WO2019019111A1 - Procédé de commande de simulation de vol, serveur et dispositif terminal - Google Patents
Procédé de commande de simulation de vol, serveur et dispositif terminal Download PDFInfo
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- WO2019019111A1 WO2019019111A1 PCT/CN2017/094733 CN2017094733W WO2019019111A1 WO 2019019111 A1 WO2019019111 A1 WO 2019019111A1 CN 2017094733 W CN2017094733 W CN 2017094733W WO 2019019111 A1 WO2019019111 A1 WO 2019019111A1
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- WIPO (PCT)
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- input device
- aircraft
- identification code
- system interface
- server
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
Definitions
- the invention relates to the technical field of simulation simulation software, in particular to a flight simulation control method, a server and a terminal device.
- a dedicated input device ie controller
- the user needs to practice the operation mode of the input device when using the software or participating in the game, thereby improving the learning cost of the user and reducing the user learning and entertainment experience.
- the invention provides a flight simulation control method, a server and a terminal device.
- a flight simulation control method configured on a server side, the method comprising:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- a flight simulation control method which is configured on a terminal device side, and the method includes:
- a flight simulation control method which is configured on a terminal device side, and the method includes:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- a server comprising a processor and a memory, the memory storing a number of instructions, the processor for reading an instruction from the memory to implement:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- a terminal device comprising a processor and a memory, the memory storing a plurality of instructions, the processor for reading an instruction from the memory to implement:
- a terminal device comprising a processor and a memory, the memory storing a plurality of instructions, the processor for reading an instruction from the memory to implement:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- a machine readable storage medium having stored thereon a plurality of computer instructions, the computer instructions being executed as follows:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- a machine readable storage medium having stored thereon a plurality of computer instructions, the computer instructions being executed as follows:
- a ninth aspect of the invention there is provided a machine readable storage medium having stored thereon a plurality of computer instructions that, when executed, perform the following processing:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- the present invention determines the corresponding system interface according to the identification code of the external input device, and maps the operations of the input device to the aircraft model according to the The operation of the operating button controls the motion of the aircraft in the system interface. It can be seen that the embodiment of the present invention can be applied to scenarios of multiple input devices, so that the user can use the familiar input device to perform game or flight simulation, thereby reducing the time cost of the learning operation mode. In addition, the user can also control the same terminal device with different input devices, simulate and control the flight of the aircraft, and get the real flight experience.
- FIG. 1 is an application scenario diagram of a flight simulation control method according to an embodiment of the present invention
- FIG. 2 is a schematic flow chart of a flight simulation control method according to an embodiment of the present invention.
- FIG. 3 is a schematic diagram of a system interface according to an embodiment of the present invention.
- FIG. 4 to FIG. 5 are schematic diagrams of an input device according to an embodiment of the present invention.
- FIG. 6 is a schematic structural diagram of a server according to an embodiment of the present invention.
- FIG. 7 is a schematic structural diagram of a terminal device according to an embodiment of the present invention.
- FIG. 8 is a schematic structural diagram of a terminal device according to another embodiment of the present invention.
- a dedicated input device ie controller
- the user participates in an aircraft simulation flight for one hour. Because the aircraft is not familiar with input devices during flight simulation (eg, aircraft remote control, keyboard, gamepad, etc.), a familiar process is required. After entering the device, the time has also arrived, resulting in a poor user experience.
- the user owns a device, and the aircraft simulation software or the aircraft entertainment game is newly added to the device. Since the device only has a keyboard, although the user can be familiar with the keyboard, the user does not feel the real feeling of driving the aircraft. At this time, if the device is compatible with the aircraft-made aircraft remote controller, the flight of the aircraft is controlled by the aircraft remote controller, and the user is experienced to enjoy the flight.
- FIG. 1 is an application scenario in which a terminal device 101 has a communication interface through which a communication interface can be used
- the input device 102 is in communication connection.
- the terminal device 101 is communicatively coupled to the server 104 via a local area network (LAN) or a wide area network (WAN) 103.
- the method can be applied to the terminal device 101 or the server 104, for example, by an application or software installed on the terminal device or the server.
- the terminal device may be a smart phone, a tablet computer or a control terminal.
- FIG. 2 is a schematic flow chart of a flight simulation control method according to an embodiment of the present invention. Referring to FIG. 2, the method is configured on the server, and includes steps 201 to 203:
- Step 201 Determine an identification code of the external input device.
- the identification code is the only identifier capable of identifying the input device.
- the terminal device acquires the identification code of the input device, and then sends the identification code of the input device to the energy server.
- the identification code of the input device can also be recognized by the server.
- Step 202 Determine a system interface corresponding to the identifier.
- a plurality of system interfaces are set in the server, and each system interface corresponds to one input device, because different input devices have different operation buttons.
- the input device matches the system interface to improve the user experience.
- Step 203 Map each operation button of the input device to an aircraft model to control an action of the aircraft in the system interface according to the operation of the operation button.
- the aircraft model may be implemented by simulation software or a mathematical model in a game, or may be implemented by hardware.
- the aircraft model may include a dynamic model and a display model of the aircraft.
- the power model is mapped to each operation button of the input device, and the parameters thereof can be adjusted according to the operation of each operation button.
- the display model includes an aircraft that is presented to the user in the system interface. It will be appreciated that as the parameters of the aircraft model change, the corresponding aircraft motion will also change.
- the server can adjust the parameters of the aircraft by the above operations, and then be displayed by the action of the aircraft on the system interface. The user can confirm the correct operation of the aircraft through the action of each aircraft in the operation interface to improve the control accuracy.
- the embodiment of the present invention can be applied to scenarios of multiple input devices.
- the user can use the familiar input device to combine the system boundary.
- Game or flight simulation can reduce the time cost of learning operations.
- the user interface can be more familiar with the operation mode due to the prompt of the system interface, which can reduce the learning cost, and can enable the user to experience the fun of different control modes and obtain the real flight experience.
- the input device may be one or more of an aircraft remote controller, a game controller, and a keyboard, and the user is described in conjunction with the scenario of FIG.
- the terminal device 101 acquires an identification code of one or more input devices 102.
- the confirmation process of the identification code includes:
- each communication interface may have a one-to-one correspondence with the input device 102.
- the terminal device 101 can send the identification code of the communication interface to the server 104, and then the server 104 acquires the identification of the input device 104 according to the correspondence between the communication interface and the input device 102. code.
- the identification code of the communication interface can also be directly used as the identification code of the input device 102. This embodiment can also be implemented without affecting other configurations. Program.
- the terminal device 101 is small in size and the number of communication interfaces is limited, and multiple input devices 102 are required to share a communication interface, such as a USB interface.
- the terminal device 101 detects that the communication interface accesses the input device 102, it can interact with the input device 102: for example, the terminal device 101 sends an identification request to the input device 102, and the input device 102 transmits to the terminal device 101 in response to the identification request. Its own identification code.
- the terminal device 101 transmits the acquired identification code of the input device 102 to the server 104. This saves the purpose of the communication interface.
- the terminal device 101 accesses the input device 102 to the service.
- the device 104 sends access information for prompting the server 104 that the input device 102 has access to the terminal device 101.
- the server 101 interacts with the input device 102 via the communication connection 103 to obtain the identification code of the input device 102. This can save the interaction time between the terminal device 101 and the input device 102, and improve the control efficiency.
- the server 103 After confirming the identification code of the input device 102, the server 103 determines its corresponding system interface based on the identification code.
- the system interface is pre-stored in the server 104 and each system interface corresponds to an input device 102. In this way, the input device matches the system interface to improve the user experience.
- the terminal device 101 can access multiple input devices 102 at the same time.
- the server 104 determines the priority of the multiple input devices 102 according to the identification code. In this embodiment, the priority is from the highest to the lowest. , gamepad and keyboard. That is, the server 104 determines the system interface corresponding to the aircraft remote controller as the final system interface, and transmits the above system interface to the terminal device 101.
- Figure 3 illustrates a system interface including an aircraft flight display area and a plurality of virtual keys (e.g., weight, altitude, speed, direction, ..., back, forward, etc.).
- the aircraft flight display area may display an action of the aircraft and a flight scene, and the plurality of virtual buttons may display flight parameters corresponding to the aircraft or control information of the input device.
- the system interface can be adjusted and laid out according to actual needs, which is not limited in this embodiment.
- the server 104 determines the source of the control information according to the control information of the input device 102, and then displays the system interface corresponding to the input device. If the server 104 receives the control information of the plurality of input devices at the same time, the system interface corresponding to the input device with the highest priority is displayed at this time.
- the server 104 maps the operational buttons of the input device 102 to the aircraft model, ie to the dynamic model of the aircraft. Then, according to the operation of each operation button of the input device, the model of the aircraft is adjusted according to the control command, and the action of the aircraft is controlled. If the virtual button in FIG. 3 exists in the system interface, the operation of each operation button can also be displayed through the parameters of the virtual button in the system interface.
- the pre-configured mapping relationship table is stored in the server 104, and the aircraft remote controller shown in FIG. 4, the game controller and the keyboard shown in FIG. 5 are taken as an example, and the mapping is off. The table is shown in Tables 1 and 2.
- Table 1 is the mapping relationship between the operation buttons of the input device and the menu-related parameters in the aircraft model. According to the mapping relationship of Table 1, the user can adjust various parameters of the aircraft model through the input device.
- Table 2 shows the mapping relationship between the operation buttons of the input device and the flight parameters of the aircraft in the aircraft model. According to the mapping relationship of Table 2, the user can adjust various parameters in the aircraft model through the input device to achieve the purpose of adjusting the motion of the aircraft.
- the server 104 transmits the above-mentioned aircraft model parameters to the terminal device 101, and the terminal device 101 completes the first display.
- Each parameter in each aircraft model may be a default value when first displayed, or may be a parameter of the current flight state of the aircraft.
- the terminal device 101 When the user operates the operation button of the input device 102, the terminal device 101 generates a corresponding control command according to the corresponding operation, and transmits the control command to the server 104.
- the aircraft model in the server 104 adjusts the corresponding parameters according to the mapping relationship between the control command and the parameters. For example, if the operation button is triggered once, the preset step size can be added based on the original value of the parameter to obtain the parameter update value.
- the preset step size can be adaptively adjusted according to the characteristics of each parameter, which is not limited in this embodiment.
- the terminal device 101 If the operation button is a joystick, the terminal device 101 generates a corresponding control command according to the rotation angle of the joystick.
- the control intensity indicated by the control command is positively correlated with the rotation angle.
- the server 104 adds a plurality of preset steps corresponding to the rotation angle based on the original value of the corresponding parameter according to the control instruction. long.
- the sensitivity coefficient corresponding to the default rocker in this embodiment is 1. If the user tends to have higher sensitivity, the sensitivity coefficient can be adjusted to be greater than 1, which can reduce the action of triggering the joystick; if the user tends to have lower sensitivity, the sensitivity coefficient can be adjusted to be less than 1, so that the user can use a larger action. A smaller amount of parameter variation is obtained.
- the flight simulation control method provided in this embodiment is configured on the terminal device.
- the input device accesses the terminal device through a communication interface, the terminal device determines an identification code of the input device, and then determines a system interface according to the identification code, and maps each operation button of the input device to the aircraft model. Then, the aircraft model in the terminal device adjusts the corresponding parameters according to the operation of each button of the input device, and displays the action of the aircraft in the system interface.
- the input device accesses the terminal device through a communication interface
- the terminal device determines an identification code of the input device, and then determines a system interface according to the identification code, and maps each operation button of the input device to the aircraft model.
- the aircraft model in the terminal device adjusts the corresponding parameters according to the operation of each button of the input device, and displays the action of the aircraft in the system interface.
- FIG. 6 is a schematic structural diagram of a server according to an embodiment of the present invention.
- the server 600 includes a processor 601, a memory 602, and a communication interface 603.
- a plurality of instructions are stored in the memory 602, and the processor 601 is configured to read instructions from the memory to implement:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- the processor 601 maps the operation buttons of the input device to the aircraft model, including:
- Each operation button of the input device is mapped to an aircraft model according to a mapping relationship table.
- the processor 601 is further configured to:
- the action of the aircraft is controlled in accordance with the control command.
- the processor 601 acquires a control instruction that the terminal device sends an operation button corresponding to the input device, and includes:
- control instruction corresponds to a rocker on the terminal device, adjusting a parameter of the aircraft model according to a control intensity indicated by the control instruction; a control intensity indicated by the control instruction and a rotation angle of the rocker are positive Related.
- the processor 601 determines an identifier of the external input device, including:
- the processor 601 determines a system interface corresponding to the identifier, including:
- the system interface corresponding to the input device with the highest priority is determined as the system interface to be displayed.
- the input device includes one or more of an aircraft remote controller, a game controller, and a keyboard.
- the priority of the input device from high to low is: an aircraft remote controller, a game controller, and a keyboard.
- FIG. 7 is a schematic structural diagram of a terminal device according to an embodiment of the present invention.
- the terminal device 700 includes a processor 701, a memory 702, and a communication interface 703.
- a number of instructions are stored in the memory 702, and the processor 701 is configured to read instructions from the memory to implement:
- the processor 701 is configured to:
- the control instruction is used to instruct the server to adjust parameters of the aircraft model according to a mapping relationship between an operation button and an aircraft model;
- the processor 701 is configured to generate a corresponding control instruction according to the operation of the operation button, including:
- the operation button is a rocker
- a corresponding control command is generated according to the rotation angle of the rocker; and the control intensity indicated by the control command is positively correlated with the rotation angle.
- FIG. 8 is a schematic structural diagram of a terminal device according to an embodiment of the present invention.
- the terminal device 800 includes a processor 801, a memory 802, and a communication interface 803.
- a number of instructions are stored in the memory 802, and the processor 801 is configured to read instructions from the memory to implement:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- the processor 801 maps the operation buttons of the input device to the aircraft model, including:
- Each operation button of the input device is mapped to an aircraft model according to a mapping relationship table.
- the processor 801 is further configured to:
- the parameters of the aircraft model are adjusted according to the control command.
- the processor 801 generates a corresponding control instruction according to the operation information of the operation button, including:
- the operation button is a rocker
- a corresponding control command is generated according to the rotation angle of the rocker; and the control intensity indicated by the control command is positively correlated with the rotation angle.
- the processor 801 determines an identifier of the external input device, including:
- the processor 801 determines an identifier of the external input device, including:
- the identification code of the input device is determined according to a correspondence between the communication interface and the input device.
- the processor 801 determines a system interface corresponding to the identifier, including:
- the system interface corresponding to the input device with the highest priority is determined as the system interface to be displayed.
- the input device includes one or more of an aircraft remote controller, a game controller, and a keyboard.
- the priority of the input device from high to low is: an aircraft remote controller, a game controller, and a keyboard.
- An embodiment of the invention further provides a machine readable storage medium having stored thereon a plurality of computer instructions, the computer instructions being executed as follows:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- An embodiment of the invention further provides a machine readable storage medium having stored thereon a plurality of computer instructions, the computer instructions being executed as follows:
- a system interface corresponding to the identification code of the input device is received, and an action of the aircraft.
- An embodiment of the invention further provides a machine readable storage medium having stored thereon a plurality of computer instructions, the computer instructions being executed as follows:
- Each operational button of the input device is mapped to an aircraft model to control the motion of the aircraft in the system interface in accordance with the operation of the operational button.
- the disclosed apparatus and method may be implemented in other manners.
- the device embodiments described above are merely illustrative.
- the division of the unit is only a logical function division.
- there may be another division manner for example, multiple units or components may be combined or Can be integrated into another system, or some features can be ignored or not executed.
- the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, device or unit, and may be in an electrical, mechanical or other form.
- the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, may be located in one place, or may be distributed to multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of the embodiment.
- each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
- the above integrated unit can be implemented in the form of hardware or in the form of hardware plus software functional units.
- the above-described integrated unit implemented in the form of a software functional unit can be stored in a computer readable storage medium.
- the above software functional unit is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) or a processor to perform the methods of the various embodiments of the present invention.
- the foregoing storage medium includes: a U disk, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk, or an optical disk, and the like, which can store program codes. .
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Abstract
L'invention concerne un procédé de commande de simulation de vol, un serveur et un dispositif terminal, le procédé consistant : à déterminer un code d'identification d'un dispositif d'entrée externe (201) ; à déterminer une interface de système correspondant au code d'identification (202) ; et à mapper diverses touches d'opérations d'un dispositif d'entrée vers un modèle d'aéronef, afin de commander les actions d'un aéronef dans l'interface de système selon l'opération des touches (203). On peut voir que le procédé de commande de simulation de vol, le serveur et le dispositif terminal peuvent être appliqués à des scènes de dispositifs d'entrée multiples, et qu'un utilisateur peut utiliser un dispositif d'entrée avec lequel il est déjà familier pour le jeu ou la simulation de vol, réduisant ainsi le temps et le coût d'apprentissage d'un mode d'opération. Par ailleurs, l'utilisateur peut également utiliser différents dispositifs d'entrée pour commander le même dispositif terminal, simuler et commander le vol de l'aéronef, et obtenir une expérience de vol réelle.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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PCT/CN2017/094733 WO2019019111A1 (fr) | 2017-07-27 | 2017-07-27 | Procédé de commande de simulation de vol, serveur et dispositif terminal |
CN201780005601.3A CN108521797B (zh) | 2017-07-27 | 2017-07-27 | 飞行仿真控制方法、服务器、终端设备 |
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PCT/CN2017/094733 WO2019019111A1 (fr) | 2017-07-27 | 2017-07-27 | Procédé de commande de simulation de vol, serveur et dispositif terminal |
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CN112558955A (zh) * | 2019-09-10 | 2021-03-26 | 广州途道信息科技有限公司 | 机器人的编程和控制方法、可读存储介质和计算设备 |
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CN102929683A (zh) * | 2012-08-08 | 2013-02-13 | 韦创科技有限公司 | 输入设备的全自动化仿真系统 |
US20140049461A1 (en) * | 2012-08-17 | 2014-02-20 | Innomind Solution Company Limited | Fully automatic simulation system of an input device |
CN105120329A (zh) * | 2015-09-08 | 2015-12-02 | 冠捷显示科技(厦门)有限公司 | 一种应用于电视游戏控制的输入适配方法 |
US20170083194A1 (en) * | 2009-07-08 | 2017-03-23 | Steelseries Aps | Apparatus and method for managing operations of accessories |
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CN102789171A (zh) * | 2012-09-05 | 2012-11-21 | 北京理工大学 | 一种可视化无人机飞行控制半实物仿真测试方法及系统 |
CN103093047B (zh) * | 2013-01-12 | 2015-06-17 | 天津大学 | 典型飞行器视景仿真系统 |
CN104462669A (zh) * | 2014-11-24 | 2015-03-25 | 成都盛军电子设备有限公司 | 一种飞行仿真系统 |
CN204705825U (zh) * | 2015-03-13 | 2015-10-14 | 吉林医药学院 | 无人机三维立体显控综合训练系统 |
CN104765280B (zh) * | 2015-03-13 | 2018-05-01 | 吉林医药学院 | 无人机三维立体显控综合训练系统 |
CN104932530A (zh) * | 2015-06-04 | 2015-09-23 | 中国航空无线电电子研究所 | 一种无人机操控系统及其下行遥测方法、上行遥测方法 |
CN105159141B (zh) * | 2015-08-11 | 2019-03-22 | 中国航空工业集团公司西安飞机设计研究所 | 电传控制律传动比的验证方法及装置 |
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- 2017-07-27 CN CN201780005601.3A patent/CN108521797B/zh not_active Expired - Fee Related
- 2017-07-27 WO PCT/CN2017/094733 patent/WO2019019111A1/fr active Application Filing
Patent Citations (4)
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US20170083194A1 (en) * | 2009-07-08 | 2017-03-23 | Steelseries Aps | Apparatus and method for managing operations of accessories |
CN102929683A (zh) * | 2012-08-08 | 2013-02-13 | 韦创科技有限公司 | 输入设备的全自动化仿真系统 |
US20140049461A1 (en) * | 2012-08-17 | 2014-02-20 | Innomind Solution Company Limited | Fully automatic simulation system of an input device |
CN105120329A (zh) * | 2015-09-08 | 2015-12-02 | 冠捷显示科技(厦门)有限公司 | 一种应用于电视游戏控制的输入适配方法 |
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CN108521797B (zh) | 2021-04-06 |
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