Atmosphere data acquisition control system for general aviation aircraft

Abstract

The utility model provides an atmosphere data acquisition control system for a general aviation aircraft, and aims to solve the problem of poor compatibility caused by the fact that the conventional atmosphere data acquisition system for the general aviation aircraft cannot integrate various types of meteorological detection equipment. The system comprises a main module, user interface equipment, an external interface and a task operation table. The main module comprises a data acquisition and processing module, a data storage module, an exchange module and an atmosphere data analysis module. According to the utility model, by integrating a plurality of external devices with different functions and using a specific data processing and analyzing mode, centralized control and unified data processing of the plurality of external devices are realized, and the problems of independent operation and poor compatibility of the existing atmospheric data acquisition system of the general aviation aircraft are solved; and meanwhile, due to the modular design, the convenience of installation, maintenance and use of external equipment is improved, and good expansion capacity is achieved so as to meet various operation requirements.

Description

Technical Field

[0001] The utility model relates to the field of meteorological monitoring and avionics integration, in particular to an atmospheric data acquisition and control system for general aviation aircraft. Background Art

[0002] Current general aviation aircraft systems for atmospheric data collection and weather modification operations typically utilize diverse and decentralized meteorological detection equipment, catalytic operation systems, and air-to-ground communication systems, lacking unified, integrated control. This independence leads to poor system compatibility, particularly between different devices. This limitation also prevents existing domestic aircraft from simultaneously carrying both foreign and domestic meteorological detection equipment, and from centrally processing meteorological data and transmitting air-to-ground data. Consequently, existing general aviation aircraft are limited to carrying only one type of meteorological detection equipment and performing simple data integration when performing weather modification operations. Utility Model Content

[0003] The utility model provides an atmospheric data acquisition and control system for general aviation aircraft to solve the problem of poor compatibility caused by the inability to integrate various types of meteorological detection equipment in existing general aviation aircraft atmospheric data acquisition systems.

[0004] The technical solution adopted in this utility model is:

[0005] An atmospheric data acquisition and control system for general aviation aircraft, comprising:

[0006] The main module is used for multi-source data acquisition, data processing, data fusion, and communication between different external devices.

[0007] User interface equipment, including a mission integration system display, a keyboard, a mouse, and a maritime satellite phone, wherein the mission integration system display is connected to the main module, and the keyboard and mouse are connected to the main module.

[0008] The external interface is used for connecting the atmospheric data acquisition and control system of general aviation aircraft with external devices to achieve high integration.

[0009] Furthermore, the system also includes:

[0010] A mission control console is installed in the aircraft cabin to provide an installation location for the main module and the user interface device, while providing an intuitive meteorological data observation and operation platform for meteorological operators.

[0011] Furthermore, the main module includes:

[0012] The data acquisition and processing module is responsible for real-time acquisition and analysis of data from different types of external devices in various interactive systems.

[0013] The data storage module is used to store all meteorological data analyzed by the data acquisition and processing module in real time and to review historical data.

[0014] The switching module is connected with the data acquisition and processing module and the data storage module to form an efficient communication network, thereby ensuring the stability and high reliability of air-to-ground data transmission between the aircraft and the ground office.

[0015] The atmospheric data analysis module is used to further set specific parameters for related external devices and analyze meteorological data in a targeted manner.

[0016] Furthermore, the data acquisition and processing module includes:

[0017] The communication data acquisition and processing submodule is connected to the switching module.

[0018] A domestic equipment data acquisition and processing submodule, wherein the domestic equipment data acquisition and processing submodule is connected to the switching module.

[0019] Foreign equipment data acquisition and processing submodule A, the foreign equipment data acquisition and processing submodule A is connected to the switching module.

[0020] The foreign equipment data acquisition and processing submodule B is connected to the switching module.

[0021] The switching module is connected to the communication data acquisition and processing sub-module, the domestic equipment data acquisition and processing sub-module, the foreign equipment data acquisition and processing sub-module A, and the foreign equipment data acquisition and processing sub-module B. Each sub-module collects data from the corresponding external device and converts the data into a unified format to solve the problem of independent operation and poor compatibility between external devices.

[0022] Furthermore, the main module is an industrial computer of the task integration system. The industrial computer of the task integration system includes a chassis and a host computer. The chassis contains slots and a backplane.

[0023] The switching module is an onboard network switch board.

[0024] The communication data acquisition and processing submodule is a communication data acquisition and processing submodule board. The communication data acquisition and processing submodule board.

[0025] The domestic equipment data acquisition and processing submodule is a domestic equipment data acquisition and processing submodule board.

[0026] The foreign equipment data acquisition and processing submodule A is a foreign equipment data acquisition and processing submodule A submodule board.

[0027] The foreign equipment data acquisition and processing submodule B is a foreign equipment data acquisition and processing submodule B board.

[0028] The data storage module is a data storage module board.

[0029] The onboard network switch board, the communication data acquisition and processing submodule board, the domestic equipment data acquisition and processing submodule board, the foreign equipment data acquisition and processing submodule A submodule board, the foreign equipment data acquisition and processing submodule B, and the data storage module board are inserted into the slots and connected together through the backplane to form the efficient communication network. The host computer is connected to the chassis.

[0030] The switching module board is connected to the communication data acquisition and processing sub-module board, the domestic equipment data acquisition and processing sub-module board, the foreign equipment data acquisition and processing sub-module A sub-module board, and the foreign equipment data acquisition and processing sub-module B board. Each sub-module collects data from the corresponding external device, and processes and analyzes the data into a unified format. The switching module board transmits the data in the unified format to the host computer, and the host computer can control all boards, thereby solving the problem of independent operation and poor compatibility between external devices.

[0031] Furthermore, the atmospheric data analysis module includes:

[0032] System configuration module, which is used for route preset, atmospheric data configuration, system settings, seeding operation settings, data transmission control, data storage configuration and macro recording control.

[0033] The monitoring and display module is used for real-time monitoring display, operation log display, atmospheric data display, aircraft track display and track playback display.

[0034] Air-to-ground communication module, which is used for atmospheric data transmission, maritime communication management, Beidou communication management and short message transmission.

[0035] The data analysis module is used for domestic equipment data analysis, foreign equipment data analysis and Ethernet data analysis.

[0036] Furthermore, the main control chip of all boards is FPGA.

[0037] Furthermore, the host computer and the chassis are connected via a 10Gbps Ethernet cable for high-speed data transmission and improved reliability of data transmission.

[0038] Furthermore, the chassis has at least 6 slots.

[0039] Furthermore, the FPGA is an UltraScale series FPGA.

[0040] The beneficial effects of the utility model are:

[0041] The utility model realizes centralized control of multiple external devices and unified data processing by integrating multiple external devices with different functions and using specific data processing and analysis methods, solving the problems of independent operation and poor compatibility of existing general aviation aircraft atmospheric data acquisition systems. At the same time, the modular design improves the convenience of installation, maintenance and use of external devices, and has good expansion capabilities to adapt to various operational needs.

[0042] The utility model contains FPGA, which has the characteristics of high-speed data processing and analysis, low latency and support for multiple function integration. The use of FPGA and high-speed communication protocol solves the problems of data transmission lag and difficulty in real-time sharing in existing general aviation aircraft atmospheric data acquisition systems, improves the efficiency of data transmission and processing, and ensures the real-time and reliability of meteorological data.

[0043] The upper computer of the utility model is connected to the chassis via a 10Gbps Ethernet network cable, which improves the speed and reliability of data transmission.

[0044] The chassis of the industrial computer of the present invention contains the remaining slots as reserved slots, which is convenient for future upgrading and expansion.

[0045] This utility model supports multiple communication protocols, ensuring compatibility with various types of meteorological detection equipment (external devices) both domestically and internationally, resolving the issue of inconsistent data protocols between different external devices. The use of a data storage module enables real-time storage of all analyzed meteorological data and allows for historical data access, facilitating operational assessment and subsequent data analysis, providing a basis for further operational optimization.

[0046] The atmospheric data analysis module in this utility model is used to further configure specific parameters for related external devices and analyze meteorological data in a targeted manner. It provides a unified user interface that integrates and displays data from domestic and foreign meteorological detection equipment, and features data analysis, device control, real-time display, and air-ground interaction. BRIEF DESCRIPTION OF THE DRAWINGS

[0047] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.

[0048] Figure 1 This is a system connection block diagram of Example 1.

[0049] Figure 2 Integrate the functional block diagram for the atmospheric data parsing module. DETAILED DESCRIPTION

[0050] The embodiments disclosed below are used to implement the structure of the present invention. In order to simplify the disclosure of the present invention, the components and settings of specific examples are described below. Of course, it is only an example and is not intended to limit the present invention.

[0051] The embodiments of the utility model are described in detail below with reference to the accompanying drawings.

[0052] Example 1

[0053] First, the system composition of this embodiment is introduced. Figure 1 This is a system connection block diagram of Example 1.

[0054] In this embodiment, the atmospheric data acquisition and control system for general aviation aircraft includes: a main module, a user interface device, an external interface, and a mission control console. The following is a detailed description:

[0055] The main module is used for multi-source data acquisition, data processing, data fusion, and communication between different external devices.

[0056] The user interface device includes a mission integration system display, a keyboard, a mouse, and a maritime satellite phone. The mission integration system display is connected to the main module, and the keyboard and mouse are connected to the main module. The display is the terminal display interface, which displays data from multiple meteorological detection equipment, including important meteorological information such as temperature, humidity, air pressure, wind speed, etc., to help operators understand the current operation status and meteorological data changes at any time. At the same time, as part of the user interface, the display not only provides data display, but also allows operators to control system functions through keyboard and mouse, such as adjusting meteorological detection equipment, sending operation instructions, and controlling data upload and download. The role of the maritime satellite phone is to achieve remote communication through satellite communication equipment, and to maintain real-time contact with the ground command center when general aviation aircraft perform missions. For example, meteorological operators can have voice calls with ground personnel to coordinate mission details and ensure accurate and smooth information communication.

[0057] The external interface is used for connecting the atmospheric data acquisition and control system of general aviation aircraft with external devices to achieve high integration.

[0058] A mission control console is installed in the aircraft cabin to provide an installation location for the main module and the user interface device, while providing an intuitive meteorological data observation and operation platform for meteorological operators.

[0059] In this embodiment, the main module includes:

[0060] The data acquisition and processing module is responsible for real-time acquisition and analysis of data from different types of external devices in various interactive systems.

[0061] The data storage module is used to store all meteorological data analyzed by the data acquisition and processing module in real time and to review historical data.

[0062] The switching module is connected with the data acquisition and processing module and the data storage module to form an efficient communication network, thereby ensuring the stability and high reliability of air-to-ground data transmission between the aircraft and the ground office.

[0063] The atmospheric data analysis module is used to further set specific parameters for related external devices and analyze meteorological data in a targeted manner.

[0064] In this embodiment, the data acquisition and processing module includes:

[0065] The communication data acquisition and processing submodule is connected to the switching module.

[0066] A domestic equipment data acquisition and processing submodule, wherein the domestic equipment data acquisition and processing submodule is connected to the switching module.

[0067] Foreign equipment data acquisition and processing submodule A. In this embodiment, foreign equipment data acquisition and processing submodule A is the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing submodule. The atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing submodule is connected to the switching module.

[0068] Foreign equipment data acquisition and processing submodule B: In this embodiment, the foreign equipment data acquisition and processing submodule B is a PROSENSING INC equipment data acquisition and processing submodule. The PROSENSING INC equipment data acquisition and processing submodule is connected to the switching module.

[0069] The exchange module is connected to the communication data acquisition and processing submodule, the domestic equipment data acquisition and processing submodule, the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing submodule, and the Prosensing Inc. equipment data acquisition and processing submodule. Each submodule collects data from the corresponding external device and converts the data into a unified format to solve the problem of independent operation and poor compatibility between external devices.

[0070] In this embodiment, the main module is an industrial computer of a task integration system, which includes a chassis having slots and a backplane inside.

[0071] The switching module is an onboard network switch board.

[0072] The communication data acquisition and processing submodule is a communication data acquisition and processing submodule board. The communication data acquisition and processing submodule board.

[0073] The domestic equipment data acquisition and processing submodule is a domestic equipment data acquisition and processing submodule board.

[0074] The DROPLET MEASUREMENT TECHNOLOGIES equipment data acquisition and processing submodule is a DROPLET MEASUREMENT TECHNOLOGIES equipment data acquisition and processing submodule board.

[0075] The PROSENSING INC equipment data acquisition and processing submodule is a PROSENSING INC equipment data acquisition and processing submodule board.

[0076] The data storage module is a data storage module board.

[0077] The onboard network switch board, the communication data acquisition and processing submodule board, the domestic equipment data acquisition and processing submodule board, the DROPLET MEASUREMENT TECHNOLOGIES equipment data acquisition and processing submodule board, the PROSENSING INC equipment data acquisition and processing submodule board, and the data storage module board are inserted into the slots and connected together via the backplane to form an efficient communication network. The host computer and the chassis are connected via a 10Gbps Ethernet cable for high-speed data transmission and improved data transmission reliability. The chassis has eight slots, six of which are used to insert the aforementioned boards, and the remaining two slots are reserved for future upgrades and expansion.

[0078] The switching module board is connected to the communication data acquisition and processing sub-module board, the domestic equipment data acquisition and processing sub-module board, the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing sub-module board, and the PROSENSING INC equipment data acquisition and processing sub-module board. Each sub-module collects data from the corresponding external device, and processes and analyzes the data and converts it into a unified format. The switching module board transmits the data in the unified format to the host computer, and the host computer can control all the boards, solving the problem of independent operation and poor compatibility between external devices.

[0079] In this embodiment, the atmospheric data analysis module includes:

[0080] System configuration module, which is used for route preset, atmospheric data configuration, system settings, seeding operation settings, data transmission control, data storage configuration and macro recording control.

[0081] The monitoring and display module is used for real-time monitoring display, operation log display, atmospheric data display, aircraft track display and track playback display.

[0082] Air-to-ground communication module, which is used for atmospheric data transmission, maritime communication management, Beidou communication management and short message transmission.

[0083] The data analysis module is used for domestic equipment data analysis, foreign equipment data analysis and Ethernet data analysis.

[0084] Attachment Figure 2 Integrate the functional block diagram for the atmospheric data parsing module.

[0085] In this embodiment, the main control chip for all boards is an UltraScale series FPGA. UltraScale series FPGAs have a large number of logic units, which can meet the needs of complex logic design. UltraScale series FPGAs integrate high-speed transceiver modules, enabling extremely high data transmission rates. They also integrate multiple functional modules such as PCI Express hard cores, Ethernet MAC modules, and memory controllers, enabling high-speed communication between the onboard network switch board and other boards.

[0086] This embodiment adds an external air-to-ground communication system, a weather detection system, and a catalytic operation system to the complete structure of the atmospheric data acquisition and control system for general aviation aircraft, as shown in the attached figure. Figure 1 Among them, the air-to-ground communication system includes satellite communication equipment and airborne Beidou equipment, the meteorological detection system includes domestically produced equipment and foreign equipment, and the catalytic operation system includes flame strip spreading equipment and flame bomb spreading equipment.

[0087] Among them, the domestically produced equipment includes: cloud particle spectrometer, cloud particle imager, precipitation particle imager, and atmospheric data acquisition pod;

[0088] Foreign equipment includes PIP (precipitation imager), CCP (cloud combination sounder), PCASP (passive cavity aerosol sounder), AIMMS (aircraft integrated meteorological measurement probe), CCN-200, (cloud condensation nucleus analyzer), KPR (airborne Ka-band cloud radar) and GVR (airborne microwave radiometer).

[0089] Each external device is connected to the external interface of the general aviation aircraft atmospheric data acquisition and control system of this embodiment. The specific connection relationship is as follows:

[0090] The satellite communication device is connected to the RJ45 interface of the maritime satellite phone. At the same time, the satellite communication device is connected to the communication data processing submodule board through Ethernet.

[0091] The airborne Beidou device is connected to the serial RS232 interface of the communication data processing submodule board.

[0092] The cloud particle spectrometer is connected to the serial RS485 interface of the data acquisition and processing sub-module board of the domestic equipment.

[0093] The cloud particle imager is connected to the serial RS485 interface of the data acquisition and processing submodule board of the domestic equipment.

[0094] The precipitation particle imager is connected to the serial RS485 interface of the data acquisition and processing sub-module board of the domestic equipment.

[0095] The atmospheric data acquisition pod is connected to the serial RS422 interface of the domestic equipment data acquisition and processing sub-module board.

[0096] The PIP is connected to the serial RS422 interface of the data acquisition and processing submodule board of the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES).

[0097] The CCP is connected to the serial RS422 interface of the data acquisition and processing submodule board of the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES).

[0098] The PCASP is connected to the serial RS422 interface of the data acquisition and processing submodule board of the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES).

[0099] AIMMS is connected to the serial RS232 interface of the data acquisition and processing submodule board of the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES).

[0100] CCN-200 is connected to the serial RS232 interface of the data acquisition and processing submodule board of the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES).

[0101] KPR is connected to the data acquisition and processing submodule board of PROSENSING INC equipment via LAN (local area network).

[0102] GVR is connected to the data acquisition and processing submodule board of PROSENSING INC equipment via LAN (local area network).

[0103] The flame strip spreading equipment is connected to the GPIO interface of the data acquisition and processing sub-module board of the PROSENSING INC equipment.

[0104] The flame bomb dispersing equipment is connected to the GPIO interface of the data acquisition and processing submodule board of PROSENSING INC.

[0105] In this embodiment, the task integration system display and the task integration system industrial computer are connected via a DVI interface cable.

[0106] The keyboard and mouse are connected to the task integration system industrial computer via USB cables.

[0107] After introducing the system composition of this embodiment, the working principle of the general aviation aircraft atmospheric data acquisition and control system of this embodiment is described below:

[0108] In this embodiment, the communication data acquisition and processing submodule board, the domestic equipment data acquisition and processing submodule board, the atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing submodule board, and the Prosensing Inc. equipment data acquisition and processing submodule board are responsible for real-time acquisition of data from different types of external devices in various interactive systems. Different data processing module boards will perform data processing and analysis on the collected data. The specific implementation method is: different types of external devices (satellite communication equipment and airborne Beidou equipment of the air-to-ground communication system, domestic equipment and foreign equipment of the meteorological detection system, and flame strip spreading equipment and flame bomb spreading equipment of the catalytic operation system) are connected with different data processing module boards (communication data acquisition and processing submodule board, domestic equipment data acquisition and processing submodule board, atmospheric droplet detection technology company (DROPLET MEASUREMENT TECHNOLOGIES) equipment data acquisition and processing submodule board, Prosensing Inc. The interfaces (serial RS232, RS422, RS485, Ethernet, GPIO, and LAN) on the INC equipment's data acquisition and processing submodule boards are connected, transmitting data via different communication protocols (because different interfaces represent different communication protocols). Data collected by the different data processing module boards is transmitted to the board's onboard FPGA. The FPGA processes and parses the data transmitted via different communication protocols and stores it in internal registers or memory modules (RAM). The FPGA then transmits the register or memory module data using the same communication protocol (PCI Express) via a high-speed interface connected to the backplane, then through the backplane and the onboard network switch board to the host computer and data storage module board. The data storage module board contains the FPGA and memory chips, capable of processing, parsing, and storing large amounts of data.

[0109] By integrating multiple external devices with different functions and using specific data processing and parsing methods, this utility model achieves centralized control and unified data processing for multiple external devices. This addresses the independent operation and poor compatibility issues of existing general aviation aircraft atmospheric data acquisition systems. Its modular design also improves the ease of installation, maintenance, and use of external devices, providing excellent scalability to accommodate diverse operational needs. FPGAs offer high-speed data processing and parsing, low latency, and support for multiple functional integration. The use of FPGAs and the high-speed PCI Express communication protocol addresses the data transmission lag and difficulty in real-time sharing in existing general aviation aircraft atmospheric data acquisition systems, improving data transmission and processing efficiency and ensuring the real-time and reliability of meteorological data. This embodiment of the general aviation aircraft atmospheric data acquisition and control system supports multiple communication protocols, ensuring compatibility with various types of domestic and international meteorological detection equipment (external devices) and resolving the issue of inconsistent data communication protocols between different external devices. The use of a data storage module board enables real-time storage of all parsed meteorological data and allows for historical data access, facilitating operational evaluation and subsequent data analysis, providing a basis for further optimization.

[0110] The atmospheric data analysis module provides a unified user interface that integrates and displays data from domestic and foreign meteorological detection equipment, and has data analysis, equipment control, real-time display and air-ground interaction functions.

[0111] In the atmospheric data analysis module interface, specific parameters of related external devices can be further set, and relevant meteorological data can be analyzed in a targeted manner; operators can use the atmospheric data analysis module interface to review historical observation data, and can download and analyze meteorological data through an external user interface.

[0112] The atmospheric data analysis module interface serves as the terminal display and system control interface, with four main functions: monitoring and display, system settings, air-to-ground communication, and data analysis. During use, the atmospheric data analysis module allows real-time monitoring of aircraft parameters and various types of meteorological detection data. The acquired meteorological data is then analyzed and processed separately, with a meteorological data display window corresponding to each detection device provided on the display interface for the operator to select and observe. The atmospheric data analysis module also records aircraft operating status information, including takeoff time, flight path, and operating area. The atmospheric data analysis module automatically records and collects aircraft position information provided by Beidou communication equipment and generates an aircraft track map. The track playback interface displays and displays aircraft track and parameter information, facilitating analysis of operational effectiveness and flight status. Furthermore, the atmospheric data analysis module can be customized based on the aircraft system status, including the catalyst load, operating area, and operation plan for the current operation. In the air-ground communication interface, operators can control the transmission of aircraft parameters and meteorological data, and receive catalytic operation instructions and related data from the ground. The atmospheric data analysis module provides two optional network channels: maritime communication and Beidou communication equipment. They can be selected according to the actual situation during flight, ensuring the stability of network transmission quality.

Claims

1. An atmospheric data acquisition and control system for general aviation aircraft, characterized in that: include: Main module, which is used for multi-source data acquisition, data processing, data fusion, and communication between different external devices; A user interface device, comprising a mission integration system display, a keyboard, a mouse, and a maritime satellite phone; wherein the mission integration system display is connected to the main module, and the keyboard and mouse are connected to the main module; The external interface is used for connecting the atmospheric data acquisition and control system of the general aviation aircraft to the external device through the external interface.

2. The atmospheric data acquisition and control system for general aviation aircraft according to claim 1, characterized in that: Also includes: A mission control console is installed in the aircraft cabin to provide an installation location for the main module and the user interface device, while providing an intuitive meteorological data observation and operation platform for meteorological operators.

3. The atmospheric data acquisition and control system for general aviation aircraft according to claim 2, characterized in that: The main module includes: A data acquisition and processing module, which is responsible for real-time acquisition and analysis of data from various types of external devices in various interactive systems; A data storage module, which is used to store all meteorological data analyzed by the data acquisition and processing module in real time and to review historical data; a switching module connected to the data acquisition and processing module and the data storage module; The atmospheric data analysis module is used to further set specific parameters for related external devices and analyze meteorological data in a targeted manner.

4. The atmospheric data acquisition and control system for general aviation aircraft according to claim 3, characterized in that: The data acquisition and processing module includes: a communication data acquisition and processing submodule, the communication data acquisition and processing submodule being connected to the switching module; a domestic equipment data acquisition and processing submodule, the domestic equipment data acquisition and processing submodule being connected to the switching module; Foreign equipment data acquisition and processing submodule A, the foreign equipment data acquisition and processing submodule A is connected to the switching module; The foreign equipment data acquisition and processing submodule B is connected to the switching module.

5. The atmospheric data acquisition and control system for general aviation aircraft according to claim 4, characterized in that: The main module is an industrial computer for the task integration system; the industrial computer for the task integration system includes a chassis and a host computer; the chassis contains slots and a backplane; The switching module is an onboard network switch card; The communication data acquisition and processing submodule is a communication data acquisition and processing submodule board; the communication data acquisition and processing submodule board; The domestic equipment data acquisition and processing submodule is a domestic equipment data acquisition and processing submodule board; The foreign equipment data acquisition and processing submodule A is a foreign equipment data acquisition and processing submodule A board; The foreign equipment data acquisition and processing submodule B is a foreign equipment data acquisition and processing submodule B board; The data storage module is a data storage module board; The onboard network switch board, the communication data acquisition and processing sub-module board, the domestic equipment data acquisition and processing sub-module board, the foreign equipment data acquisition and processing sub-module A board, the foreign equipment data acquisition and processing sub-module B and the data storage module board are inserted into the slots and connected together through the backplane, and the host computer is connected to the chassis.

6. The atmospheric data acquisition and control system for general aviation aircraft according to claim 3, characterized in that: The atmospheric data analysis module includes: A system configuration module, which is used for route preset, atmospheric data configuration, system settings, seeding operation settings, data transmission control, data storage configuration and macro recording control; A monitoring and display module, which is used for real-time monitoring display, operation log display, atmospheric data display, aircraft track display and track playback display; An air-to-ground communication module, which is used for atmospheric data transmission, maritime communication management, Beidou communication management, and short message transmission; The data analysis module is used for domestic equipment data analysis, foreign equipment data analysis and Ethernet data analysis.

7. The atmospheric data acquisition and control system for general aviation aircraft according to claim 5, characterized in that: The main control chip of all boards is FPGA.

8. The atmospheric data acquisition and control system for general aviation aircraft according to claim 5, characterized in that: The host computer and the chassis are connected via a 10Gbps Ethernet cable for high-speed data transmission and improved data transmission reliability.

9. The atmospheric data acquisition and control system for general aviation aircraft according to claim 5, characterized in that: The chassis has at least 6 slots.

10. The atmospheric data acquisition and control system for general aviation aircraft according to claim 7, characterized in that: The FPGA is an UltraScale series FPGA.

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