终端向基站发送普通消息，基站向卫星发送该普通消息，卫星接收到该普通消息后，将该普通消息的内容发送给第二终端，第二终端接收到该普通消息的内容后，在卫星消息功能项中以卫星消息的形式显示该普通消息的内容。
如图1E所示的接收卫星消息。该应用场景(或架构)可以包括：第一终端、卫星、云网络和第二终端，第一终端向云网络发送普通消息，云网络接收到该普通消息后，将该普通消息发送卫星，卫星接收到该普通消息后，将该普通消息的内容发送给第二终端，第二终端接收到该普通消息的内容后，在卫星消息功能项中以卫星消息的形式显示该普通消息的内容。
以上，图1A至图1E中给出的场景中都只示意出了一颗卫星，实际上，上述过程也可以涉及多颗卫星，以两颗卫星为例，其中一颗卫星从第一终端接收到卫星消息后，可以将该卫星消息发送给另一颗卫星，由另一颗卫星将该卫星消息发送给第二终端或者其他设备(如：基站或云网络)。
以上所描述的第一终端和第二终端都可以是手机、平板电脑(pad)、便携式游戏机、掌上电脑(personal digital assistant，PDA)、笔记本电脑、超级移动个人计算机(ultra mobile personal computer，UMPC)、手持计算机、上网本、车载媒体播放设备、可穿戴电子设备、虚拟现实(virtual reality，VR)终端设备、增强现实(augmentedreality，AR)终端设备等数显产品。本申请实施例仅以第一终端和第二终端是手机为例进行描述。
请参考图2，为本申请实施例提供的一种终端的结构示意图。如图2所示，终端可以包括处理器210，外部存储器接口220，内部存储器221，通用串行总线(universal serial bus，USB)接口230，充电管理模块240，电源管理模块241，电池242，天线1，天线2，天线3，移动通信模块250，卫星通信模块251，无线通信模块260，音频模块270，扬声器270A，受话器270B，麦克风270C，耳机接口270D，传感器模块280，按键290，马达291，指示器292，摄像头293，显示屏294，以及用户标识模块(subscriber identification module，SIM)卡接口295等。其中，传感器模块280可以包括压力传感器280A，陀螺仪传感器280B，气压传感器280C，磁传感器280D，加速度传感器280E，距离传感器280F，接近光传感器280G，指纹传感器280H，温度传感器280J，触摸传感器280K，环境光传感器280L，骨传导传感器280M和运动传感器280N等。
可以理解的是，本实施例示意的结构并不构成对终端的具体限定。在另一些实施例中，终端可以包括比图示更多或更少的部件，或者组合某些部件，或者拆分某些部件，或者不同的部件布置。图示的部件可以以硬件，软件或软件和硬件的组合实现。
处理器210可以包括一个或多个处理单元，例如：处理器210可以包括应用处理器(application processor，AP)，调制解调处理器，图形处理器(graphics processing unit，GPU)，图像信号处理器(image signal processor，ISP)，控制器，存储器，视频编解码器，数字信号处理器(digital signal processor，DSP)，基带处理器，和/或神经网络处理器(neural-network processing unit，NPU)等。其中，不同的处理单元可以是独立的器件，也可以集成在一个或多个处理器中。
控制器可以是终端的神经中枢和指挥中心。控制器可以根据指令操作码和时序信号，产生操作控制信号，完成取指令和执行指令的控制。
处理器210中还可以设置存储器，用于存储指令和数据。在一些实施例中，处理器210中的存储器为高速缓冲存储器。该存储器可以保存处理器210刚用过或循环使用的指令或数据。如果处理器210需要再次使用该指令或数据，可从所述存储器中直接调用。避免了重复存取，减少了处理器210的等待时间，因而提高了系统的效率。
在一些实施例中，处理器210可以包括一个或多个接口。接口可以包括集成电路(inter-integrated circuit，I2C)接口，集成电路内置音频(inter-integrated circuit sound，I2S)接口，脉冲编码调制(pulse code modulation，PCM)接口，通用异步收发传输器(universal asynchronous receiver/transmitter，UART)接口，移动产业处理器接口(mobile industry processor interface，MIPI)，通用输入输出(general-purpose input/output，GPIO)接口，用户标识模块(subscriber identity module，SIM)接口，和/或通用串行总线(universal serial bus，USB)接口等。
可以理解的是，本实施例示意的各模块间的接口连接关系，只是示意性说明，并不构成对终端的结构限定。在另一些实施例中，终端也可以采用上述实施例中不同的接口连接方式，或多种接口连接方式的组合。
充电管理模块240用于从充电器接收充电输入。其中，充电器可以是无线充电器，也可以是有线充电器。在一些有线充电的实施例中，充电管理模块240可以通过USB接口230接收有线充电器的充电输入。在一些无线充电的实施例中，充电管理模块240可以通过终端的无线充电线圈接收无线充电输入。充电管理模块240为电池242充电的同时，还可以通过电源管理模块241为终端供电。
电源管理模块241用于连接电池242，充电管理模块240与处理器210。电源管理模块241接收电池242和/或充电管理模块240的输入，为处理器210，内部存储器221，外部存储器，显示屏294，摄像头293，和无线通信模块260等供电。电源管理模块241还可以用于监测电池容量，电池循环次数，电池健康状态(漏电，阻抗)等参数。在其他一些实施例中，电源管理模块241也可以设置于处理器210中。在另一些实施例中，电源管理模块241和充电管理模块240也可以设置于同一个器件中。
终端的无线通信功能可以通过天线1，天线2，天线3，移动通信模块250，卫星通信模块251，无线通信模块260，调制解调处理器以及基带处理器等实现。
天线1、天线2和天线3用于发射和接收电磁波信号。终端中的每个天线可用于覆盖单个或多个通信频带。不同的天线还可以复用，以提高天线的利用率。例如：可以将天线1复用为无线局域网的分集天线。在另外一些实施例中，天线可以和调谐开关结合使用。天线3可以用于向卫星发射信号，和/或从卫星接收信号。
移动通信模块250可以提供应用在终端上的包括2G/3G/4G/5G等无线通信的解决方案。移动通信模块250可以包括至少一个滤波器，开关，功率放大器，低噪声放大器(low noise amplifier，LNA)等。移动通信模块250可以由天线1接收电磁波，并对接收的电磁波进行滤波，放大等处理，传送至调制解调处理器进行解调。移动通信模块250还可以对经调制解调处理器调制后的信号放大，经天线1转为电磁波辐射出去。在一些实施例中，移动通信模块250的至少部分功能模块可以被设置于处理器210中。在一些实施例中，移动通信模块250的至少部分功能模块可以与处理器210的至少部分模块被设置在同一个器件中。
卫星通信模块251可以提供应用在终端上与卫星通信的解决方案。卫星通信模块251可以是集成至少一个通信处理模块的一个或多个器件。卫星通信模块251经由天线3接收电磁波，将电磁波信号调频以及滤波处理，将处理后的信号发送到处理器210。卫星通信模块251还可以从处理器210接收待发送的信号，对其进行调频，放大，经天线3转为电磁波辐射出去。
调制解调处理器可以包括调制器和解调器。其中，调制器用于将待发送的低频基带信号调制成中高频信号。解调器用于将接收的电磁波信号解调为低频基带信号。随后解调器将解调得到的低频基带信号传送至基带处理器处理。低频基带信号经基带处理器处理后，被传递给应用处理器。应用处理器通过音频设备(不限于扬声器270A，受话器270B等)输出声音信号，或通过显示屏294显示图像或视频。在一些实施例中，调制解调处理器可以 是独立的器件。在另一些实施例中，调制解调处理器可以独立于处理器210，与移动通信模块250或其他功能模块设置在同一个器件中。
无线通信模块260可以提供应用在终端上的包括无线局域网(wirelesslocal area networks，WLAN)(如无线保真(wireless fidelity，Wi-Fi)网络)，蓝牙(bluetooth，BT)，全球导航卫星系统(global navigation satellite system，GNSS)，调频(frequency modulation，FM)，近距离无线通信技术(near field communication，NFC)，红外技术(infrared，IR)等无线通信的解决方案。无线通信模块260可以是集成至少一个通信处理模块的一个或多个器件。无线通信模块260经由天线2接收电磁波，将电磁波信号调频以及滤波处理，将处理后的信号发送到处理器210。无线通信模块260还可以从处理器210接收待发送的信号，对其进行调频，放大，经天线2转为电磁波辐射出去。
在一些实施例中，终端的天线1和移动通信模块250耦合，天线2和无线通信模块260耦合，使得终端可以通过无线通信技术与网络以及其他设备通信。所述无线通信技术可以包括全球移动通讯系统(global system for mobile communications，GSM)，通用分组无线服务(general packet radio service，GPRS)，码分多址接入(codedivision multiple access，CDMA)，宽带码分多址(wideband code division multipleaccess，WCDMA)，时分码分多址(time-division code division multiple access，TDSCDMA)，长期演进(long term evolution，LTE)，BT，GNSS，WLAN，NFC，FM，和/或IR技术等。所述GNSS可以包括全球卫星定位系统(global positioning system，GPS)，全球导航卫星系统(global navigation satellite system，GLONASS)，北斗卫星导航系统(beidounavigation satellite system，BDS)，准天顶卫星系统(quasi-zenith satellitesystem，QZSS)和/或星基增强系统(satellite based augmentation systems，SBAS)。
终端通过GPU，显示屏294，以及应用处理器等实现显示功能。GPU为图像处理的微处理器，连接显示屏294和应用处理器。GPU用于执行数学和几何计算，用于图形渲染。处理器210可包括一个或多个GPU，其执行程序指令以生成或改变显示信息。
显示屏294用于显示图像，视频等。该显示屏294包括显示面板。显示面板可以采用液晶显示屏(liquid crystaldisplay，LCD)，有机发光二极管(organic light-emitting diode，OLED)，有源矩阵有机发光二极体或主动矩阵有机发光二极体(active-matrix organic light emitting diode，AMOLED)，柔性发光二极管(flex light-emitting diode，FLED)，Miniled，MicroLed，Micro-oLed，量子点发光二极管(quantum dot light emitting diodes，QLED)等。
终端可以通过ISP，摄像头293，视频编解码器，GPU，显示屏294以及应用处理器等实现拍摄功能。
ISP用于处理摄像头293反馈的数据。例如，拍照时，打开快门，光线通过镜头被传递到摄像头感光元件上，光信号转换为电信号，摄像头感光元件将所述电信号传递给ISP处理，转化为肉眼可见的图像。ISP还可以对图像的噪点，亮度，肤色进行算法优化。ISP还可以对拍摄场景的曝光，色温等参数优化。在一些实施例中，ISP可以设置在摄像头293中。
摄像头293用于捕获静态图像或视频。物体通过镜头生成光学图像投射到感光元件。感光元件可以是电荷耦合器件(charge coupled device，CCD)或互补金属氧化物半导体(complementary metal-oxide-semiconductor，CMOS)光电晶体管。感光元件把光信号转换成电信号，之后将电信号传递给ISP转换成数字图像信号。ISP将数字图像信号输出到DSP加工处理。DSP将数字图像信号转换成标准的RGB，YUV等格式的图像信号。在一些实施例中，终端可以包括1个或N个摄像头293，N为大于1的正整数。
摄像头293还可以用于根据感知到的外部的环境和用户的动作，终端向用户提供个性化的、情景化的业务体验。其中，摄像头293能够获取丰富、准确的信息使得终端感知外部的环境、用户的动作。具体的，本申请实施例中，摄像头293可以用于识别终端的使用者是第一用户还是第二用户。
数字信号处理器用于处理数字信号，除了可以处理数字图像信号，还可以处理其他数字信号。例如，当终端在频点选择时，数字信号处理器用于对频点能量进行傅里叶变换等。
视频编解码器用于对数字视频压缩或解压缩。终端可以支持一种或多种视频编解码器。这样，终端可以播放或录制多种编码格式的视频，例如：动态图像专家组(moving picture experts group，MPEG)1，MPEG2，MPEG3，MPEG4等。
NPU为神经网络(neural-network，NN)计算处理器，通过借鉴生物神经网络结构，例如借鉴人脑神经元之间传递模式，对输入信息快速处理，还可以不断的自学习。通过NPU可以实现终端的智能认知等应用，例如：图像识别，人脸识别，语音识别，文本理解等。
外部存储器接口220可以用于连接外部存储卡，例如Micro SD卡，实现扩展终端的存储能力。外部存储卡通过外部存储器接口220与处理器210通信，实现数据存储功能。例如将音乐，视频等文件保存在外部存储卡中。
内部存储器221可以用于存储计算机可执行程序代码，所述可执行程序代码包括指令。处理器210通过运行存储在内部存储器221的指令，从而执行终端的各种功能应用以及数据处理。例如，在本申请实施例中，处理器210可以通过执行存储在内部存储器221中的指令，响应于用户在显示屏294的操作，在显示屏显示对应的显示内容。内部存储器221可以包括存储程序区和存储数据区。其中，存储程序区可存储操作系统，至少一个功能所需的应用程序(比如声音播放功能，图像播放功能等)等。存储数据区可存储终端使用过程中所创建的数据(比如音频数据，电话本等)等。此外，内部存储器221可以包括高速随机存取存储器，还可以包括非易失性存储器，例如至少一个磁盘存储器件，闪存器件，通用闪存存储器(universalflashstorage，UFS)等。
终端可以通过音频模块270，扬声器270A，受话器270B，麦克风270C，耳机接口270D，以及应用处理器等实现音频功能。例如音乐播放，录音等。
音频模块270用于将数字音频信息转换成模拟音频信号输出，也用于将模拟音频输入转换为数字音频信号。音频模块270还可以用于对音频信号编码和解码。在一些实施例中，音频模块270可以设置于处理器210中，或将音频模块270的部分功能模块设置于处理器210中。扬声器270A，也称“喇叭”，用于将音频电信号转换为声音信号。终端可以通过扬声器270A收听音乐，或收听免提通话。受话器270B，也称“听筒”，用于将音频电信号转 换成声音信号。当终端接听电话或语音信息时，可以通过将受话器270B靠近人耳接听语音。麦克风270C，也称“话筒”，“传声器”，用于将声音信号转换为电信号。当拨打电话或发送语音信息或需要通过语音助手触发终端执行某些功能时，用户可以通过人嘴靠近麦克风270C发声，将声音信号输入到麦克风270C。终端可以设置至少一个麦克风270C。在另一些实施例中，终端可以设置两个麦克风270C，除了采集声音信号，还可以实现降噪功能。在另一些实施例中，终端还可以设置三个，四个或更多麦克风270C，实现采集声音信号，降噪，还可以识别声音来源，实现定向录音功能等。
耳机接口270D用于连接有线耳机。耳机接口270D可以是USB接口230，也可以是3.5mm的开放移动终端平台(open mobile terminal platform，OMTP)标准接口，美国蜂窝电信工业协会(cellular telecommunications industry association of the USA，CTIA)标准接口。
压力传感器280A用于感受压力信号，可以将压力信号转换成电信号。在一些实施例中，压力传感器280A可以设置于显示屏294。压力传感器280A的种类很多，如电阻式压力传感器，电感式压力传感器，电容式压力传感器等。电容式压力传感器可以是包括至少两个具有导电材料的平行板。当有力作用于压力传感器280A，电极之间的电容改变。终端根据电容的变化确定压力的强度。当有触摸操作作用于显示屏294，终端根据压力传感器280A检测所述触摸操作强度。终端也可以根据压力传感器280A的检测信号计算触摸的位置。在一些实施例中，作用于相同触摸位置，但不同触摸操作强度的触摸操作，可以对应不同的操作指令。例如：当有触摸操作强度小于压力阈值的触摸操作作用于短消息应用图标时，执行查看短消息的指令。当有触摸操作强度大于或等于压力阈值的触摸操作作用于短消息应用图标时，执行新建短消息的指令。
陀螺仪传感器280B可以用于确定终端的运动姿态。在一些实施例中，可以通过陀螺仪传感器280B确定终端围绕三个轴(即，x，y和z轴)的角速度。陀螺仪传感器280B可以用于拍摄防抖。示例性的，当按下快门，陀螺仪传感器280B检测终端抖动的角度，根据角度计算出镜头模组需要补偿的距离，让镜头通过反向运动抵消终端的抖动，实现防抖。陀螺仪传感器280B还可以用于导航，体感游戏场景。另外，陀螺仪传感器280B，还可以用于测量终端的旋转幅度或移动距离。
气压传感器280C用于测量气压。在一些实施例中，终端通过气压传感器280C测得的气压值计算海拔高度，辅助定位和导航。
磁传感器280D包括霍尔传感器。终端可以利用磁传感器280D检测翻盖皮套的开合。在一些实施例中，当终端是翻盖机时，终端可以根据磁传感器280D检测翻盖的开合。进而根据检测到的皮套的开合状态或翻盖的开合状态，设置翻盖自动解锁等特性。
加速度传感器280E可检测终端在各个方向上(一般为三轴)加速度的大小。当终端静止时可检测出重力的大小及方向。还可以用于识别终端姿态，应用于横竖屏切换，计步器等应用。另外，加速度传感器280E，还可以用于测量终端的朝向(即朝向的方向向量)。
距离传感器280F，用于测量距离。终端可以通过红外或激光测量距离。在一些实施例中，拍摄场景，终端可以利用距离传感器280F测距以实现快速对焦。
接近光传感器280G可以包括例如发光二极管(LED)和光检测器，例如光电二极管。发光二极管可以是红外发光二极管。终端通过发光二极管向外发射红外光。终端使用光电二极管检测来自附近物体的红外反射光。当检测到充分的反射光时，可以确定终端附近有物体。当检测到不充分的反射光时，终端可以确定终端附近没有物体。终端可以利用接近光传感器280G检测用户手持终端贴近耳朵通话，以便自动熄灭屏幕达到省电的目的。接近光传感器280G也可用于皮套模式，口袋模式自动解锁与锁屏。
环境光传感器280L用于感知环境光亮度。终端可以根据感知的环境光亮度自适应调节显示屏294亮度。环境光传感器280L也可用于拍照时自动调节白平衡。环境光传感器280L还可以与接近光传感器280G配合，检测终端是否在口袋里，以防误触。
指纹传感器280H用于采集指纹。终端可以利用采集的指纹特性实现指纹解锁，访问应用锁，指纹拍照，指纹接听来电等。
温度传感器280J用于检测温度。在一些实施例中，终端利用温度传感器280J检测的温度，执行温度处理策略。例如，当温度传感器280J上报的温度超过阈值，终端执行降低位于温度传感器280J附近的处理器的性能，以便降低功耗实施热保护。在另一些实施例中，当温度低于另一阈值时，终端对电池242加热，以避免低温导致终端异常关机。在其他一些实施例中，当温度低于又一阈值时，终端对电池242的输出电压执行升压，以避免低温导致的异常关机。
触摸传感器280K，也称“触控面板”。触摸传感器280K可以设置于显示屏294，由触摸传感器280K与显示屏294组成触摸屏，也称“触控屏”。触摸传感器280K用于检测作用于其上或附近的触摸操作。触摸传感器可以将检测到的触摸操作传递给应用处理器，以确定触摸事件类型。可以通过显示屏294提供与触摸操作相关的视觉输出。在另一些实施例中，触摸传感器280K也可以设置于终端的表面，与显示屏294所处的位置不同。
骨传导传感器280M可以获取振动信号。在一些实施例中，骨传导传感器280M可以获取人体声部振动骨块的振动信号。骨传导传感器280M也可以接触人体脉搏，接收血压跳动信号。在一些实施例中，骨传导传感器280M也可以设置于耳机中，结合成骨传导耳机。音频模块270可以基于所述骨传导传感器280M获取的声部振动骨块的振动信号，解析出语音信号，实现语音功能。应用处理器可以基于所述骨传导传感器280M获取的血压跳动信号解析心率信息，实现心率检测功能。
运动传感器280N可以获取运动数据。
按键290包括开机键，音量键等。按键290可以是机械按键。也可以是触摸式按键。终端可以接收按键输入，产生与终端的用户设置以及功能控制有关的键信号输入。
其中，终端通过传感器模块280中的各类传感器、按键290、和/或摄像头293等识别本申请实施例中所提的操作(包括第一操作、第二操作、第三操作等)。
马达291可以产生振动提示。马达291可以用于来电振动提示，也可以用于触摸振动反馈。例如，作用于不同应用(例如拍照，音频播放等)的触摸操作，可以对应不同的振动反馈效果。作用于显示屏294不同区域的触摸操作，马达291也可对应不同的振动反馈效果。不同的应用场景(例如：时间提醒，接收信息，闹钟，游戏等)也可以对应不同的振动 反馈效果。触摸振动反馈效果还可以支持自定义。
指示器292可以是指示灯，可以用于指示充电状态，电量变化，也可以用于指示消息，未接来电，通知等。
SIM卡接口295用于连接SIM卡。SIM卡可以通过插入SIM卡接口295，或从SIM卡接口295拔出，实现和终端的接触和分离。终端可以支持1个或N个SIM卡接口，N为大于1的正整数。SIM卡接口295可以支持Nano SIM卡，Micro SIM卡，SIM卡等。同一个SIM卡接口295可以同时插入多张卡。所述多张卡的类型可以相同，也可以不同。SIM卡接口295也可以兼容不同类型的SIM卡。SIM卡接口295也可以兼容外部存储卡。终端通过SIM卡和网络交互，实现通话以及数据通信等功能。在一些实施例中，终端采用eSIM，即：嵌入式SIM卡。eSIM卡可以嵌在终端中，不能和终端分离。
下面将以下终端是手机为例对本申请实施例提供的终端的卫星短消息的发送方法以及接收方法进行描述。该方法可以由终端执行，也可以由终端的部件(例如处理器、芯片、或芯片系统等)执行。
本申请实施例提供的消息传输的方法可以应用于前面所介绍的终端，该消息传输的方法可以包括消息发送的方法和消息接收的方法，下面分别进行介绍。
如图3所示，本申请实施例提供的消息发送的方法的一实施例可以包括：
301.终端显示寻星引导界面。
该寻星引导界面包括卫星标识，卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系。
本申请实施例中，可以是终端响应于用户新建卫星消息的操作或者回复卫星消息的操作，显示卫星消息编辑界面，卫星消息编辑界面用于用户输入第一卫星消息的内容。然后，终端可以响应于用户对第一卫星消息的发送操作，显示寻星引导界面。
本申请实施例中，与卫星消息相关的操作(如：新建卫星消息的操作或者回复卫星消息的操作)可以是在卫星消息功能项中完成的，卫星消息功能项可以设置于信息应用中，如：短消息应用或者其他通信应用。当然，也可以为卫星消息设计一个卫星消息应用来实现该卫星消息功能项的功能。如果该卫星消息功能项设置于短消息应用中，则该短消息应用具有普通短消息的功能+卫星短消息的功能。如果该卫星消息功能项设置于即时通信应用中，则该即时通信应用具有即时通信功能+卫星消息的功能。如果为卫星消息设计了卫星消息应用，则该卫星消息应用至少具有卫星消息的功能。
用户通常在信号不好或者移动通信无服务的情况下可以使用卫星消息的功能。本申请实施例中以设置在短消息应用为例进行说明，在短消息应用中涉及到的卫星消息可以称为卫星短消息。
以短消息应用为例，如图4A所示，终端响应于用户在手机主界面上对信息应用(短消息应用)401的点击操作，显示如图4B所示的信息界面。该信息界面中包括卫星短消息功能项402。终端响应于用户在图4B所示的信息界面上对卫星短消息功能项402的点击操作，显示如图4C所示的卫星短消息界面。该卫星短消息界面上包括“新建卫星短消息”的标识403，还可以包括“接收卫星短消息”的标识404。用户可以通过“新建卫星短消息”的标 识403进入新建卫星短消息的界面，可以通过“接收卫星短消息”的标识404进入接收卫星短消息的界面。需要说明的是，本申请实施例所列举的场景是以短消息为例进行说明的，如果不是短消息的场景，图4B和图4C中可以卫星短消息的字样修改为卫星消息。
在发送卫星消息(卫星短消息)的过程中，终端响应于用户对“新建卫星短消息”的标识403的点击操作，显示如图4D所示的新建卫星短消息界面。该新建卫星短消息界面中用户可以在收件人的框中选择收件人，如图4D中所示的收件人“Mary”，然后在编辑框中编辑第一卫星消息的内容，如图4D中所示的“一切正常，请勿担心”。本申请实施例提供的新建卫星短消息界面中会包括“携带位置”的标识405，该标识通常处于默认选择状态，终端向目标卫星发送第一卫星消息的内容时会自动携带当前终端所处位置的位置信息。当然，用户也可以通过点击“√”的位置来取消携带位置的功能。如果不勾选该携带位置的功能，发送第一卫星消息的内容时就不会携带当前终端所处位置的位置信息。
本申请实施例中，终端可以响应于用户对图4D中发送按键406的点击操作，会显示如图5A所示的加载界面。该加载界面中可以显示例如“请尽量处于开阔地带，避免视线空间上存在异物遮挡信号”的提示信息，还可以显示加载进度。
需要说明的是，终端响应于用户对发送按键406的点击操作也可以不显示如图5A所示的加载界面，可以直接显示加载后的结果界面，加载后的结果界面都可以称为寻星引导界面。
302.终端响应于用户对终端的移动操作，更新卫星标识的显示位置。
本申请实施例中，寻星引导界面用于引导用户调整终端的位置。用户可以通过卫星标识在寻星引导界面中的显示位置来确定终端与目标卫星的位置关系，进而移动终端(如：向左或向右移动终端，向上或向下移动终端)，终端会响应该移动，调整卫星标识在寻星引导界面上的显示位置。
303.若移动后的终端与目标卫星的位置关系满足消息传输条件，则终端向目标卫星发送第一卫星消息。
本申请实施例中，移动后的终端与目标卫星的位置关系满足消息传输条件可以是移动后的终端与目标卫星的位置关系可以使终端与目标卫星建立通信连接。
本申请实施例中，终端可以通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，使终端可以快速与卫星建立通信连接，从而可以使终端快速进行卫星消息的发送。
本申请实施例中，寻星引导界面中还可以包括寻星提示信息，该寻星提示信息用于提示用户移动终端的方向。如:寻星提示信息为向左移动终端、向右移动终端、向上移动终端或向下移动终端。需要说明的是，该寻星提示信息通常是终端按照最短移动路径给出的提示，这样，用户按照寻星提示信息移动终端，可以快速的将终端移动到适合与目标卫星建立通信连接的位置，进而加快了终端向目标卫星发送卫星消息或接收卫星消息的速度。
本申请实施例中的寻星引导界面，以及发送卫星消息的界面可以有多种表现形式，该表现形式与调整终端和目标卫星的方位角和俯仰角的顺序有关。关于方位角和俯仰角可以参阅图5B所示的三维坐标系(xyz)进行理解，如图5B所示，终端位于三维坐标系的圆心，终端上与卫星通信的天线为y轴方向，那么方位角为y轴与卫星在xy平面上的投影点C与 圆心的连线的夹角，俯仰角为卫星在xy平面上的投影点C与圆心的连线，以及卫星与圆心的连线的夹角。
本申请实施例中，寻星引导界面可以包括第一寻星引导界面和第二寻星引导界面。第一寻星引导界面包括第一卫星标识和第一对准区域，第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域。第二寻星引导界面包括第二卫星标识和第二对准区域，第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
本申请实施例中，寻星引导界面可以不划分为第一寻星引导界面和第二寻星引导界面，而是，寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域；第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
本申请实施例中，寻星引导界面的表现形式与调整终端与目标卫星的方位角和俯仰角的顺序相关，下面根据调整终端与目标卫星的方位角和俯仰角的顺序对不同表现形式的寻星引导界面进行介绍。
方案1.一种调整方位角的寻星引导界面(第一寻星引导界面)。
本申请实施例中，调整方位角时的一种寻星引导界面可以参阅图5C进行理解。如图5C所示，寻星引导界面中会显示“寻星中”的信息501，还会显示“信号状态”的标识502，目前图5C中，四个信号格都处于空白状态，表示还没有信号，图5C中的用于调整终端与目标卫星的位置关系的区域用圆盘区域503表示，第一卫星标识504会显示在圆盘区域503中，与目标卫星通信的天线覆盖的区域用扇形表示，通常为圆盘区域503的中心线的正负15°的范围，中心线为过圆盘503圆心，与y轴平行的线，该扇形区域可以称为第一对准区域505。该寻星引导界面中还可以显示寻星提示信息，如图5C中的“向右转动手机”的字样506，是调整方位角的一种寻星提示信息。
需要说明的是，本申请实施例中，第一卫星标识504以及第一对准区域505在圆盘区域505中的位置是以终端中与目标卫星通信的天线的位置作为参考，确定目标卫星相对于终端的水平方位，并在圆盘区域503的相应位置中显示第一卫星标识504。第一卫星标识504的位置可以是通过目标卫星进行手机定位的方式进行反向计算来确定的。
需要说明的是，寻星引导界面上显示的寻星提示信息的具体内容与第一卫星标识504所处的位置有关，如图5C中，第一卫星标识504位于第一对准区域505的右侧，也就是从第一对准区域505的中心线右侧的0°到180°的范围，为了使第一卫星标识504能以较短的路径或者以较小的转动角度进入到第一对准区域505，终端通常会给出“向右转动手机”的寻星提示信息。如果，第一卫星标识504位于第一对准区域505的左侧，也就是从第一对准区域505的中心线左侧的0°到180°的范围，为了使第一卫星标识504能以较短的路径或者以较小的转动角度进入到第一对准区域505，终端通常会给出“向左转动手机”的 寻星提示信息。虽然本申请实施例中，未给出第一卫星标识504位于第一对准区域505的左侧的示意图，但依据此处的文字描述，结合图5C也很容易理解第一卫星标识504位于第一对准区域505左侧的方案。
在图5C所示的寻星引导界面上，若用户按照“向右转动手机”的寻星提示信息来操作，或者用户向左转动手机的度数是360°与向右转动度数的差值，都可以将第一卫星标识504转动到第一对准区域505，终端的界面会随之刷新，显示如图5D所示的寻星引导界面。如图5D所示的寻星引导界面中，第一卫星标识504位于第一对准区域505的中心线的位置，表示已调整好方位角，因为俯仰角还没调整，所以如图5D所示的寻星引导界面中“信号状态”的标识502的四个信号格还都处于空白状态。
需要说明的是，本申请实施例中，第一卫星标识的显示位置位于第一对准区域之外时，第一对准区域以第一颜色显示；第一卫星标识的显示位置位于第一对准区域之内时，第一对准区域以第二颜色显示，第一颜色与第二颜色不同。
结合前面的卫星短消息的场景，相对于图5C，第一对准区域505在还未调整方位角时可以以第一颜色显示，如图5E所示，在调整好方位角后，第一卫星标识504位于第一对准区域505后，相对于图5D，该第一对准区域505可以以第二颜色显示，如图5F所示，第一颜色与第二颜色不同。这样，通过颜色变化可以更好的提示用户已经完成方位角的对准。
方案2.一种调整俯仰角的寻星引导界面(第二寻星引导界面)。
本申请实施例中，调整俯仰角时的一种寻星引导界面可以参阅图6A进行理解。如图6A所示，寻星引导界面中会显示“寻星中”的信息，还会显示“信号状态”的标识，目前图6A中，四个信号格都处于空白状态，表示还没有信号，图6A中的用于调整终端与目标卫星的位置关系的区域用圆盘区域表示。关于图6A中的这些内容可以参阅图5C中对501、502和503的介绍进行理解。
第二卫星标识601会显示在圆盘区域中，第二对准区域602是与圆盘区域通信的一个小圆盘。该寻星引导界面中还可以显示寻星提示信息，如图6A中的“向上抬手机”的字样603，是调整俯仰角的一种寻星提示信息。
需要说明的是，本申请实施例中，第二卫星标识601以及第二对准区域602在圆盘区域中的位置是以终端中与目标卫星通信的天线的位置作为参考，确定目标卫星相对于终端的俯仰方位，并在圆盘区域的相应位置中显示第二卫星标识601。
需要说明的是，寻星引导界面上显示的寻星提示信息的具体内容与第二卫星标识601所处的位置有关，如图6A中，第二卫星标识601位于第二对准区域602的正下方，终端会给出“向上抬手机”的寻星提示信息。如果，第二卫星标识601位于第二对准区域602的正上方，终端会给出“向下压手机”的寻星提示信息。虽然本申请实施例中，未给出第二卫星标识601位于第二对准区域602的正上方的示意图，但依据此处的文字描述，结合图6A也很容易理解第二卫星标识601位于第二对准区域602的正上方的方案。
在图6A所示的寻星引导界面上，若用户按照“向上抬手机”的寻星提示信息来操作，将第二卫星标识601移动到第二对准区域602，终端的界面会随之刷新，显示如图6B所示的寻星引导界面。如图6B所示的寻星引导界面中，第二卫星标识601位于第二对准区域 602的中心位置，表示已调整好俯仰角。
需要说明的是，第二卫星标识的显示位置位于第二对准区域之外时，第二对准区域以第三颜色显示；第二卫星标识的显示位置位于第二对准区域之内时，第二对准区域以第四颜色显示，第三颜色与第四颜色不同。
结合前面卫星短消息的场景，相对于图6A，第二对准区域602在还未调整方位角时可以以第三颜色显示，在调整好方位角后，第二卫星标识601位于第二对准区域602后，该第二对准区域602还可以以第四颜色显示，第三颜色与第四颜色不同，虽然第二对准区域602的颜色变化过程没有通过示意图展示，但也可以结合图5E和图5F的颜色变化过程进行理解。这样，通过颜色变化可以更好的提示用户已经完成俯仰角的对准。
方案3.一种先调整方位角再调整俯仰角的寻星引导界面。
该方案3即先显示第一寻星引导界面，再显示第二寻星引导界面，对应于前面步骤301和302，该过程具体可以包括：显示第一寻星引导界面，响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；当第一卫星标识位于第一对准区域时，显示第二寻星引导界面；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
结合前面方案1和方案2所介绍的卫星短消息的场景，本申请实施例中，若按照先调整方位角再调整俯仰角的顺序进行寻星调整，终端会先后显示图5C、图5D、图6A和图6B，然后可以得到如图6C所示的发送卫星消息的界面。如图6C所示，按照先方位角再俯仰角的顺序调整，在发送卫星短消息的界面可以只显示调整俯仰角的界面的第二卫星标识601和第二对准区域602，不显示第一卫星标识504和第一对准区域505。另外，在发送卫星短消息的界面上的“信号状态”的标识604中的四格信号中有3个处于满格状态，表示已与卫星建立连接，该发送卫星短消息的界面上还可以显示“正在发送”的字样605，以及还可以显示“请保持手持姿势”的字样606。
方案4.一种先调整俯仰角再调整方位角的寻星引导界面。
该方案4即先显示第二寻星引导界面，再显示第一寻星引导界面，对应于前面步骤301和302，该过程具体可以包括：显示第二寻星引导界面，响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置；当第二卫星标识位于第二对准区域时，显示第一寻星引导界面；响应于用户对终端的向左移动或向右移动操作，更新第一卫星标识的显示位置。
结合前面方案1和方案2所介绍的卫星短消息的场景，本申请实施例中，若按照先调整俯仰角再调整方位角的顺序进行寻星调整，终端会先后显示图6A、图6B、5C和图5D，然后可以得到如图6D所示的发送卫星短消息的界面。如图6D所示，按照先俯仰角再方位角的顺序调整，在发送卫星短消息的界面可以只显示调整方位角的界面的第一卫星标识504和第一对准区域505，不显示第二卫星标识601和第二对准区域602。另外，在发送卫星短消息的界面上的“信号状态”的标识604中的四格信号中有3个处于满格状态，表示已与卫星建立连接，该发送卫星短消息的界面上还可以显示“正在发送”的字样605，以及还可以显示“请保持手持姿势”的字样606。
方案5.另一种先调整方位角再调整俯仰角的寻星引导界面。
该方案5即先显示第一寻星引导界面，再显示第二寻星引导界面，不同于方案3的部分的第二寻星引导界面不显示第一卫星标识和第一对准区域的是：该方案5中的第二寻星引导界面还显示第一卫星标识和第一对准区域。
结合前面卫星短消息的场景，本申请实施例中，若按照先调整方位角再调整俯仰角的顺序进行寻星调整，终端会先后显示图5C、图5D、然后显示图7A所示的寻星引导界面。
如图7A所示，该寻星引导界面中在调整俯仰角时不仅显示了第二卫星标识601和第二对准区域602，还显示了第一卫星标识504和第一对准区域505。除此之外，该图7A所示的寻星引导界面中还可以显示“向上抬手机”的寻星提示信息、“信号状态”，以及“寻星中”等字样。对于这些内容，前面图6A部分已经介绍过，这里不再重复介绍。
在图7A所示的寻星引导界面上，若用户按照“向上抬手机”的寻星提示信息来操作，将第二卫星标识601移动到第二对准区域602，终端的界面会随之刷新，显示如图7B所示的寻星引导界面。如图7B所示的寻星引导界面中，第二卫星标识601位于第二对准区域602的中心位置，表示已调整好俯仰角，同时还会显示第一卫星标识504位于第一对准区域505。
需要说明的是，若在调整俯仰角的过程中，第一卫星标识504偏离出了第一对准区域505，则还可以采用前面介绍的调整方位角的原理再次将第一卫星标识504调回第一对准区域505。
在图7B的基础上，终端会刷新出如图7C所示的发送卫星短消息的界面。如图7C所示，按照先方位角再俯仰角的顺序调整，在发送卫星短消息的界面可以既显示调整俯仰角的界面的第二卫星标识601和第二对准区域602，又显示第一卫星标识504和第一对准区域505。另外，在发送卫星短消息的界面上的“信号状态”的标识604中的四格信号中有3个处于满格状态，表示已与卫星建立连接，该发送卫星短消息的界面上还可以显示“正在发送”的字样605，以及还可以显示“请保持手持姿势”的字样606。
方案6.另一种先调整俯仰角再调整方位角的寻星引导界面。
该方案6即先显示第二寻星引导界面，再显示第一寻星引导界面，不同于方案4的部分的第一寻星引导界面不显示第二卫星标识和第二对准区域的是：该方案6中的第一寻星引导界面还显示第二卫星标识和第二对准区域。
结合前面卫星短消息的场景，本申请实施例中，若按照先调整俯仰角再调整方位角的顺序进行寻星调整，终端会先后显示图6A、图6B、然后显示图8A所示的寻星引导界面。
如图8A所示，该寻星引导界面中在调整俯仰角时不仅显示了第一卫星标识504和第一对准区域505，还显示了第二卫星标识601和第二对准区域602。除此之外，该图8A所示的寻星引导界面中还可以显示“向右转动手机”的寻星提示信息、“信号状态”，以及“寻星中”等字样。对于这些内容，前面图5C部分已经介绍过，这里不再重复介绍。
在图8A所示的寻星引导界面上，若用户按照“向右转动手机”的寻星提示信息来操作，将第一卫星标识504转动到第一对准区域505，终端的界面会随之刷新，显示如图7B所示的寻星引导界面。如图7B所示的寻星引导界面中，第一卫星标识504位于第一对准区域 505，表示已调整好方位角，同时还会显示第二卫星标识601位于第二对准区域602。
需要说明的是，若在调整方位角的过程中，第二卫星标识601偏离出了第二对准区域602，则还可以采用前面介绍的调整俯仰角的原理再次将第二卫星标识601调回第二对准区域602。
在图7B的基础上，终端会刷新出如图7C所示的发送卫星短消息的界面。如图7C所示，按照先俯仰角再方位角的顺序调整，在发送卫星短消息的界面可以既显示调整方位角的界面的第一卫星标识504和第一对准区域505，又显示第二卫星标识601和第二对准区域602。另外，在发送卫星短消息的界面上的“信号状态”的标识604中的四格信号中有3个处于满格状态，表示已与卫星建立连接，该发送卫星短消息的界面上还可以显示“正在发送”的字样605，以及还可以显示“请保持手持姿势”的字样606。
方案7.另一种先调整方位角再调整俯仰角的寻星引导界面。
该方案7的寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域。前面实施例中的步骤302具体包括：响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
结合前面卫星短消息的场景，本申请实施例中，若按照先调整方位角再调整俯仰角的顺序进行寻星调整，终端按顺序可以显示如图8B所示的寻星引导界面。
如图8B所示，该寻星引导界面中，该寻星引导界面中在调整方位角时不仅显示了第一卫星标识504和第一对准区域505，还显示了第二卫星标识601和第二对准区域602。除此之外，该图8B所示的寻星引导界面中还可以显示“向右转动手机”的寻星提示信息、“信号状态”，以及“寻星中”等字样。对于这些内容，前面图5C部分已经介绍过，这里不再重复介绍。
在图8B所示的寻星引导界面上，若用户按照“向右转动手机”的寻星提示信息来操作，将第一卫星标识504转动到第一对准区域505，终端的界面会随之刷新，显示如图7A所示的寻星引导界面。然后在如图7A所示的寻星引导界面的基础上调整俯仰角刷新出如图7B所示的寻星引导界面中，进而刷新出如图7C所示的发送卫星短消息的界面。
方案8.另一种先调整俯仰角再调整方位角的寻星引导界面。
结合前面卫星短消息的场景，本申请实施例中，若按照先调整俯仰角再调整方位角的顺序进行寻星调整，终端按顺序可以显示如图8C所示的寻星引导界面。
如图8C所示，该寻星引导界面中，该寻星引导界面中在调整方位角时不仅显示了第一卫星标识504和第一对准区域505，还显示了第二卫星标识601和第二对准区域602。除此之外，该图8C所示的寻星引导界面中还可以显示“向上抬手机”的寻星提示信息、“信号状态”，以及“寻星中”等字样。对于这些内容，前面图5C部分已经介绍过，这里不再重复介绍。
在图8C所示的寻星引导界面上，若用户按照“向上抬手机”的寻星提示信息来操作，将第二卫星标识601移动到第二对准区域602，终端的界面会随之刷新，显示如图8A所示的寻星引导界面。然后在如图8A所示的寻星引导界面的基础上调整方位角刷新出如图7B 所示的寻星引导界面中，进而刷新出如图7C所示的发送卫星短消息的界面。
方案9.一种同时调整方位角和俯仰角的寻星引导界面。
结合前面卫星短消息的场景，本申请实施例中，不仅可以按照前面介绍的8种方案有先后顺序的调整方位角和俯仰角，还可以同时调整方位角和俯仰角，当同时调整方位角的俯仰角时，终端可以直接显示如图9所示的寻星引导界面，在图9中，与前面图8B或图8C不同的是，图9中的寻星提示信息是“向右转动手机+向上抬手机”。
在图9所示的寻星引导界面上，若用户按照“向右转动手机+向上抬手机”的寻星提示信息来同步操作，将第一卫星标识504转动到第一对准区域505，将第二卫星标识601移动到第二对准区域602，终端的界面会随之刷新，显示如图7B所示的寻星引导界面中，进而刷新出如图7C所示的发送卫星短消息的界面。
以上所介绍的寻星调整的方案中，寻星引导界面和发送卫星短消息的界面中都只显示了一颗卫星的卫星标识，实际上，本申请中，并不限定寻星引导界面和发送卫星短消息的界面中所显示的卫星数量，当能与终端通信的卫星有多颗时，可以在寻星引导界面和发送卫星短消息的界面显示多颗卫星的卫星标识，下面以显示两颗卫星的卫星标识为例，结合前面显示一颗卫星时的方案7介绍方案10。
方案10.显示多颗卫星的卫星标识时的先调整方位角再调整俯仰角的寻星引导界面。
如图10A所示的寻星引导界面上包括两颗卫星的卫星标识，其中第一卫星(目标卫星)的第一卫星标识504和第二卫星标识601前面已经介绍过，第二卫星的第一卫星标识用1001表示，第二卫星标识用1002表示。该图10A所示的方案中，调整第一卫星标识504所代表的第一卫星是较优的方案，所以终端的在该图10A所示的寻星引导界面上给出了“向右转动手机”的寻星提示信息。
在图10A的基础上，若用户按照“向右转动手机”的寻星提示信息来同步操作，将第一卫星标识504转动到第一对准区域505，终端的界面会随之刷新，显示如图10B所示的寻星引导界面。该如图10B所示的寻星引导界面中显示了“向上抬手机”的寻星提示信息，若用户按照该“向上抬手机”的寻星提示信息进行操作，将第二卫星标识601移动到第二对准区域602，终端的界面会随之刷新，显示如图10C所示的寻星引导界面，进而刷新出如图10D所示的发送卫星短消息的界面。
本申请实施例所介绍的方案10中，在上述方案7的基础上增加了第二卫星的第一卫星标识1001和第二卫星标识1002，实际上，在前面介绍的除方案7之外的其他方案1-6，方案8和9的基础上，都可以增加类似于方案10所介绍的另外一颗卫星的卫星标识。而且，终端会根据另一颗卫星与第一对准区域的关系来确定所显示的寻星提示信息，可见，多颗卫星时的寻星引导界面以及发送卫星短消息的界面可以有多种，对此本申请实施例中不再做一一介绍。而且，本申请实施例中，方案1至方案10中的第一对准区域和第二对准区域中在方位角和俯仰角对准前后都可以设置不同的颜色，都可以参阅前面的图5E和图5F进行理解，对于颜色的填充和变化过程，本申请实施例中不再做一一介绍。
本申请实施例中，在发送第一卫星消息之后，还可以：响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息之后的位置变化；若终端发送第一卫星消息之后的 位置变化小于第一阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
还可以是，在发送第一卫星消息之后，还可以：响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息时的时间；若终端发送第一卫星消息时的时间距离用户触发第二卫星消息的发送操作之间的时间差小于第二阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
结合前面卫星短消息的场景，本申请实施例中，在终端发送第一卫星短消息后，可以收到卫星反馈的发送成功的消息，针对前面给收件人“Mary”发送的消息，可以显示如图11A所示的界面。若用户担心第二终端不能成功接收，还可以保持终端调整好方位角和俯仰角的姿势向同一收件人再发送一次第二卫星短消息。因为与上一次发送卫星短消息的时间间隔很小或者手机的位置变化变化很小，所以再次发送卫星短消息时可以不用再次进入寻星引导界面，若第二卫星短消息也发送成功，则终端会显示如图11B所示的界面。
本申请实施例中，在终端发送第一卫星短消息后，还可以保持终端调整好方位角和俯仰角的姿势，向另外一个收件人发送第二卫星短消息，如图11C所示，向收件人“Lucy”发送第二卫星短消息。因为向收件人“Lucy”发送第二卫星短消息与上一次向收件人“Mary”发送卫星短消息的时间间隔很小或者手机的位置变化变化很小，所以向收件人“Lucy”发送第二卫星短消息时可以不用再次进入寻星引导界面，若向收件人“Lucy”发送的第二卫星短消息也发送成功，则终端会显示如图11D所示的界面。
图11A至图11D都是描述的卫星短消息发送成功的情形，在向目标卫星发送第一卫星消息之后，该方法还包括：接收到第一卫星消息发送失败的响应消息；根据第一卫星消息发送失败的响应消息，显示寻星引导界面。
结合前面卫星短消息的场景，当卫星短消息发送失败时，以向收件人“Lucy”发送第二卫星短消息失败为例，终端会显示如图11E所示的界面。
针对发送失败的情形，终端可以再次显示寻星引导界面，以方便用户再次进行寻星对准。在发送失败时，终端的显示界面中还可以弹出“是否更换一颗卫星”的提示信息。
另外，本申请实施例中，还可以将未发送成功的普通消息转换为卫星消息发送，该过程可以是：在显示寻星引导界面之前，向基站发送普通消息；接收到普通消息发送失败的响应消息；响应于普通消息发送失败的响应消息，显示寻星引导界面。
在卫星短消息的场景中，当普通短消息发送失败时，终端可以自动转入卫星短消息发送，将该普通短消息的内容自动填入到卫星短消息的编辑区，并启动前面实施例所描述的寻星过程。也可以是，当普通短消息发送失败时，提示用户是否转卫星短消息发送，如果用户选择“是”，即用户同意转入卫星短消息发送，终端将该普通短消息的内容自动填入到卫星短消息的编辑区，并启动前面实施例所描述的寻星过程。
以上介绍了消息发送的方法的相应内容，下面对消息接收的方法进行介绍。
如图12所示，本申请实施例提供的消息接收的方法的一实施例可以包括：
1201.终端显示寻星引导界面。
该寻星引导界面包括卫星标识，卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系。
1202.终端响应于用户对终端的移动操作，更新卫星标识的显示位置。
1203.若移动后的终端与目标卫星的位置关系满足消息传输条件，则终端从目标卫星接收第一卫星消息。
本申请实施例中，终端可以通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，使终端可以快速与卫星建立通信连接，从而可以使终端快速进行卫星消息的接收。
本申请实施例中，步骤1201和1202都可以参阅前面消息接收的方法的相应内容进行理解。此处不再重复介绍，不同的是，步骤1203是从目标卫星接收第一卫星消息，而步骤303是向目标卫星发送第一卫星消息。
本申请实施例中，以卫星消息是卫星短消息为例，接收卫星短消息的操作可以是在如图13A所示的界面中操作的，如响应于用户对图13A中接收卫星短消息的标识404的点击操作，启动如图5A所示的加载界面，或者显示其他前面接收卫星短消息过程中介绍的寻星引导界面，然后按照前面接收卫星短消息过程中介绍方案1至方案10或者其他可行的方案进行寻星引导，使得终端与卫星建立通信连接，进而通过卫星接收卫星短消息。
终端接收到卫星短消息的一个界面可以参阅图13B进行理解，如图13B所示，接收到Peter发送来的卫星短消息“开车来这个位置接我”，其中还携带位置信息。
本申请实施例中，无论是消息发送的方法，还是消息接收的方法，都可以通过卫星来实现对消息的发送或接收，而且还可以实现终端与目标卫星的对准，提高了消息发送的成功率，尤其是在移动通信信号较弱或者移动通信信号无服务的区域，提高了消息发送的成功率。
以上介绍了卫星消息的发送过程以及卫星消息的接收过程，下面结合附图，介绍本申请实施例提供的终端。
如图14所示，本申请实施例提供的终端140包括：
显示单元1401，用于显示寻星引导界面，寻星引导界面包括卫星标识，卫星标识在寻星引导界面上的显示位置用于指示终端与目标卫星的位置关系。
处理单元1402，用于响应于用户对终端的移动操作，更新显示单元1401显示的卫星标识的显示位置。
收发单元1403，用于若处理单元1402响应用户移动后的终端与目标卫星的位置关系满足消息传输条件，则向目标卫星发送第一卫星消息或从目标卫星接收第一卫星消息。
本申请实施例中，终端可以通过寻星引导界面引导用户调整终端与目标卫星之间的位置关系，使终端可以快速与卫星建立通信连接，从而可以使终端快速进行卫星消息的发送或接收。
可选地，寻星引导界面还包括寻星提示信息，寻星提示信息用于提示用户移动终端的方向。
可选地，寻星引导界面包括第一寻星引导界面和第二寻星引导界面；第一寻星引导界面包括第一卫星标识和第一对准区域，第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二寻星引导界面包括第二卫星标识和第二对准区域，第二卫星标 识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
可选地，显示单元1401，具体用于显示第一寻星引导界面。
处理单元1402，具体用于响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置。
显示单元1401，具体用于当第一卫星标识位于第一对准区域时，显示第二寻星引导界面。
处理单元1402，具体用于响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
可选地，显示单元1401，具体用于显示第二寻星引导界面。
处理单元1402，具体用于响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
显示单元1401，具体用于当第二卫星标识位于第二对准区域时，显示第一寻星引导界面。
处理单元1402，具体用于响应于用户对终端的向左移动或向右移动操作，更新第一卫星标识的显示位置。
可选地，寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域；第一卫星标识用于指示终端与目标卫星在方位角上的位置关系，当终端与目标卫星在方位角上的位置关系满足消息传输条件时，第一卫星标识位于第一对准区域；第二卫星标识用于指示终端与目标卫星在俯仰角上的位置关系，当终端与目标卫星在俯仰角上的位置关系满足消息传输条件时，第二卫星标识位于第二对准区域。
可选地，处理单元1402，具体用于响应于用户对终端的向左移动操作或向右移动操作，更新第一卫星标识的显示位置；响应于用户对终端的向上移动操作或向下移动操作，更新第二卫星标识的显示位置。
可选地，第一卫星标识的显示位置位于第一对准区域之外时，第一对准区域以第一颜色显示；第一卫星标识的显示位置位于第一对准区域之内时，第一对准区域以第二颜色显示，第一颜色与第二颜色不同。
可选地，第二卫星标识的显示位置位于第二对准区域之外时，第二对准区域以第三颜色显示；第二卫星标识的显示位置位于第二对准区域之内时，第二对准区域以第四颜色显示，第三颜色与第四颜色不同。
可选地，显示单元1401，还用于当终端用于发送第一卫星消息时，在显示寻星引导界面之前，响应于用户新建卫星消息的操作或者回复卫星消息的操作，显示卫星消息编辑界面，卫星消息编辑界面用于用户输入第一卫星消息的内容。
可选地，显示单元1401，具体用于响应于用户对第一卫星消息的发送操作，显示寻星引导界面。
可选地，显示单元1401，具体用于响应于用户接收卫星消息的操作，显示寻星引导界面。
可选地，收发单元1403，还用于向基站发送普通消息；以及接收到普通消息发送失败的响应消息。
显示单元1401，具体用于响应于普通消息发送失败的响应消息，显示寻星引导界面。
可选地，处理单元1402，还用于响应于用户对第二卫星消息的发送操作，确定终端发送第一卫星消息之后的位置变化。
收发单元1403，还用于若终端发送第一卫星消息之后的位置变化小于第一阈值，向目标卫星发送第二卫星消息，不显示寻星引导界面。
可选地，收发单元1403，还用于接收到第一卫星消息发送失败的响应消息。
显示单元1401，还用于根据第一卫星消息发送失败的响应消息，显示寻星引导界面。
本申请实施例中，终端中各单元所执行的操作与前述图3至图13B所示实施例中描述的类似，此处不再赘述。
在本申请的另一实施例中，还提供一种计算机可读存储介质，计算机可读存储介质中存储有计算机执行指令，当终端的处理器执行该计算机执行指令时，终端执行上述图3至图13B中终端设备所执行的步骤。
在本申请的另一实施例中，还提供一种计算机程序产品，该计算机程序产品包括计算机程序代码，当计算机程序代码在计算机上执行时，计算机设备执行上述图3至图13B中终端所执行的步骤。
在本申请的另一实施例中，还提供一种芯片系统，该芯片系统包括一个或多个接口电路和一个或多个处理器；接口电路和处理器通过线路互联；接口电路用于从终端的存储器接收信号，并向处理器发送信号，信号包括存储器中存储的计算机指令；当处理器执行计算机指令时，终端执行前述上述图3至图13B中终端设备所执行的步骤。在一种可能的设计中，芯片系统还可以包括存储器，存储器，用于保存控制设备必要的程序指令和数据。该芯片系统，可以由芯片构成，也可以包含芯片和其他分立器件。
在本申请所提供的几个实施例中，应该理解到，所揭露的系统，装置和方法，可以通过其它的方式实现。例如，以上所描述的装置实施例仅仅是示意性的，例如，单元的划分，仅仅为一种逻辑功能划分，实际实现时可以有另外的划分方式，例如多个单元或组件可以结合或者可以集成到另一个系统，或一些特征可以忽略，或不执行。另一点，所显示或讨论的相互之间的耦合或直接耦合或通信连接可以是通过一些接口，装置或单元的间接耦合或通信连接，可以是电性，机械或其它的形式。
所述作为分离部件说明的单元可以是或者也可以不是物理上分开的，作为单元显示的部件可以是或者也可以不是物理单元，即可以位于一个地方，或者也可以分布到多个网络单元上。可以根据实际的需要选择其中的部分或者全部单元来实现本实施例方案的目的。
另外，在本申请各个实施例中的各功能单元可以集成在一个处理单元中，也可以是各个单元单独物理存在，也可以两个或两个以上单元集成在一个单元中。上述集成的单元可以全部或部分地通过软件、硬件、固件或者其任意组合来实现。
当使用软件实现所述集成的单元时，可以全部或部分地以计算机程序产品的形式实现。所述计算机程序产品包括一个或多个计算机指令。在计算机上加载和执行所述计算机程序 指令时，全部或部分地产生按照本申请实施例所述的流程或功能。所述计算机可以是通用计算机、专用计算机、计算机网络、或者其他可编程装置。所述计算机指令可以存储在计算机可读存储介质中，或者从一个计算机可读存储介质向另一个计算机可读存储介质传输，例如，所述计算机指令可以从一个网站站点、计算机、服务器或数据中心通过有线(例如同轴电缆、光纤、数字用户线(digital subscriber line，DSL))或无线(例如红外、无线、微波等)方式向另一个网站站点、计算机、服务器或数据中心进行传输。所述计算机可读存储介质可以是计算机能够存取的任何可用介质或者是包含一个或多个可用介质集成的服务器、数据中心等数据存储设备。所述可用介质可以是磁性介质，(例如，软盘、硬盘、磁带)、光介质(例如，DVD)、或者半导体介质(例如固态硬盘(solid state disk，SSD))等。

Claims (18)

  1. 一种消息传输的方法，应用于终端，其特征在于，包括：
    显示寻星引导界面，所述寻星引导界面包括卫星标识，所述卫星标识在所述寻星引导界面上的显示位置用于指示所述终端与目标卫星的位置关系；
    响应于用户对所述终端的移动操作，更新所述卫星标识的显示位置；
    若移动后的所述终端与所述目标卫星的位置关系满足消息传输条件，则向所述目标卫星发送第一卫星消息或从所述目标卫星接收第一卫星消息。
  2. 根据权利要求1所述的方法，其特征在于，所述寻星引导界面还包括寻星提示信息，所述寻星提示信息用于提示用户移动所述终端的方向。
  3. 根据权利要求1或2所述的方法，其特征在于，
    所述寻星引导界面包括第一寻星引导界面和第二寻星引导界面；
    所述第一寻星引导界面包括第一卫星标识和第一对准区域，所述第一卫星标识用于指示所述终端与所述目标卫星在方位角上的位置关系，当所述终端与所述目标卫星在所述方位角上的位置关系满足所述消息传输条件时，所述第一卫星标识位于所述第一对准区域；
    所述第二寻星引导界面包括第二卫星标识和第二对准区域，所述第二卫星标识用于指示所述终端与所述目标卫星在俯仰角上的位置关系，当所述终端与所述目标卫星在所述俯仰角上的位置关系满足所述消息传输条件时，所述第二卫星标识位于第二对准区域。
  4. 根据权利要求3所述的方法，其特征在于，
    所述显示寻星引导界面；所述响应于用户对所述终端的移动操作，更新所述卫星标识的显示位置，具体包括：
    显示所述第一寻星引导界面，响应于用户对所述终端的向左移动操作或向右移动操作，更新所述第一卫星标识的显示位置；
    当所述第一卫星标识位于所述第一对准区域时，显示所述第二寻星引导界面；
    响应于用户对所述终端的向上移动操作或向下移动操作，更新所述第二卫星标识的显示位置。
  5. 根据权利要求3所述的方法，其特征在于，
    所述显示寻星引导界面；所述响应于用户对所述终端的移动操作，更新所述卫星标识的显示位置，具体包括：
    显示所述第二寻星引导界面，响应于用户对所述终端的向上移动操作或向下移动操作，更新所述第二卫星标识的显示位置；
    当所述第二卫星标识位于所述第二对准区域时，显示所述第一寻星引导界面；
    响应于用户对所述终端的向左移动或向右移动操作，更新所述第一卫星标识的显示位置。
  6. 根据权利要求1或2所述的方法，其特征在于，
    所述寻星引导界面包括第一卫星标识和第一对准区域，第二卫星标识和第二对准区域；
    所述第一卫星标识用于指示所述终端与所述目标卫星在方位角上的位置关系，当所述终端与所述目标卫星在方位角上的位置关系满足所述消息传输条件时，所述第一卫星标识 位于所述第一对准区域；
    所述第二卫星标识用于指示所述终端与所述目标卫星在俯仰角上的位置关系，当所述终端与所述目标卫星在俯仰角上的位置关系满足所述消息传输条件时，所述第二卫星标识位于所述第二对准区域。
  7. 根据权利要求6所述的方法，其特征在于，所述响应于用户对所述终端的移动操作，更新所述卫星标识的显示位置，具体包括：
    响应于用户对所述终端的向左移动操作或向右移动操作，更新所述第一卫星标识的显示位置；或，
    响应于用户对所述终端的向上移动操作或向下移动操作，更新所述第二卫星标识的显示位置。
  8. 根据权利要求3-7任一项所述的方法，其特征在于，
    所述第一卫星标识的显示位置位于所述第一对准区域之外时，所述第一对准区域以第一颜色显示；所述第一卫星标识的显示位置位于所述第一对准区域之内时，所述第一对准区域以第二颜色显示，所述第一颜色与所述第二颜色不同。
  9. 根据权利要求3-8任一项所述的方法，其特征在于，
    所述第二卫星标识的显示位置位于所述第二对准区域之外时，所述第二对准区域以第三颜色显示；所述第二卫星标识的显示位置位于所述第二对准区域之内时，所述第二对准区域以第四颜色显示，所述第三颜色与所述第四颜色不同。
  10. 根据权利要求1-9任一项所述的方法，其特征在于，当所述终端用于发送所述第一卫星消息时，在所述显示寻星引导界面之前，所述方法还包括：
    响应于用户新建卫星消息的操作或者回复卫星消息的操作，显示卫星消息编辑界面，所述卫星消息编辑界面用于用户输入所述第一卫星消息的内容。
  11. 根据权利要求10所述的方法，其特征在于，所述显示寻星引导界面，具体包括：
    响应于用户对所述第一卫星消息的发送操作，显示所述寻星引导界面。
  12. 根据权利要求1-9任一项所述的方法，其特征在于，当所述终端用于接收所述第一卫星消息时，所述显示所述寻星引导界面，具体包括：
    响应于用户接收卫星消息的操作，显示所述寻星引导界面。
  13. 根据权利要求1-9任一项所述的方法，其特征在于，当所述终端用于发送所述第一卫星消息时，在所述显示寻星引导界面之前，所述方法还包括：
    向基站发送普通消息；
    接收到所述普通消息发送失败的响应消息；
    所述显示所述寻星引导界面，具体包括：
    响应于所述普通消息发送失败的响应消息，显示所述寻星引导界面。
  14. 根据权利要求1-11、13任一项所述的方法，其特征在于，在发送所述第一卫星消息之后，所述方法还包括：
    响应于用户对第二卫星消息的发送操作，确定所述终端发送所述第一卫星消息之后的位置变化；
    若所述终端发送所述第一卫星消息之后的位置变化小于第一阈值，向所述目标卫星发送所述第二卫星消息，不显示所述寻星引导界面。
  15. 根据权利要求1-11、13-14任一项所述的方法，其特征在于，在向所述目标卫星发送第一卫星消息之后，所述方法还包括：
    接收到所述第一卫星消息发送失败的响应消息；
    根据所述第一卫星消息发送失败的响应消息，显示所述寻星引导界面。
  16. 一种终端，其特征在于，包括：收发器、处理器和存储器，所述收发器和所述处理器与存储器耦合，所述存储器用于存储程序或指令，当所述程序或指令被所述处理器执行时，使得所述终端执行如权利要求1至15中任一项所述的方法。
  17. 一种计算机可读存储介质，其特征在于，所述计算机可读存储介质中存储有指令，当所述指令在终端上运行时，使得所述终端执行如权利要求1至15中任一项所述的方法。
  18. 一种计算机程序产品，其特征在于，所述计算机程序产品包括计算机程序代码，当所述计算机程序代码在计算机上运行时，使得所述计算机执行如权利要求1至15中任一项所述的方法。
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