An airborne satellite communication apparatus, method, device and medium

Abstract

The application discloses an airborne satellite communication device, method, equipment and medium, and relates to the technical field of satellite communication. The application comprises the following steps: acquiring a target satellite communication signal through an airborne satellite communication device; generating a corresponding OPENAMIP protocol through a different satellite communication system modem board integrated on a connector board card in the airborne satellite communication device; performing an analysis operation on the OPENAMIP protocol through control instruction processing software carried by a main control board in the airborne satellite communication device to obtain a corresponding to-be-executed control instruction, and configuring parameters of the airborne satellite communication device based on the to-be-executed control instruction, so that a single antenna can simultaneously adapt to the modulation and demodulation modules of two different satellite communication systems. Therefore, the application can expand the application area of satellite communication, increase the system communication capacity, and improve the use experience of high-throughput satellite communication technology of a civil aircraft.

Description

Technical Field

[0001] This invention relates to the field of satellite communication technology, and in particular to an airborne satellite communication device, method, equipment, and medium. Background Technology

[0002] Currently, air-to-ground communication in the rear cabin of civil aircraft, especially for transcontinental and transoceanic flights, primarily utilizes satellite communication. High-throughput satellite communication systems are gradually establishing network coverage globally and being deployed in the civilian sector. The current challenges facing airborne satellite communication systems include incompatibility between different satellite systems, significant differences in coverage areas, and substantial variations in system capacity and communication speeds supported by different networks. Aircraft need to switch network services when traveling to different regions. Therefore, existing airborne satellite communication equipment often has limited operating areas and cannot be scaled up. Currently, mainstream airborne satellite communication equipment only supports one satellite communication system, commonly known as single-mode equipment. The biggest difficulty with this type of equipment is that its operating range is limited by the satellite system it serves, allowing it to operate only in certain areas and not fully support transoceanic and transcontinental scenarios. In contrast to single-mode, dual-mode airborne equipment supports switching between two different satellite communication systems, allowing for switching between serving satellite networks and expanding the operating area. However, it only supports one network service at a time. When multiple satellite systems simultaneously cover an area, the spectrum resources of one satellite system are wasted, preventing an increase in system capacity.

[0003] As can be seen from the above, how to expand the application area of ​​satellite communication, increase the system communication capacity, and improve the user experience of high-throughput satellite communication technology for civil aircraft are urgent problems to be solved. Summary of the Invention

[0004] In view of this, the purpose of this invention is to provide an airborne satellite communication device, method, equipment, and medium that can expand the application range of satellite communication, increase system communication capacity, and improve the user experience of high-throughput satellite communication technology for civil aircraft. The specific solution is as follows:

[0005] In a first aspect, this application provides an airborne satellite communication device, comprising:

[0006] An airborne satellite communication antenna is used to acquire target satellite communication signals; the target satellite communication signals are satellite communication signals corresponding to the satellite communication system of the modem board in the airborne satellite communication device.

[0007] Connector board; the connector board is used to integrate modem boards of different satellite communication systems, as well as combiners and power dividers; the modem board is used to generate the corresponding OPENAMIP protocol; the combiner is used to combine the output signal power of the two modem boards, and the power divider is used to distribute the received satellite signal to the modem board;

[0008] The main control board is equipped with control command processing software. The control command processing software is used to parse the OPENAMIP protocol to obtain the corresponding control commands to be executed, and to configure the parameters of the airborne satellite communication antenna based on the control commands to be executed.

[0009] Optionally, the airborne satellite communication device further includes:

[0010] The radio frequency signal interface is a wireless signal interface that is uniquely connected to the airborne satellite communication antenna and is connected to the modulation and demodulation equipment and the airborne satellite communication antenna via a coaxial cable.

[0011] The radio frequency signal interface is used to receive satellite communication signals and transmit the output signals of the modem board.

[0012] Secondly, this application provides an airborne satellite communication method based on an airborne satellite communication device, wherein the airborne satellite communication device is the aforementioned airborne satellite communication device; wherein the method includes:

[0013] The target satellite communication signal is acquired through the airborne satellite communication antenna in the airborne satellite communication device; the target satellite communication signal is a satellite communication signal corresponding to the satellite communication system of the modem board in the airborne satellite communication device.

[0014] The corresponding OpenAMIP protocol is generated by the modem boards of different satellite communication systems integrated on the connector board in the airborne satellite communication device.

[0015] The control command processing software mounted on the main control board of the airborne satellite communication device parses the OPENAMIP protocol to obtain the corresponding control commands to be executed, and configures the parameters of the airborne satellite communication antenna based on the control commands to be executed.

[0016] Optionally, after acquiring the target satellite communication signal through the airborne satellite communication antenna in the airborne satellite communication device, the method further includes:

[0017] The power divider integrated on the connector board sends the first target satellite communication signal corresponding to the first satellite communication system to the corresponding first modem board, and sends the second target satellite communication signal corresponding to the second satellite communication system to the corresponding second modem board.

[0018] Accordingly, the generation of corresponding OPENAMIP protocols through modem boards of different satellite communication systems integrated on the connector board of the airborne satellite communication device includes:

[0019] The first OpenAM IP protocol is generated through the first modem board;

[0020] The second OPENAMIP protocol is generated through the second modem board.

[0021] Optionally, the step of parsing the OPENAMIP protocol through the control command processing software mounted on the main control board of the airborne satellite communication device to obtain the corresponding control commands to be executed, and configuring the parameters of the airborne satellite communication antenna based on the control commands to be executed, includes:

[0022] The first OpenAMIP protocol and the second OpenAMIP protocol are sent to the control command processing software;

[0023] The control command processing software parses the first OPENAMIP protocol and the second OPENAMIP protocol to obtain the corresponding first control command and second control command, and determines whether the first control command and the second control command are consistent to obtain the control command consistency judgment result.

[0024] Based on the control command consistency judgment result and the preset antenna control right arbitration rule, the control command to be executed is determined from the first control command and the second control command, and the parameters of the airborne satellite communication antenna are configured based on the control command to be executed; the preset antenna control right arbitration rule is to set either the first modem board or the second modem board as the main modem board, and to give priority to the control command generated by the main modem board as the control command to be executed.

[0025] Optionally, the step of determining the control instruction to be executed from the first control instruction and the second control instruction based on the consistency judgment result of the control instruction and the preset antenna control arbitration rule, and configuring the parameters of the airborne satellite communication antenna based on the control instruction to be executed, includes:

[0026] If the first control command and the second control command are consistent, then the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule, and the parameters of the airborne satellite communication antenna are configured based on the control command to be executed.

[0027] If the first control command and the second control command are inconsistent, the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule. After configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the parameters of the current airborne satellite communication antenna are returned to another modem board so that the other modem board can generate a corresponding output signal based on the parameters of the current airborne satellite communication antenna.

[0028] Optionally, the airborne satellite communication method further includes:

[0029] If the first control command and the second control command are inconsistent, and the control command to be executed determined according to the preset antenna control arbitration rule is abnormal, then the other control command will be used as the new control command to be executed.

[0030] Optionally, after configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the method further includes:

[0031] The first output signal generated by the first modem board and the second output signal generated by the second modem board are combined into a target output signal by the combiner integrated on the connector board, and the target output signal is sent to the radio frequency signal interface in the airborne satellite communication device.

[0032] Thirdly, this application provides an electronic device, comprising:

[0033] Memory, used to store computer programs;

[0034] A processor is used to execute the computer program to implement the aforementioned airborne satellite communication method.

[0035] Fourthly, this application provides a computer-readable storage medium for storing a computer program, wherein the computer program, when executed by a processor, implements the aforementioned airborne satellite communication method.

[0036] This application provides an airborne satellite communication method based on an airborne satellite communication device. First, the target satellite communication signal is acquired, and a corresponding OPENAMIP protocol is generated through the modem board. The target satellite communication signal is a satellite communication signal corresponding to the satellite communication system of the modem board. Then, the OPENAMIP protocol is parsed by the control command processing software to obtain the corresponding control command to be executed. Finally, the corresponding control operation is executed according to the control command to be executed.

[0037] As can be seen from the above, this application integrates two modem boards of different satellite communication systems into one unit through the power divider and combiner in the airborne satellite communication device. This allows for simultaneous reception of satellite signals from different systems without switching operations, meaning that both systems' satellite network services can be online simultaneously, utilizing both forward and reverse communication services. Furthermore, the control command processing software parses the OPENAMIP protocol, performing consistency checks on the satellite signals from different systems to select appropriate control commands for antenna parameter configuration, enabling the dual-system modem boards to share a single antenna. This expands the application area of ​​satellite communication, increases system communication capacity, and enhances the user experience of high-throughput satellite communication technology for civil aircraft. Attached Figure Description

[0038] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on the provided drawings without creative effort.

[0039] Figure 1 This is a schematic diagram of an airborne satellite communication device disclosed in this application;

[0040] Figure 2 This is a flowchart of an airborne satellite communication method based on an airborne satellite communication device disclosed in this application;

[0041] Figure 3 This is a schematic diagram of the architecture of an airborne satellite communication device disclosed in this application;

[0042] Figure 4 This application discloses a flowchart of an OPEMAMIP protocol processing software.

[0043] Figure 5 This is a structural diagram of an electronic device disclosed in this application. Detailed Implementation

[0044] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0045] Currently, air-to-ground communication in the rear cabin of civil aircraft, especially for transcontinental and transoceanic flights, primarily utilizes satellite communication. High-throughput satellite communication systems are gradually establishing network coverage globally and being deployed in the civilian sector. The current challenges facing airborne satellite communication systems include incompatibility between different satellite systems, significant differences in coverage areas, and substantial variations in system capacity and communication speeds supported by different networks. Aircraft need to switch network services when traveling to different regions. Therefore, existing airborne satellite communication equipment often has limited operating areas and cannot be scaled up. Currently, mainstream airborne satellite communication equipment only supports one satellite communication system, commonly known as single-mode equipment. The biggest difficulty with this type of equipment is that its operating range is limited by the satellite system it serves, allowing it to operate only in certain areas and not fully support transoceanic and transcontinental scenarios. In contrast to single-mode, dual-mode airborne equipment supports switching between two different satellite communication systems, allowing for switching between serving satellite networks and expanding the operating area. However, it only supports one network service at a time. When multiple satellite systems simultaneously cover an area, the spectrum resources of one satellite system are wasted, preventing an increase in system capacity. Therefore, this application provides an airborne satellite communication solution that can expand the application area of ​​satellite communication, increase the system communication capacity, and improve the user experience of high-throughput satellite communication technology for civil aircraft.

[0046] See Figure 1 As shown, this application provides an airborne satellite communication device, comprising:

[0047] An airborne satellite communication antenna 11 is used to acquire target satellite communication signals; the target satellite communication signals are satellite communication signals corresponding to the satellite communication system of the modem board in the airborne satellite communication device.

[0048] Connector board 12; the connector board is used to integrate modem boards of different satellite communication systems, as well as combiners and power dividers; the modem board is used to generate the corresponding OPENAMIP protocol; the combiner is used to combine the output signal power of the two modem boards, and the power divider is used to distribute the received satellite signal to the modem board;

[0049] The main control board 13 is equipped with control command processing software. The control command processing software is used to parse the OPENAMIP protocol to obtain the corresponding control commands to be executed, and to configure the parameters of the airborne satellite communication antenna based on the control commands to be executed.

[0050] As can be seen from the above, this application integrates two modem boards of different satellite communication systems into one unit through the power divider and combiner in the airborne satellite communication device. This allows for simultaneous reception of satellite signals from different systems without switching operations, meaning that both systems' satellite network services can be online simultaneously, utilizing both forward and reverse communication services. Furthermore, the control command processing software parses the OPENAMIP protocol, performing consistency checks on the satellite signals from different systems to select appropriate control commands for antenna parameter configuration, enabling the dual-system modem boards to share a single antenna. This expands the application area of ​​satellite communication, increases system communication capacity, and enhances the user experience of high-throughput satellite communication technology for civil aircraft.

[0051] In some specific embodiments, the airborne satellite communication device may further include:

[0052] The radio frequency (RF) signal interface is a wireless signal interface that is uniquely connected to the airborne satellite communication antenna and is connected to the modulation and demodulation equipment and the airborne satellite communication antenna via a coaxial cable; wherein, the RF signal interface is used to receive satellite communication signals and transmit the output signals of the modem board.

[0053] See Figure 2 As shown in the figure, this application discloses an airborne satellite communication method based on the aforementioned airborne satellite communication device, including:

[0054] Step S11: Obtain the target satellite communication signal through the airborne satellite communication antenna in the airborne satellite communication device.

[0055] In this embodiment, the target satellite communication signal is a satellite communication signal corresponding to the satellite communication system of the modem board in the airborne satellite communication device. The two modem boards with different satellite communication systems are integrated together by a power divider in the airborne satellite communication device. Specifically, after acquiring the target satellite communication signal through the airborne satellite communication antenna in the airborne satellite communication device, the process may further include: sending the first target satellite communication signal corresponding to the first satellite communication system to the corresponding first modem board through the power divider integrated on the connector board, and sending the second target satellite communication signal corresponding to the second satellite communication system to the corresponding second modem board. That is, by integrating the two modem boards with different satellite communication systems through the power divider, the device can simultaneously receive satellite signals of different satellite communication systems through a single intermediate frequency signal channel without requiring additional switching operations.

[0056] Step S12: Generate the corresponding OPENAMIP protocol through the modem boards of different satellite communication systems integrated on the connector board in the airborne satellite communication device.

[0057] In this embodiment, corresponding OPENAMIP protocols for different satellite communication systems are generated through modem boards of different satellite communication systems. Specifically, generating corresponding OPENAMIP protocols through modem boards of different satellite communication systems integrated on the connector board of the airborne satellite communication device may include: generating a first OPENAMIP protocol through the first modem board; and generating a second OPENAMIP protocol through the second modem board. It should be noted that the specific type of satellite communication system can be determined according to the actual application situation, and is not specifically limited here.

[0058] Step S13: The control command processing software mounted on the main control board of the airborne satellite communication device parses the OPENAMIP protocol to obtain the corresponding control command to be executed, and configures the parameters of the airborne satellite communication antenna based on the control command to be executed.

[0059] In this embodiment, the control command processing software configures the parameters of the airborne satellite communication antenna to output corresponding signals and complete the satellite communication process. Specifically, the control command processing software parses the OPENAMIP protocol to obtain corresponding control commands to be executed, and configures the parameters of the airborne satellite communication antenna based on these commands. Specifically, the step of parsing the OPENAMIP protocol through the control command processing software mounted on the main control board of the airborne satellite communication device to obtain corresponding control commands to be executed, and configuring the parameters of the airborne satellite communication antenna based on the control commands to be executed, may include: sending the first OPENAMIP protocol and the second OPENAMIP protocol to the control command processing software; parsing the first OPENAMIP protocol and the second OPENAMIP protocol through the control command processing software to obtain corresponding first control commands and second control commands, and determining whether the first control commands and the second control commands are consistent to obtain a control command consistency judgment result; determining the control command to be executed from the first control commands and the second control commands according to the control command consistency judgment result and a preset antenna control right arbitration rule, and configuring the parameters of the airborne satellite communication antenna based on the control commands to be executed; the preset antenna control right arbitration rule is that either the first modem board or the second modem board is set as the main modem board, and the control commands generated by the main modem board are given priority as the control commands to be executed. That is, the control instruction processing software determines the control instruction to be executed from the first control instruction and the second control instruction according to the antenna control arbitration rules.

[0060] Furthermore, different antenna configuration strategies are adopted based on the consistency judgment result of the control commands. Specifically, the step of determining the control command to be executed from the first control command and the second control command based on the consistency judgment result of the control commands and the preset antenna control arbitration rule, and configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, may include: if the first control command and the second control command are consistent, then the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule, and the parameters of the airborne satellite communication antenna are configured based on the control command to be executed; if the first control command and the second control command are inconsistent, then the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule, and after configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the parameters of the current airborne satellite communication antenna are returned to another modem board, so that the other modem board generates a corresponding output signal based on the parameters of the current airborne satellite communication antenna. That is, when the first control command and the second control command are inconsistent, the antenna configuration status needs to be returned to the modem board without control so that the modem board can carry out subsequent work processes.

[0061] It should be noted that if the control command to be executed determined by the preset antenna control arbitration rule is abnormal—for example, in one specific embodiment, the airborne satellite communication device is located outside the effective coverage area of ​​the satellite communication system, causing the control command to be executed to be abnormal—then it is necessary to adjust the control command to be executed according to the actual situation so that the satellite communication process can proceed normally. Specifically, the airborne satellite communication method may further include: if the first control command and the second control command are inconsistent, and the control command to be executed is abnormal because the airborne satellite communication device is located outside the effective coverage area of ​​the satellite communication system, then the other control command is used as the new control command to be executed.

[0062] It is understood that after configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the output signals generated by the modem board need to be combined into a target output signal through the combiner integrated on the connector board. Specifically, after configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, it may further include: combining the first output signal generated by the first modem board and the second output signal generated by the second modem board into a target output signal through the combiner integrated on the connector board, and sending the target output signal to the radio frequency signal interface in the airborne satellite communication device. The combiner integrates two modem boards of different satellite communication systems so that the two modem boards of different systems can simultaneously transmit signals to satellites of different systems through a single intermediate frequency channel.

[0063] As can be seen from the above, this embodiment integrates two modem boards with different satellite communication systems through the power divider and combiner in the airborne satellite communication device. This allows simultaneous reception of satellite signals from different systems without switching operations, meaning both systems can be online simultaneously, utilizing both forward and reverse communication services. Furthermore, the control command processing software parses the OPENAMIP protocol, effectively managing the antenna control commands of the two modem boards. This ensures normal and orderly antenna operation, guaranteeing that the modem boards can correctly acquire antenna signals, and allowing dual-mode devices to share a single antenna for simultaneous operation without switching. This expands the application area of ​​satellite communication, increases system communication capacity, and enhances the user experience of high-throughput satellite communication technology for civil aircraft.

[0064] Furthermore, this application provides a specific airborne satellite communication method, including:

[0065] In this embodiment, through Figure 3The illustration shows a specific airborne satellite communication device that implements the aforementioned airborne satellite communication method. The airborne satellite communication device includes two modem boards supporting different satellite communication systems, an interface board, and a main control board. The two modem boards support modulation and demodulation of signals from two different satellite communication systems, ensuring the device can normally use two different satellite network services. The airborne satellite communication device includes an interface board that houses a power divider and a combiner. Its main function is to split and combine the transmit and receive channels of the two different modem boards, ensuring that the device only needs one RF line to share a single antenna, enabling the two different system boards to simultaneously receive and transmit signals without switching between boards. The airborne satellite communication device includes a main control board that handles software protocol processing, communication data fusion, and distribution. The main control board has processor functionality; in addition to normal device scheduling and management, it needs to load OpenAMIP protocol management software. The main control board also needs to have a multi-port switch chip. The system connects to the modem board via a gigabit Ethernet port, and uses a switch to merge and distribute service data transmitted from the two different modem boards. It provides at least one gigabit Ethernet port to the outside world, enabling external service data interaction and allowing two different satellite communication systems to work simultaneously.

[0066] Further, see Figure 4 As shown, the OPENAMIP protocol management software simultaneously receives OPENAMIP protocol messages from two different types of boards, parses the received OPENAMIP protocol messages, and compares the control commands to determine whether the control commands for the antenna from both boards are consistent. If they are consistent, one board's control command is selected and passed to the antenna to perform antenna parameter configuration. If they are inconsistent, the antenna control is arbitrated, and the preset primary modem board command is selected as the configuration command. The other board's configuration command is not executed. For boards without control, the configured antenna status is returned to the board to start its subsequent normal operation process.

[0067] As can be seen from the above, this embodiment integrates two modems with different satellite communication systems using a power divider, ensuring that the device can simultaneously receive satellite signals from different systems through a single intermediate frequency (IF) signal channel without switching operations. Both systems' satellite network services can be online simultaneously, utilizing the forward communication services of different systems' satellite networks concurrently. A combiner integrates two modem boards with different satellite communication systems, allowing the two modem boards in the device to operate independently without interference, simultaneously transmitting signals to satellites of different systems through a single IF channel, and utilizing the different systems' satellite networks for reverse communication. The OPENAMIP protocol processing software parses the OPENAMIP protocol messages sent by the different modem boards and performs consistency checks on the message content. When message content is inconsistent, antenna control is arbitrated, selecting an appropriate control command to configure antenna parameters and coordinating the response of other modem boards without control, ensuring that the dual-system modem boards can share a single antenna. Therefore, this supports two different satellite network services and allows both modes to operate simultaneously without independent switching. It can not only meet the needs of expanding the application area of ​​satellite communication and satisfy the needs of the vast majority of flight routes around the world, but also simultaneously utilize the resources of two satellite systems in areas covered by multiple satellite systems, thereby expanding the system's communication capacity and improving the user experience of high-throughput satellite communication technology for civil aircraft.

[0068] Furthermore, embodiments of this application also disclose an electronic device, Figure 5 This is a structural diagram of an electronic device 20 according to an exemplary embodiment. The content of the diagram should not be construed as limiting the scope of this application. The electronic device 20 may specifically include: at least one processor 21, at least one memory 22, a power supply 23, a communication interface 24, an input / output interface 25, and a communication bus 26. The memory 22 stores a computer program, which is loaded and executed by the processor 21 to implement the relevant steps in the airborne satellite communication method disclosed in any of the foregoing embodiments. Furthermore, the electronic device 20 in this embodiment may specifically be an electronic computer.

[0069] In this embodiment, the power supply 23 is used to provide operating voltage for each hardware device on the electronic device 20; the communication interface 24 can create a data transmission channel between the electronic device 20 and external devices, and the communication protocol it follows can be any communication protocol applicable to the technical solution of this application, and is not specifically limited here; the input / output interface 25 is used to acquire external input data or output data to the outside world, and its specific interface type can be selected according to specific application needs, and is not specifically limited here.

[0070] In addition, the memory 22, as a carrier for resource storage, can be a read-only memory, random access memory, disk or optical disk, etc. The resources stored thereon can include operating system 221, computer program 222, etc., and the storage method can be temporary storage or permanent storage.

[0071] The operating system 221 is used to manage and control the various hardware devices on the electronic device 20 and the computer program 222, which may be Windows Server, Netware, Unix, Linux, etc. In addition to including computer programs capable of performing the airborne satellite communication method executed by the electronic device 20 as disclosed in any of the foregoing embodiments, the computer program 222 may further include computer programs capable of performing other specific tasks.

[0072] Furthermore, this application also discloses a computer-readable storage medium for storing a computer program; wherein, when the computer program is executed by a processor, it implements the aforementioned disclosed airborne satellite communication method. Specific steps of this method can be found in the corresponding content disclosed in the foregoing embodiments, and will not be repeated here.

[0073] The various embodiments in this specification are described in a progressive manner, with each embodiment focusing on its differences from other embodiments. Similar or identical parts between embodiments can be referred to interchangeably. For the apparatus disclosed in the embodiments, since it corresponds to the method disclosed in the embodiments, the description is relatively simple; relevant parts can be referred to in the method section.

[0074] Those skilled in the art will further recognize that the units and algorithm steps of the various examples described in conjunction with the embodiments disclosed herein can be implemented in electronic hardware, computer software, or a combination of both. To clearly illustrate the interchangeability of hardware and software, the components and steps of the various examples have been generally described in terms of functionality in the foregoing description. Whether these functions are implemented in hardware or software depends on the specific application and design constraints of the technical solution. Those skilled in the art can use different methods to implement the described functions for each specific application, but such implementation should not be considered beyond the scope of this application.

[0075] The steps of the methods or algorithms described in conjunction with the embodiments disclosed herein can be implemented directly by hardware, a software module executed by a processor, or a combination of both. The software module can be located in random access memory (RAM), main memory, read-only memory (ROM), electrically programmable ROM, electrically erasable programmable ROM, registers, hard disk, removable disk, CD-ROM, or any other form of storage medium known in the art.

[0076] Finally, it should be noted that in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes said element.

[0077] The technical solutions provided in this application have been described in detail above. Specific examples have been used to illustrate the principles and implementation methods of this application. The descriptions of the above embodiments are only for the purpose of helping to understand the methods and core ideas of this application. At the same time, for those skilled in the art, there will be changes in the specific implementation methods and application scope based on the ideas of this application. Therefore, the content of this specification should not be construed as a limitation of this application.

Claims

1. An airborne satellite communication device, characterized in that, include: Airborne satellite communication antenna, used to acquire target satellite communication signals; The target satellite communication signal is a satellite communication signal corresponding to the satellite communication system of the modem board in the airborne satellite communication device; Connector board; the connector board is used to integrate modem boards for different satellite communication systems, as well as combiners and power dividers; The modem board is used to generate the corresponding OPENAMIP protocol; The combiner is used to combine the output signal power of the two modem boards, and the power divider is used to distribute the received satellite signal to the modem board. The main control board is equipped with control command processing software. The control command processing software is used to parse the OPENAMIP protocol to obtain the corresponding control commands to be executed, and to configure the parameters of the airborne satellite communication antenna based on the control commands to be executed.

2. The airborne satellite communication device according to claim 1, characterized in that, Also includes: The radio frequency signal interface is a wireless signal interface that is uniquely connected to the airborne satellite communication antenna and is connected to the modulation and demodulation equipment and the airborne satellite communication antenna via a coaxial cable. The radio frequency signal interface is used to receive satellite communication signals and transmit the output signals of the modem board.

3. An airborne satellite communication method based on an airborne satellite communication device, characterized in that, The airborne satellite communication device is the airborne satellite communication device according to claim 1 or 2; wherein, the method includes: The target satellite communication signal is acquired through the airborne satellite communication antenna in the airborne satellite communication device; the target satellite communication signal is a satellite communication signal corresponding to the satellite communication system of the modem board in the airborne satellite communication device. The corresponding OpenAMIP protocol is generated by the modem boards of different satellite communication systems integrated on the connector board in the airborne satellite communication device. The control command processing software mounted on the main control board of the airborne satellite communication device parses the OPENAMIP protocol to obtain the corresponding control commands to be executed, and configures the parameters of the airborne satellite communication antenna based on the control commands to be executed.

4. The airborne satellite communication method according to claim 3, characterized in that, After acquiring the target satellite communication signal through the airborne satellite communication antenna in the airborne satellite communication device, the method further includes: The power divider integrated on the connector board sends the first target satellite communication signal corresponding to the first satellite communication system to the corresponding first modem board, and sends the second target satellite communication signal corresponding to the second satellite communication system to the corresponding second modem board. Accordingly, the generation of corresponding OPENAMIP protocols through modem boards of different satellite communication systems integrated on the connector board of the airborne satellite communication device includes: The first OpenAM IP protocol is generated through the first modem board; The second OPENAMIP protocol is generated through the second modem board.

5. The airborne satellite communication method according to claim 4, characterized in that, The process of parsing the OPENAMIP protocol using the control command processing software mounted on the main control board of the airborne satellite communication device to obtain corresponding control commands to be executed, and configuring the parameters of the airborne satellite communication antenna based on the control commands to be executed, includes: The first OpenAMIP protocol and the second OpenAMIP protocol are sent to the control command processing software; The control command processing software parses the first OPENAMIP protocol and the second OPENAMIP protocol to obtain the corresponding first control command and second control command, and determines whether the first control command and the second control command are consistent to obtain the control command consistency judgment result. Based on the control command consistency judgment result and the preset antenna control right arbitration rule, the control command to be executed is determined from the first control command and the second control command, and the parameters of the airborne satellite communication antenna are configured based on the control command to be executed; the preset antenna control right arbitration rule is to set either the first modem board or the second modem board as the main modem board, and to give priority to the control command generated by the main modem board as the control command to be executed.

6. The airborne satellite communication method according to claim 5, characterized in that, The step of determining the control command to be executed from the first control command and the second control command based on the consistency judgment result of the control command and the preset antenna control arbitration rule, and configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, includes: If the first control command and the second control command are consistent, then the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule, and the parameters of the airborne satellite communication antenna are configured based on the control command to be executed. If the first control command and the second control command are inconsistent, the control command generated by the main modem board is taken as the control command to be executed based on the preset antenna control arbitration rule. After configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the parameters of the current airborne satellite communication antenna are returned to another modem board so that the other modem board can generate a corresponding output signal based on the parameters of the current airborne satellite communication antenna.

7. The airborne satellite communication method according to claim 5, characterized in that, Also includes: If the first control command and the second control command are inconsistent, and the control command to be executed determined according to the preset antenna control arbitration rule is abnormal, then the other control command will be used as the new control command to be executed.

8. The airborne satellite communication method according to claim 5, characterized in that, After configuring the parameters of the airborne satellite communication antenna based on the control command to be executed, the process further includes: The first output signal generated by the first modem board and the second output signal generated by the second modem board are combined into a target output signal by the combiner integrated on the connector board, and the target output signal is sent to the radio frequency signal interface in the airborne satellite communication device.

9. An electronic device, characterized in that, include: Memory, used to store computer programs; A processor for executing the computer program to implement the airborne satellite communication method as described in any one of claims 3 to 8.

10. A computer-readable storage medium, characterized in that, Used to store a computer program, wherein the computer program, when executed by a processor, implements the airborne satellite communication method as described in any one of claims 3 to 8.

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