CN117833948A - Electronic device, communication system, communication control method, and computer device - Google Patents

Electronic device, communication system, communication control method, and computer device Download PDF

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Publication number
CN117833948A
CN117833948A CN202311873910.6A CN202311873910A CN117833948A CN 117833948 A CN117833948 A CN 117833948A CN 202311873910 A CN202311873910 A CN 202311873910A CN 117833948 A CN117833948 A CN 117833948A
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China
Prior art keywords
satellite
radio frequency
antenna
communication
frequency circuit
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CN202311873910.6A
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Chinese (zh)
Inventor
李江
杨永强
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Guangdong Oppo Mobile Telecommunications Corp Ltd
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Guangdong Oppo Mobile Telecommunications Corp Ltd
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Priority to CN202311873910.6A priority Critical patent/CN117833948A/en
Publication of CN117833948A publication Critical patent/CN117833948A/en
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Abstract

The application relates to electronic equipment, a communication system, a communication control method and computer equipment, which realize functional matching in different scenes by switching control of connection states between different radio frequency circuits and antennas in different scenes, and simultaneously can enable a first radio frequency circuit to be disconnected with the antennas in time when a second radio frequency circuit is in a transmitting state, so that the problem of channel blocking and even device damage caused by the transmission of satellite communication signals of the first radio frequency circuit is avoided. Therefore, the protection of the radio frequency channel can be realized on the basis of realizing the satellite communication and satellite positioning functions, and the overall reliability, safety and stability are improved, so that the product yield is improved, and the customer return rate, the maintenance rate and the complaint rate are reduced.

Description

Electronic device, communication system, communication control method, and computer device
Technical Field
The present disclosure relates to the field of antenna technologies, and in particular, to an electronic device, a communication system, a communication control method, and a computer device.
Background
With the development of communication technology, users and operators have higher and higher service requirements on electronic equipment, and have wider and wider requirements on the range of supporting network coverage of the electronic equipment, so that antennas in the electronic equipment are more and more, layout space is more and more limited, isolation between the antennas is difficult to ensure, and potential access blockage or risk of damage to devices is difficult.
Disclosure of Invention
The embodiment of the application provides electronic equipment, a communication system, a communication control method and computer equipment, which can solve the problems of channel blockage and device damage.
The first aspect of the present application provides an electronic device, including:
the first radio frequency circuit is used for supporting the reception of satellite positioning signals when being connected to the antenna in a conducting manner;
the second radio frequency circuit is used for supporting to transmit satellite communication signals to a target communication satellite when being connected to the antenna in a conducting mode;
the control circuit is respectively connected with the first radio frequency circuit and the second radio frequency circuit and is used for controlling connection and conduction between the first radio frequency circuit and the antenna under a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; and the electronic equipment is also used for determining the position information of the electronic equipment according to the satellite positioning signals in the satellite positioning scene, determining the target communication satellite in the satellite communication scene, controlling the connection between the first radio frequency circuit and the antenna to be disconnected, and controlling the connection between the second radio frequency circuit and the antenna to be conducted.
A second aspect of the present application provides an electronic device, comprising:
The first radio frequency circuit is used for supporting the reception of satellite positioning signals when being connected to the antenna in a conducting manner;
the second radio frequency circuit is used for supporting to transmit satellite communication signals to a target communication satellite when being connected to the antenna in a conducting mode;
the switch circuit is respectively connected with the first radio frequency circuit, the second radio frequency circuit and the antenna and is used for conducting connection between the first radio frequency circuit and the antenna in a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; the satellite positioning device is also used for disconnecting the connection between the first radio frequency circuit and the antenna and conducting the connection between the second radio frequency circuit and the antenna under the condition that the satellite positioning scene is determined and the target communication satellite is determined;
the satellite positioning signals are used for determining the position information of the electronic equipment in the satellite positioning scene, and are used for determining the target communication satellite in the satellite communication scene.
A third aspect of the present application provides a communication control method, including:
the method comprises the steps that connection between a first radio frequency circuit and an antenna is conducted under a target scene, so that the first radio frequency circuit receives satellite positioning signals through the antenna, and the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene;
Determining the position information of the electronic equipment according to the satellite positioning signals in the satellite positioning scene;
and under the satellite communication transmitting scene, determining a target communication satellite according to the satellite positioning signal, and under the condition that the target communication satellite is determined, controlling the disconnection of the connection between the first radio frequency circuit and the antenna and controlling the connection of the second radio frequency circuit to the antenna, so that the second radio frequency circuit transmits the satellite communication signal to the target communication satellite.
A fourth aspect of the present application provides a communication system comprising a plurality of satellites, a master station and an electronic device as described above;
wherein the target communication satellite is one of the plurality of satellites; the satellite communication signals carry call information; the electronic equipment is used for carrying out satellite communication with the master control station through the target communication satellite.
A fifth aspect of the present application provides a computer device comprising:
a memory storing a computer program and a processor implementing the steps of the communication control method as described above when the processor executes the computer program.
A sixth aspect of the present application provides a computer-readable storage medium having stored thereon a computer program which, when executed by a processor, implements the steps of the communication control method as described above.
According to the electronic equipment, the communication system, the communication control method, the computer equipment and the computer readable storage medium, the function matching under different scenes is realized by realizing the switching control of the connection states between different radio frequency circuits and the antennas under different scenes, and meanwhile, the connection between the first radio frequency circuit and the antennas can be timely disconnected when the second radio frequency circuit is in the transmitting state, so that the problems of channel blocking and even device damage caused by the transmission of satellite communication signals of the first radio frequency circuit are avoided. Therefore, the protection of the radio frequency channel can be realized on the basis of realizing the satellite communication and satellite positioning functions, and the overall reliability, safety and stability are improved, so that the product yield is improved, and the customer return rate, the maintenance rate and the complaint rate are reduced. Meanwhile, the electronic equipment has simple structure and low cost, and can realize large-scale production.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is one of the block diagrams of an electronic device according to an embodiment;
FIG. 2 is a second block diagram of an electronic device according to an embodiment;
FIG. 3 is a third block diagram of an electronic device according to an embodiment;
FIG. 4 is a fourth block diagram of an electronic device of an embodiment;
FIG. 5 is a fifth block diagram of an electronic device according to an embodiment;
FIG. 6 is a sixth block diagram of an electronic device according to an embodiment;
FIG. 7 is a block diagram of an electronic device according to an embodiment;
FIG. 8 is one of the flow charts of the communication control method of an embodiment;
FIG. 9 is a second flowchart of a communication control method according to an embodiment;
fig. 10 is a schematic diagram of a scenario of a communication system according to an embodiment.
Detailed Description
In order to make the objects, technical solutions and advantages of the present application more apparent, the present application will be further described in detail with reference to the accompanying drawings and examples. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the present application.
It will be understood that the terms "first," "second," and the like, as used herein, may be used to describe various elements, but these elements are not limited by these terms. These terms are only used to distinguish one element from another element and should not be construed as indicating or implying a relative importance or number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In the description of the present application, the meaning of "plurality" is at least two, such as two, three, etc., unless explicitly defined otherwise. It will be understood that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present.
In the field of communications, in order to support network coverage of different operators, antennas supporting up to ten frequency bands are often required on a metal frame of an electronic device. Such as LTE low, medium and high frequency antennas; an antenna of NR 5G such as a new frequency n78, n79, etc. or a spectrum re-cultivation frequency n1, n3, n7, etc.; WIFI/GPS/NFC antennas for short-range communications, etc. Therefore, the layout space of the antennas in the electronic equipment is more and more limited, and on the basis of ensuring that the transmission and reception performance indexes of each antenna are all compliant, the isolation between the antennas is difficult to ensure, so that the risk of blocking a potential passage or damaging a device is avoided. Based on this, in order to improve the problems of via blocking and via device damage, the present application provides an electronic apparatus, a communication system, a communication method, a computer apparatus, and a computer storage medium.
The electronic device according to the embodiments of the present application has a satellite positioning function and a satellite communication function, and may be a handheld device, a vehicle-mounted device, a smart car, a wearable device, a computing device or other processing devices connected to a wireless modem, and various forms of User Equipment (UE) (e.g., a Mobile phone), a Mobile Station (MS), and so on. For convenience of description, the above-mentioned devices are collectively referred to as electronic devices.
The electronic device of the embodiment of the application may be applied to a communication system, where the communication system may include a plurality of satellites, a master control station and an electronic device, where the electronic device may perform satellite communication with the master control station through a target communication satellite in the plurality of satellites, for example, the master control station may perform a related operation or a related feedback based on the call information by transmitting a satellite communication signal carrying the call information to the master control station through the target communication satellite, and the master control station may be, for example, a base station; the electronic equipment can also position and navigate the electronic equipment through a plurality of satellites, so that the multifunctional coverage is realized.
Fig. 1 is a block diagram of an electronic device according to an embodiment, referring to fig. 1, in this embodiment, the electronic device includes: the first rf circuit 10, the second rf circuit 20 and the control circuit (in the figure, the antennas that are connected by conducting the first rf circuit 10 and the second rf circuit 20 are shown as examples, such as ANT1 and ANT2 in the figure, which are not limiting, meanwhile, only the connection state between the first rf circuit 10 and the second rf circuit 20 and the antennas is shown at a certain moment, the control circuit is not shown, the dotted line represents that the connection between the rf circuit and the antennas is in the disconnection state at the moment, and the solid line represents that the connection between the rf circuit and the antennas is in the conduction state at the moment).
A first radio frequency circuit 10 for supporting reception of satellite positioning signals when connected to the antenna in a conductive manner; a second radio frequency circuit 20 for supporting transmission of satellite communication signals to a target communication satellite when connected to the antenna in a conductive manner; the control circuit is respectively connected with the first radio frequency circuit 10 and the second radio frequency circuit 20 and is used for controlling connection and conduction between the first radio frequency circuit 10 and the antenna under a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; and the electronic device is further used for determining the position information of the electronic device according to the satellite positioning signal in a satellite positioning scene, determining a target communication satellite in a satellite communication scene, controlling the connection between the first radio frequency circuit 10 and the antenna to be disconnected, and controlling the connection between the second radio frequency circuit 20 and the antenna to be conducted.
When the first radio frequency circuit 10 is connected to the antenna in a conductive manner, both the satellite communication transmission scene and the satellite positioning scene can support the reception of satellite positioning signals to assist positioning and searching satellites, specifically, in the satellite communication transmission scene, the satellite positioning signals can be used for a control circuit to determine a target communication satellite in a plurality of satellites, so that the electronic equipment performs satellite communication with the target communication satellite; in a satellite positioning scene, the satellite positioning signals can be used for a control circuit to determine the current position information of the electronic equipment so as to realize positioning and navigation functions.
Optionally, according to different usage scenarios of the user, the geographic area in which the electronic device is located may be different, and the visible satellites corresponding to different areas may be different, so the control circuit may determine the current position information of the electronic device according to the satellite positioning signal in the satellite positioning scenario, then determine the visible satellites in the target area according to the current position information, and then control the visible satellites in the target area of the first radio frequency circuit 10 to search for satellites during the satellite communication transmission scenario, so as to improve the efficiency of determining the target communication satellite.
Optionally, the satellite positioning signal may carry a data packet of satellite position information, and the control circuit may obtain position information of each satellite based on the data packet, determine distance information between the electronic device and each satellite according to the position information, and so on, so as to determine the target communication satellite and calculate current position coordinates of the electronic device according to the distance information corresponding to the plurality of satellites, so as to obtain current position information of the electronic device.
Wherein the second rf circuit 20, when in conductive connection to the antenna, supports transmitting satellite communication signals to the target communication satellite for communication with the target communication satellite. The satellite communication signal may, for example, carry call information to communicate with the master station via the target communication satellite. The satellite communication coverage capability is strong, and is not limited by the geographical environment, the climate condition and the time, so that the electronic device in the embodiment is integrated with the satellite communication function through the second radio frequency circuit 20, and the requirements of users can be met.
The control circuit is connected with the first radio frequency circuit 10 and the second radio frequency circuit 20 respectively, and based on the first radio frequency circuit 10 and the second radio frequency circuit 20, the control circuit can realize related control functions, auxiliary satellite searching functions, positioning functions and satellite communication functions:
on the one hand, the control circuit may determine the current scene type based on the received communication instruction, so as to implement the related control function according to the scene type, so as to control the connection states between the first radio frequency channel, the second radio frequency channel and the antenna respectively, specifically, whether in the satellite communication transmission scene or the satellite positioning scene, the first radio frequency circuit 10 may be controlled to be connected to the antenna in a conducting manner, the first radio frequency circuit 10 may be controlled to be disconnected from the antenna in the satellite communication transmission scene, and then the second radio frequency circuit 20 may be controlled to be connected to the antenna in a conducting manner, thereby, function matching under different scenes may be implemented, and meanwhile, the connection between the first radio frequency circuit 10 and the antenna may be timely disconnected when the second radio frequency circuit 20 is in the transmission state, so that the problems of channel blockage and even device damage caused by the transmission of the satellite communication signal by the first radio frequency circuit 10 are avoided, and the safety and stability of the circuit are improved.
On the other hand, the control circuit can also realize relevant auxiliary satellite searching function, positioning function and communication function based on the received satellite positioning signal, specifically, in the satellite communication transmission scene, the control circuit can determine a target communication satellite based on the satellite positioning signal so as to support the auxiliary satellite searching function together with the first radio frequency circuit 10; under the satellite communication emission scene, the control circuit also realizes communication connection with a target communication satellite based on a satellite communication signal, and then can realize communication connection with a main control station based on the target communication satellite, so that a communication function can be realized; in a satellite positioning scene, the control circuit can determine the current position information of the electronic equipment based on satellite positioning signals, so that the positioning navigation function can be realized.
It will be appreciated that the satellite communication signal of the second rf circuit 20 is adjacent to the frequency band of the satellite positioning signal of the first rf circuit 10, and the satellite communication signal is usually transmitted with high power, so that when the second rf circuit 20 transmits the satellite communication signal, the generated interference signal easily falls near the operating frequency band of the first rf circuit 10, and if no protection measures are taken, the interference will be blocked on the path where the first rf circuit 10 is located, and even the internal devices of the first rf circuit 10 are damaged. Jamming interference may be understood as the blocking of the receiver of the first radio frequency circuit 10 by satellite communication signals to demodulate satellite positioning signals.
The electronic device of the embodiment, through the first radio frequency circuit 10, the second radio frequency circuit 20 and the control circuit, can realize the switching control of the connection states between different radio frequency circuits and the antenna under different scenes, and realize the function matching under different scenes, and meanwhile, the first radio frequency circuit 10 can be disconnected with the antenna in time when the second radio frequency circuit 20 is in the transmitting state, so that the problems of channel blocking and even device damage caused by the transmission of satellite communication signals of the first radio frequency circuit 10 are avoided, and the safety and stability of the circuit are improved. Therefore, the electronic equipment of the embodiment can realize the protection of the radio frequency channel on the basis of realizing the satellite communication and satellite positioning functions, and improve the overall reliability, safety and stability, thereby improving the product yield, and reducing the customer return rate, the maintenance rate and the complaint rate, so as to improve the user experience. Meanwhile, the electronic equipment has simple structure and low cost, and can realize large-scale production.
In one embodiment, as shown in fig. 2, the electronic device further comprises a switching circuit 30.
The switch circuit 30 is respectively connected to the control circuit 40 (connection lines between the switch circuit 30 and the control circuit 40 are not shown in the figure), the first rf circuit 10, the second rf circuit 20, and the antenna, and is configured to switch the on-off state between each rf circuit and the antenna under the control of the control circuit 40.
The controlled end of the switch circuit 30 is connected to the control circuit 40, two first ends of the switch circuit 30 are respectively connected to the first rf circuit 10 and the second rf circuit 20, and the second end of the switch circuit 30 is connected to the antenna, so that the switch circuit 30 can switch the on-off state between each rf circuit and the antenna according to the control signal of the control circuit 40. Specifically, in a target scene, connection between a first radio frequency channel and an antenna is conducted; in the case of a satellite positioning scenario and a target communication satellite is determined, the connection between the first radio frequency circuit 10 and the antenna is disconnected and the connection between the second radio frequency circuit 20 and the antenna is turned on. Therefore, the control circuit 40 can assist to control the on-off states of the first radio frequency circuit 10, the second radio frequency circuit 20 and the antenna through the switch circuit 30, and on the basis of realizing function matching under different scenes and lower hardware cost, the problems of blocking a passage and even damaging devices caused by the transmission of satellite communication signals of the first radio frequency circuit 10 are avoided, and the safety, stability and reliability of the circuit are improved.
Alternatively, the switch circuit 30 may be connected to one antenna, so that the first rf circuit 10 and the second rf circuit 20 are respectively connected to the same antenna in a conductive manner at different times, so as to support the reception of satellite positioning signals and the transmission of satellite communication signals by the same antenna. Optionally, the switch circuit 30 may be connected to multiple antennas, and the first rf circuit 10 and the second rf circuit 20 may support conducting connection to the same antenna or different antennas at different times (fig. 2 illustrates connection to different antennas for illustration, but not limitation), so as to support receiving satellite positioning signals and transmitting satellite communication signals through the same or different antennas.
In one embodiment, as shown in fig. 3, the switching circuit 30 is connected to a first antenna (ANT 1 in the figure) and a second antenna (ANT 2 in the figure), and the switching circuit 30 includes: a first switch module 310 and a second switch module 320.
The first switch module 310 is respectively connected with the control circuit 40 (connection lines between each switch module and the control circuit 40 are not shown in the figure), the first radio frequency circuit 10 and the first antenna, and is used for conducting connection between the first radio frequency circuit 10 and the first antenna in a satellite communication transmission scene, and is also used for disconnecting connection between the first radio frequency circuit 10 and the first antenna in a satellite communication transmission scene and in a situation that the control circuit 40 determines a target communication satellite; the second switch module 320 is connected to the control circuit 40, the second rf circuit 20, and the second antenna, and is configured to conduct connection between the second rf circuit 20 and the second antenna when the satellite communication transmits a scene and the first switch module 310 disconnects the connection between the first rf circuit 10 and the first antenna.
The first switch module 310 is disposed on a connection path between the first rf circuit 10 and the first antenna, and the connection between the first rf circuit 10 and the first antenna can be controlled by controlling the on-off condition of the first switch module 310. The second switch module 320 is disposed on a connection path between the second rf circuit 20 and the second antenna, and the connection between the second rf circuit 20 and the second antenna can be controlled by controlling the on/off condition of the second switch module 320. By arranging the first switch module 310 and the second switch module 320, each switch module is arranged on the connection path between each radio frequency circuit and the antenna, so that the on and off conditions of each switch module can be independently controlled, and the radio frequency path can be switched more accurately. Alternatively, each switching module comprises a switching device, which may be, for example, a single pole single throw switch.
Alternatively, the control circuit 40 may output a first control signal to the first switch module 310 and the second switch module 320 to control the first switch module 310 and the second switch module 320 to be in a conductive state, respectively, and may output a second control signal to the first switch module 310 and the second switch module 320 to control the first switch module 310 and the second switch module 320 to be in an off state, respectively. Optionally, the control circuit 40 may be configured with a control interface, where the control interface includes one of a mipi (Mobile Industry Processor Interface ) interface and a GPIO (General Purpose Input Output, general purpose input/output) interface, and the control circuit 40 may send the first control signal and the second control signal to each switch module through level change control of the mipi interface or the GPIO interface, thereby improving control efficiency.
In one embodiment, as shown in fig. 4, the first switch module 310 is further connected to the ground plane (connection state of the control circuit and the switch circuit is not shown in the figure), and is further configured to conduct the connection between the first antenna and the ground plane in the case where the satellite communication transmission scenario is the satellite communication transmission scenario and the control circuit 40 determines the target communication satellite, so that when the second radio frequency circuit 20 transmits the satellite communication signal, the interference energy possibly received by the first antenna is released to the ground, so as to further ensure that the first radio frequency circuit 10 is not affected by the satellite communication signal transmitted by the second radio frequency circuit 20, and at the same time ensure that when the first radio frequency circuit 10 is subsequently connected to the first antenna in a re-conduction manner, the interference energy remains; in addition, under the condition of satellite communication scene, the first antenna is grounded, and the environment near the second antenna can be purer, so that the directivity of the second antenna when transmitting communication signals is more concentrated, the antenna efficiency is higher, and the test value of TRP (Total Radiated Power, omnidirectional radiation power)/TIS (Total Isotropic Sensitivity, omnidirectional radiation sensitivity) is higher. Alternatively, the first switch module 310 may be a single pole double throw switch, thereby implementing a selective switching function between conducting the first antenna to the first radio frequency circuit 10 and to the ground plane. Alternatively, the first switching module 310 may be connected to the ground plane through an impedance matching of 50Ω, so that interference energy may be transferred to the ground in the circuit with maximum power, thereby reducing the residue of interference energy.
In one embodiment, as shown in fig. 5, the first radio frequency circuit 10 includes: a first filtering module 110, a low noise amplifying module 120 and a second filtering module 130.
The first filtering module 110 is connected to the switch circuit 30, and is configured to perform filtering processing on the satellite positioning signal received by the antenna when the first filtering module is connected to the antenna in a conducting manner; the low-noise amplification module 120 is connected with the first filtering module 110, and is used for performing low-noise amplification on the satellite positioning signal filtered by the first filtering module 110; the second filtering module 130 is connected to the low noise amplifying module 120 and the control module, respectively, and is configured to perform filtering processing on the satellite positioning signal subjected to the low noise amplifying processing.
The first filtering module 110 and the second filtering module 130 are respectively configured to perform filtering processing on the received signals, specifically, the first filtering module 110 is configured to perform primary filtering processing on the received satellite positioning signals, and the second filtering module 130 is configured to perform secondary filtering processing on the received satellite positioning signals, so that the sensitivity and accuracy of the satellite positioning signals can be improved through dual filtering processing, and the accuracy of satellite positioning and target communication satellite determination can be improved. The low noise amplifier is connected to the first filtering module 110 and the second filtering module 130, and is configured to perform low noise amplification on the satellite positioning signal after the primary filtering process of the first filtering module 110, and output the satellite positioning signal to the second filtering module 130. Thus, the first filtering module 110, the low noise amplifying module 120 and the second filtering module 130 implement receiving processing of the satellite positioning signal. Alternatively, each filtering module may include a filter (SAW, surface Acoustic Wave Filter), and the low noise amplifying module 120 may include a low noise amplifier (LAN, low Noise Amplifier).
In the related art, the sustainable power range of the filter and the low noise amplifier is generally small, for example, the sustainable power range of the filter is 13dbm, and the sustainable power range of the low noise amplifier is 10dbm; the transmission power of the satellite communication signal is usually larger than the tolerable power range of the filtering module, for example, 36dbm may be reached, so that if no protection measures are taken, the filter and the low noise amplifier may be damaged during the transmission of the satellite communication signal. The on-off state of each radio frequency circuit and each antenna is switched based on the control circuit 40 and the switch circuit 30, so that the potential damage risk of the filter and the low-noise amplifier can be effectively avoided.
In one embodiment, the number of first rf circuits 10 is plural, or the electronic device also includes other rf circuits. Taking the plurality of first rf circuits 10 as an example, the electronic device may further include a combining module connected to the switch circuit 30 and the plurality of first rf circuits 10, respectively, for performing a combining process on the satellite positioning signals received by the antenna when the antenna is connected to the antenna, and outputting the satellite positioning signals to each of the first rf circuits 10 correspondingly.
The combining module may perform a combining processing function (it may be understood that, when receiving a signal, the combining processing function may be understood as splitting the received signal to obtain signals in different frequency bands) so as to respectively and correspondingly transmit the obtained signals in different frequency bands to each first radio frequency circuit 10, and on the other hand, the bearable power range of the combining module is generally higher than that of the filtering module, and by setting the combining module located at the front end (near the antenna side), suppression of interference blocking may be further implemented, for example, the combining module may be 16dbm and may suppress 3dbm.
In one embodiment, the second radio frequency circuit 20 includes: and the power amplification module is used for receiving the satellite communication signals to be transmitted, carrying out power amplification processing on the satellite communication signals and outputting the satellite communication signals to the antenna which is connected in a conducting mode. The Power amplification module may include a Power Amplifier (PA) or other functional devices to implement other auxiliary functions, for example, a low noise amplifier to implement a receiving function at the same time. When the power amplification module further includes a low noise amplifier, the power amplification module may be a power amplifier module (L-pa·mid, pa·mid With LNA) With a built-in low noise amplifier, or may be a power amplifier switching module (LPAF, LNA-PA ASM module With integrated filter) With a filter and a low noise amplifier integrated therein.
In one embodiment, as shown in fig. 6, the control circuit 40 includes: a radio frequency transceiver 410 and a control module 420.
The radio frequency transceiver 410 is connected to the first radio frequency circuit 10 and the second radio frequency circuit 20, and is configured to receive the satellite positioning signal received and processed by the first radio frequency circuit 10, and output a satellite communication signal to be transmitted to the second radio frequency circuit 20; the control module 420 is connected with the radio frequency transceiver 410, and is used for determining a target scene according to the received control instruction, and controlling the on-off state of the switch circuit 30 according to the target scene; the method comprises the steps of analyzing satellite positioning signals received by the radio frequency transceiver 410 according to control instructions to determine a target communication satellite or determine current position information of the electronic equipment; and is further configured to control the rf transceiver 410 to output satellite communication signals according to the control instruction in case the target communication satellite is determined.
The radio frequency transceiver 410 is configured to implement a transceiving process, and may include a receiver for receiving a signal and a transmitter for outputting a signal to be transmitted, and specifically, the receiver of the radio frequency transceiver 410 may be connected to a receiving output end of the first radio frequency circuit 10 and the control module 420, respectively, so as to receive a satellite positioning signal received by the first radio frequency circuit 10, and output satellite positioning to the control module 420; the transmitter of the rf transceiver 410 may be respectively connected to the transmission input terminal of the second rf circuit 20 and the control module 420, so as to output the satellite communication signal output by the control module 420 to the second rf circuit 20.
The control module 420 is connected to the radio frequency transceiver 410, and the control module 420 can receive a control instruction input by a user, and can also obtain a working state of each radio frequency circuit and related radio frequency signals based on the radio frequency transceiver 410, and realize direct control or indirect control on the on-off state of the switch circuit according to the related control instruction. For example, the control module 420 may be connected to the switching circuit to directly control the on-off state of the switching circuit; for example, the control module 420 may be connected to the switch circuit through the rf transceiver 410, and the control module 420 may instruct the rf transceiver 410 to control the on-off state of the switch circuit by outputting a control command to the rf transceiver 410.
Alternatively, the control module 420 may include a satellite communication baseband processor, a radio frequency baseband processor (Modem), a central Controller (CPU), and the like, where the satellite communication baseband processor and the radio frequency baseband processor are respectively connected to the CPU and also respectively connected to the radio frequency transceiver 410. Alternatively, the satellite communication baseband processor and the radio frequency baseband processor may be used to perform conversion and inverse conversion processes of the digital signal to the radio frequency signal, respectively, including packaging and framing of the digital signal, conversion, modulation, up-conversion, etc. of the digital signal, or send the received signal to the CPU through a series of inverse processes. The inverse process may include down conversion, demodulation, conversion of analog-to-digital signals, de-encapsulation, etc. Optionally, the satellite communication baseband processor can receive a satellite communication instruction input by a user and synchronize the instruction to the CPU, the CPU can issue the instruction to the radio frequency baseband processor to control the switch circuit 30 to conduct connection between the first radio frequency circuit 10 and the antenna, the satellite communication baseband processor receives a satellite positioning signal through the radio frequency transceiver 410, further determines a target communication satellite based on the satellite positioning signal, and feeds back the target communication satellite to the CPU, and the CPU can issue the instruction to the radio frequency baseband processor to control the switch circuit 30 to disconnect the connection between the first radio frequency circuit 10 and the antenna, and control the switch circuit 30 to conduct connection between the second radio frequency circuit 20 and the antenna after the connection is disconnected, so as to perform satellite communication.
The current target scene can be determined in time through the interaction between the control module 420 and the radio frequency transceiver 410, and the on-off state switching between each radio frequency circuit and the antenna is realized based on the target scene, so that the internal devices of the first radio frequency circuit 10 are protected on the basis of realizing the satellite positioning function and the satellite communication function, the problems of channel blocking and device damage are avoided, and the whole normal operation of the electronic equipment is ensured.
In one embodiment, the control module 420 may control the switch circuit 30 to conduct the connection between the first rf circuit 10 and the antenna to enable the first rf circuit 10 to continue receiving the satellite positioning signal when determining that the satellite communication scenario is over. Alternatively, the satellite communication baseband processor in the control circuit 40 may determine whether to end satellite communication currently according to a user instruction, and in the case of determining to end satellite communication, feedback the end information to the CPU, so that the CPU may issue an instruction to the radio frequency baseband processor to control the switch circuit 30 to conduct the connection between the first radio frequency circuit 10 and the antenna.
In one embodiment, the control module 420 is further configured to obtain distance information between each satellite and the electronic device according to satellite positioning signals from each satellite, and determine a target communication satellite according to the distance information, where the target communication satellite is a satellite closest to the electronic device. Therefore, the control module 420 can select the satellite closest to the electronic device based on the distance information and communicate with the satellite, which is beneficial to reducing the transmitting power when the second radio frequency circuit 20 transmits satellite communication signals, thereby further weakening the influence on the first radio frequency circuit 10 on the basis of ensuring the satellite communication quality, and simultaneously being beneficial to reducing the overall power consumption of the second radio frequency circuit 20.
In one embodiment, the control module 420 is further configured to determine a target communication satellite according to each satellite positioning signal, where the target communication satellite is a satellite corresponding to the satellite positioning signal with the greatest signal strength. The intensity of the satellite positioning signal is inversely proportional to the distance between the satellite and the electronic device, and the greater the intensity, the closer the satellite is to the electronic device, so that when the satellite corresponding to the satellite positioning signal with the largest signal intensity is the satellite closest to the electronic device, the control module 420 can directly determine the target communication satellite according to the intensity of the satellite positioning signal, which is beneficial to improving the confirmation efficiency of the target communication satellite and further improving the overall satellite communication efficiency.
In one embodiment, the first rf circuit 10 may be a global positioning system (Global Positioning System, GPS) circuit, and the satellite positioning signals may be GPS satellite positioning signals, so that the control circuit 40 may utilize the GPS satellite positioning signals to assist in positioning satellites to determine the target communication satellite; on the other hand, the GPS signals can be directly utilized to locate and navigate the electronic equipment in real time in the global scope. It can be understood that the technical solution of the present application is not limited to GPS circuits with high risk, and other radio frequency paths such as LTE/NR/WIFI/NFC are also applicable, especially antennas with high risk of isolation from satellite communication antennas in antenna design.
Fig. 7 is a block diagram of an electronic device according to an embodiment, and referring to fig. 7, in this embodiment, the electronic device includes: a first radio frequency circuit 10, a second radio frequency circuit 20 and a switching circuit 30.
A first radio frequency circuit 10 for supporting reception of satellite positioning signals when connected to the antenna in a conductive manner; a second radio frequency circuit 20 for supporting transmission of satellite communication signals to a target communication satellite when connected to the antenna in a conductive manner; the switch circuit 30 is respectively connected with the first radio frequency circuit 10, the second radio frequency circuit 20 and the antenna, and is used for conducting connection between the first radio frequency circuit 10 and the antenna in a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; and the antenna is further used for disconnecting the first radio frequency circuit 10 from the antenna and conducting the second radio frequency circuit 20 from the antenna under the condition of satellite positioning and determining a target communication satellite; the satellite positioning signals are used for determining the position information of the electronic equipment in a satellite positioning scene, and are used for determining the target communication satellite in a satellite communication scene.
For the description of the first rf circuit 10, the second rf circuit 20 and the switch circuit 30, reference is made to the above embodiments, and the description thereof is omitted herein.
According to the electronic equipment, through the first radio frequency circuit 10, the second radio frequency circuit 20 and the switch circuit 30, switching control of connection states between different radio frequency circuits and antennas can be achieved under different scenes, functional matching under different scenes is achieved, meanwhile, the first radio frequency circuit 10 can be disconnected with the antennas in time when the second radio frequency circuit 20 is in a transmitting state, and therefore the problems of channel blocking and even device damage caused by satellite communication signals of the first radio frequency circuit 10 are avoided, and safety and stability of the circuit are improved. Therefore, the electronic equipment of the embodiment can realize the protection of the radio frequency channel on the basis of realizing the satellite communication and satellite positioning functions and low hardware cost, and improves the overall reliability, safety and stability, thereby improving the product yield, and reducing the customer return rate, maintenance rate and complaint rate, so as to improve the user experience. Meanwhile, the electronic equipment has simple structure and low cost, and can realize large-scale production.
In one embodiment, the electronic device further comprises: the control circuit is respectively connected with the first radio frequency circuit, the second radio frequency circuit and the switch circuit and is used for controlling the switch circuit to connect the first radio frequency circuit to the antenna in a conducting manner under a target scene, wherein the target scene comprises at least one of a satellite communication transmitting scene and a satellite positioning scene; the electronic device is also used for determining the position information of the electronic device according to the satellite positioning signals in a satellite positioning scene, determining a target communication satellite in a satellite communication scene, controlling the switch circuit to disconnect the first radio frequency circuit from the antenna, and controlling the switch circuit to conduct the connection between the second radio frequency circuit and the antenna. For a description of the control circuit, reference is made to the above embodiments, and details thereof are omitted herein.
Fig. 8 is a flowchart of a communication control method according to an embodiment, which can be applied to the above-mentioned electronic device, and the related description of the electronic device is referred to in the previous embodiment, and is not repeated herein. Referring to fig. 8, in the present embodiment, the communication control method includes steps 802 to 806.
Step 802, connecting the first radio frequency circuit and the antenna under a target scene, so that the first radio frequency circuit receives satellite positioning signals through the antenna, and the target scene comprises at least one of a satellite communication transmitting scene and a satellite positioning scene.
In step 804, in the satellite positioning scenario, the location information of the electronic device is determined according to the satellite positioning signal.
Step 806, in the satellite communication transmitting scenario, determining a target communication satellite according to the satellite positioning signal, and in the case of determining the target communication satellite, controlling the connection between the first radio frequency circuit and the antenna to be disconnected, and controlling the second radio frequency circuit to be connected to the antenna in a conducting manner, so that the second radio frequency circuit transmits the satellite communication signal to the target communication satellite.
In one embodiment, referring to fig. 9, in this embodiment, a first rf path may be conductively connected to a first antenna, a second rf path may be conductively connected to a second antenna, and the communication control method includes steps 902-906.
Step 902, connecting the first radio frequency circuit and the first antenna under a target scene, so that the first radio frequency circuit receives a satellite positioning signal through the first antenna, and the target scene comprises at least one of a satellite communication transmitting scene and a satellite positioning scene.
In step 904, in the satellite positioning scenario, location information of the electronic device is determined according to the satellite positioning signal.
Step 906, in the satellite communication transmitting scenario, determining a target communication satellite according to the satellite positioning signal, and controlling the first antenna to be switched from conductive connection with the first radio frequency channel to conductive connection with the ground plane and controlling the second radio frequency circuit to be conductive connected to the second antenna under the condition that the target communication satellite is determined.
The communication control method of the present embodiment may be executed by the control circuit in the related embodiment of the electronic device, and the related description may refer to the related description of the electronic device, which is not repeated herein.
According to the communication control method, through switching control of connection states between different radio frequency circuits and antennas in different scenes, function matching in different scenes is achieved, meanwhile, the first radio frequency circuit can be disconnected with the antennas in time when the second radio frequency circuit is in a transmitting state, and therefore the problem that a channel is blocked and even devices are damaged due to satellite communication signals of the first radio frequency circuit is avoided. Therefore, the protection of the radio frequency channel can be realized on the basis of realizing the satellite communication and satellite positioning functions, and the reliability, the safety and the stability of the whole device are improved.
It should be understood that, although the steps in the flowcharts are shown in order as indicated by the arrows, the steps are not necessarily performed in order as indicated by the arrows. The steps are not strictly limited to the order of execution unless explicitly recited herein, and the steps may be executed in other orders. Moreover, at least some of the steps in the flowcharts may include a plurality of sub-steps or stages that are not necessarily performed at the same time, but may be performed at different times, and the order of execution of the sub-steps or stages is not necessarily sequential, but may be performed in rotation or alternately with at least a portion of the sub-steps or stages of other steps or other steps.
The embodiment of the application also provides a communication system, referring to fig. 10, the communication system includes a plurality of satellites, a master control station (a in the figure) and the electronic device (B in the figure) of the above embodiment; wherein the target communication satellite (C in the figure) is one of a plurality of satellites; the satellite communication signals carry call information; the electronic equipment is used for carrying out satellite communication with the master control station through the target communication satellite. For the description of the satellite, the master station and the electronic device, reference is made to the above embodiments, and details thereof are not repeated here. In the present embodiment, based on the foregoing electronic apparatus, a secure and reliable communication system can be provided.
The embodiment of the application also provides a computer device, which comprises: the computer program comprises a memory and a processor, wherein the memory stores a computer program, and the processor realizes the steps of the communication control method when executing the computer program.
The embodiment of the application also provides a computer readable storage medium, on which a computer program is stored, characterized in that the computer program, when executed by a processor, implements the steps of the communication control method as above.
Any reference to memory, storage, database, or other medium used herein may include non-volatile and/or volatile memory. Suitable nonvolatile memory can include Read Only Memory (ROM), programmable ROM (PROM), electrically Programmable ROM (EPROM), electrically Erasable Programmable ROM (EEPROM), or flash memory. Volatile memory can include random access memory (RM), which acts as external cache memory. By way of illustration and not limitation, RMs are available in a variety of forms, such as Static RMs (SRMs), dynamic RMs (DRMs), synchronous DRMs (SDRMs), double data rates SDRM (DDR SDRM), enhanced SDRMs (ESDRMs), synchronous link (synchronous) DRMs (SLDRMs), memory bus (Rmbus) direct RMs (RDRMs), direct memory bus dynamic RMs (DRDRMs), and memory bus dynamic RMs (RDRMs).
The technical features of the above embodiments may be arbitrarily combined, and all possible combinations of the technical features in the above embodiments are not described for brevity of description, however, as long as there is no contradiction between the combinations of the technical features, they should be considered as the scope of the description. The foregoing examples represent only a few embodiments of the present application, which are described in more detail and are not thereby to be construed as limiting the scope of the present application. It should be noted that it would be apparent to those skilled in the art that various modifications and improvements could be made without departing from the spirit of the present application, which would be within the scope of the present application. Accordingly, the scope of protection of the present application is to be determined by the claims appended hereto.

Claims (15)

1. An electronic device, comprising:
the first radio frequency circuit is used for supporting the reception of satellite positioning signals when being connected to the antenna in a conducting manner;
the second radio frequency circuit is used for supporting to transmit satellite communication signals to a target communication satellite when being connected to the antenna in a conducting mode;
the control circuit is respectively connected with the first radio frequency circuit and the second radio frequency circuit and is used for controlling connection and conduction between the first radio frequency circuit and the antenna under a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; and the electronic equipment is also used for determining the position information of the electronic equipment according to the satellite positioning signals in the satellite positioning scene, determining the target communication satellite in the satellite communication scene, controlling the connection between the first radio frequency circuit and the antenna to be disconnected, and controlling the connection between the second radio frequency circuit and the antenna to be conducted.
2. The electronic device of claim 1, further comprising:
and the switch circuit is respectively connected with the control circuit, the first radio frequency circuit, the second radio frequency circuit and the antenna and is used for switching the on-off state between each radio frequency circuit and the antenna under the control of the control circuit.
3. The electronic device of claim 2, wherein the switching circuit comprises:
the first switch module is respectively connected with the control circuit, the first radio frequency circuit and the first antenna, and is used for conducting connection between the first radio frequency circuit and the first antenna in the satellite communication transmission scene and disconnecting the connection between the first radio frequency circuit and the first antenna in the satellite communication transmission scene and under the condition that the control circuit determines the target communication satellite;
the second switch module is respectively connected with the control circuit, the second radio frequency circuit and the second antenna and is used for conducting connection between the second radio frequency circuit and the second antenna under the condition that the first switch module breaks connection between the first radio frequency circuit and the first antenna in the satellite communication transmission scene.
4. The electronic device of claim 3, wherein the first switch module is further coupled to a ground plane and further configured to conduct a connection between the first antenna and the ground plane if the satellite communication transmission scenario and the control circuit determines the target communication satellite.
5. The electronic device of claim 2, wherein the first radio frequency circuit comprises:
the first filtering module is connected with the switch circuit and is used for filtering the satellite positioning signals received by the antenna when the first filtering module is connected to the antenna in a conducting manner;
the low-noise amplification module is connected with the first filtering module and is used for carrying out low-noise amplification processing on the satellite positioning signals after the filtering processing of the first filtering module;
and the second filtering module is respectively connected with the low-noise amplifying module and the control module and is used for filtering the satellite positioning signals subjected to low-noise amplifying processing.
6. The electronic device of claim 2, wherein the control circuit comprises:
the radio frequency transceiver is respectively connected with the first radio frequency circuit and the second radio frequency circuit, and is used for receiving the satellite positioning signals received and processed by the first radio frequency circuit and outputting the satellite communication signals to be transmitted to the second radio frequency circuit;
The control module is connected with the radio frequency transceiver and used for determining the target scene according to the received control instruction and controlling the on-off state of the switch circuit according to the target scene; the satellite positioning signal receiving module is used for analyzing the satellite positioning signal received by the radio frequency transceiver according to the control instruction so as to determine the target communication satellite or determine the current position information of the electronic equipment; and the radio frequency transceiver is also used for controlling the radio frequency transceiver to output the satellite communication signal according to the control instruction under the condition that the target communication satellite is determined.
7. The electronic device of claim 6, wherein the control module is further configured to obtain distance information of each satellite from the electronic device based on the satellite positioning signals from each satellite, and determine the target communication satellite based on the distance information, the target communication satellite being a satellite closest to the electronic device.
8. The electronic device of claim 6, wherein the control module is further configured to determine the target communication satellite according to each of the satellite positioning signals, the target communication satellite being a satellite corresponding to the satellite positioning signal with the greatest signal strength.
9. The electronic device of any of claims 1-8, wherein the satellite positioning signals comprise GPS signals.
10. An electronic device, comprising:
the first radio frequency circuit is used for supporting the reception of satellite positioning signals when being connected to the antenna in a conducting manner;
the second radio frequency circuit is used for supporting to transmit satellite communication signals to a target communication satellite when being connected to the antenna in a conducting mode;
the switch circuit is respectively connected with the first radio frequency circuit, the second radio frequency circuit and the antenna and is used for conducting connection between the first radio frequency circuit and the antenna in a target scene, wherein the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene; the satellite positioning device is also used for disconnecting the connection between the first radio frequency circuit and the antenna and conducting the connection between the second radio frequency circuit and the antenna under the condition that the satellite positioning scene is determined and the target communication satellite is determined;
the satellite positioning signals are used for determining the position information of the electronic equipment in the satellite positioning scene, and are used for determining the target communication satellite in the satellite communication scene.
11. A communication control method, characterized by comprising:
the method comprises the steps that connection between a first radio frequency circuit and an antenna is conducted under a target scene, so that the first radio frequency circuit receives satellite positioning signals through the antenna, and the target scene comprises at least one of a satellite communication emission scene and a satellite positioning scene;
determining the position information of the electronic equipment according to the satellite positioning signals in the satellite positioning scene;
and under the satellite communication transmitting scene, determining a target communication satellite according to the satellite positioning signal, and under the condition that the target communication satellite is determined, controlling the disconnection of the connection between the first radio frequency circuit and the antenna and controlling the connection of the second radio frequency circuit to the antenna, so that the second radio frequency circuit transmits the satellite communication signal to the target communication satellite.
12. The communication control method of claim 11, wherein the first rf path is conductively connected to a first antenna and the second rf path is conductively connected to a second antenna; the communication control method further includes:
and under the satellite communication transmitting scene, determining a target communication satellite according to the satellite positioning signal, and under the condition that the target communication satellite is determined, controlling the first antenna to be switched from conducting connection with the first radio frequency channel to conducting connection with the ground plane and controlling the second radio frequency circuit to be conducting connected to the second antenna.
13. A communication system comprising a plurality of satellites, a master station and an electronic device as claimed in claims 1-10;
wherein the target communication satellite is one of the plurality of satellites; the satellite communication signals carry call information; the electronic equipment is used for carrying out satellite communication with the master control station through the target communication satellite.
14. A computer device, comprising:
a memory storing a computer program, and a processor implementing the steps of the communication control method according to any one of claims 11-12 when the processor executes the computer program.
15. A computer-readable storage medium, on which a computer program is stored, characterized in that the computer program, when being executed by a processor, implements the steps of the communication control method according to any one of claims 11-12.
CN202311873910.6A 2023-12-29 2023-12-29 Electronic device, communication system, communication control method, and computer device Pending CN117833948A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202311873910.6A CN117833948A (en) 2023-12-29 2023-12-29 Electronic device, communication system, communication control method, and computer device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202311873910.6A CN117833948A (en) 2023-12-29 2023-12-29 Electronic device, communication system, communication control method, and computer device

Publications (1)

Publication Number Publication Date
CN117833948A true CN117833948A (en) 2024-04-05

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Family Applications (1)

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Country Status (1)

Country Link
CN (1) CN117833948A (en)

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