A control and detection integrated launch control system

By integrating online detection units and control units into a unified launch control system, the problems of insufficient equipment maintainability and space occupation have been solved. This has enabled the miniaturization of launch control equipment and rapid fault location, thereby improving equipment reliability and detection efficiency.

CN115755730BActive Publication Date: 2025-11-25GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
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Patent Information

Application Number
CN202211580571.8
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2022-12-09
Publication Date
2025-11-25
Estimated Expiration
2042-12-09

AI Technical Summary

Technical Problem

Existing launch control equipment lacks integrated testing methods, resulting in insufficient maintainability. Furthermore, separate control and testing modules increase equipment space requirements and development costs, hindering miniaturization.

Method used

An integrated control and detection transmission control system was designed. By integrating an online detection unit and a control unit, and utilizing a test CPU and a control CPU for signal acquisition and control, the transmission control and detection are unified, reducing external equipment and interconnection cables, and improving the timeliness of signal detection and acquisition rate.

Benefits of technology

This reduces the space occupancy of launch control equipment, improves the efficiency of fault location and troubleshooting, enhances the reliability and maintainability of the equipment, and meets the requirements for equipment miniaturization.

✦ Generated by Eureka AI based on patent content.

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Abstract

The application provides a kind of control and detection integration launch control system;Including online detection unit and control unit, the online detection unit and control unit are connected with peripheral interface;The application integrates the launch control part and detection part of launch control equipment, while meeting the launch control, can avoid increasing external detection equipment, reduce the interconnection cable and detection signal pressure drop caused by external equipment, reduce the space occupancy of launch control system, increase the timeliness and acquisition rate of signal detection, detect the fault of equipment through test, isolate the fault to the specified replaceable unit, which is beneficial to the rapid positioning and elimination of fault.
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Description

TECHNICAL FIELD

[0001] The present application relates to a control and detection integrated launch control system. BACKGROUND

[0002] Under the condition of rapid development of informatization, the degree of automation, electrification, digitization and intelligence of the launch control equipment of the aircraft is higher and higher, so that various faults may occur in the use and test of the launch control equipment, and the control equipment is required to have high reliability and safety. Under the new situation, the launch control equipment should be able to effectively deal with various unexpected situations, quickly test and maintain, and ensure the effective operation of the ground launch control system under the condition of simple launch area site facilities.

[0003] Most of the existing launch control equipment does not have detection means, which causes insufficient maintainability of the equipment and shortens the life cycle of the equipment. The control equipment with detection means mostly separates the control module and the detection module for independent operation, which not only increases the development cost, but also increases the installation space, which is not conducive to the development of small equipment. For example, a control system based on a meteorological detection rocket disclosed in CN112783023A takes a DSP processor module as the core, connects with the ground control system through a CAN bus communication module, communicates with other systems through an RS-422 serial communication module, and detects the power supply parameters of the rocket through an AD acquisition circuit, but the control and detection are separated into two systems, which increases the required space of the control system. SUMMARY

[0004] To solve the above technical problems, the present application provides a control and detection integrated launch control system.

[0005] The present application is realized by the following technical solutions.

[0006] The present application provides a control and detection integrated launch control system; comprising an online detection unit and a control unit, the online detection unit and the control unit are connected with an external interface;

[0007] The online detection unit comprises a test CPU, the test CPU is connected with a CSAD module, the CSAD module is connected with an AD signal board and a CSDL module respectively, and the AD signal board and the CSDL module are connected with the external interface;

[0008] The control unit comprises a control CPU, the control CPU is connected with a COM module and a KIO module through a CAN bus, the KIO module is connected with an FKDY module, and the COM module, the KIO module and the FKDY module are connected with the external interface.

[0009] The control CPU completes the reception and feedback of the control instructions between the external devices through the CAN bus.

[0010] The control CPU controls the COM module to complete 1-way synchronous clock input and 8-way full-duplex RS422 communication according to the communication protocol of the peripheral device.

[0011] The KIO module controls 90-way digital output and 56-way single-end input through the control CPU.

[0012] The FKDY module receives the digital quantity of the KIO module and sends the transmission logic to the peripheral device.

[0013] The test CPU collects the digital quantity output by the FKDY under the control of the control CPU and sends it to the peripheral device.

[0014] The beneficial effects of the present application are that the transmission control part and the detection part of the transmission control device are integrated, which can avoid increasing external detection devices, reduce the interconnection cable and detection signal pressure drop caused by external devices, reduce the space occupancy of the transmission control system, increase the timeliness and collection rate of signal detection, detect the fault of the device through testing, isolate the fault to the specified replaceable unit, and facilitate the rapid positioning and elimination of the fault. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 is the system principle of the present application;

[0016] Figure 2 is a structural schematic view of the present application;

[0017] 1 - box, 2 - COM board, 3 - control CPU board, 4 - KIO board, 5 - test CPU board, 6 - AD board, 7 - ADB board, 8 - FKDY board, 9 - CSDL board, 10 - power supply, 11 - BUS board. DETAILED DESCRIPTION

[0018] The technical solutions of the present application are further described below, but the scope of protection is not limited to the description.

[0019] As shown in Figure 1 , a control and detection integrated transmission control system; comprising an online detection unit and a control unit, the online detection unit and the control unit are connected with a peripheral device interface;

[0020] The online detection unit comprises a test CPU, the test CPU is connected with a CSAD module, the CSAD module is connected with an AD signal board and a CSDL module respectively, and the AD signal board and the CSDL module are connected with the peripheral device interface.

[0021] The control unit comprises a control CPU, the control CPU is connected with the COM module and the KIO module through the CAN bus, the KIO module is connected with the FKDY module, and the COM module, the KIO module and the FKDY module are connected with peripheral interfaces.

[0022] The control CPU receives and feeds back control instructions between the peripheral and the control CPU through the CAN bus.

[0023] The control CPU controls the COM module to complete 1-way synchronous clock input and 8-way full-duplex RS422 communication according to the communication protocol of the peripheral.

[0024] The KIO module controls 90-way digital output and 56-way single-end input through the control CPU.

[0025] The FKDY module receives the digital quantity of the KIO module and sends the transmission logic to the peripheral.

[0026] The test CPU collects the digital quantity output by the control CPU to the FKDY and sends it to the peripheral.

[0027] As shown in Figure 2 An embodiment of the application is shown in the figure, the device mainly comprises a box, a connector, a control CPU board, a COM board, a KIO board, a test CPU board, an AD signal board, an ADB board, a CSDL1 board, a CSDL2 board, an FKDY board, a BUS board, a filter assembly, a power module, a state indicating lamp and software. The connector, the BUS board, the filter assembly and the power module are integrated through the box, and the control CPU board, the COM board, the KIO board, the test CPU board, the AD signal board, the ADB board, the CSDL1 board, the CSDL2 board and the software are integrated through the BUS board.

[0028] The specific process is: the working power supply passes through the filtering assembly and the power module, and then the equipment is started. When different input signals of external equipment enter the equipment through the connector, the following working process is entered: through the control software, the control instruction receiving and feedback between the equipment and the external equipment are completed through the CAN communication of the control CPU board, and meanwhile, according to the communication protocol requirements between the external equipment and the equipment, the control COM board completes 1-way synchronous clock input and 8-way full-duplex RS422 communication, and through the bus control KIO board, 90-way digital output (0V-24V) and 56-way single-ended input (0V-24V) are completed, and the transmitting logic flow is completed by the FKDY board driven by the digital output of the KIO board. At the same time, the data line and the address line of the test CPU board are used to complete the acquisition control and data reading of the ADB board, the ADB board completes the digital-to-analog conversion of the voltage signals processed by the AD signal board, the CSDL1 board and the CSDL2 board, and 24-way (0mA-20mA) current signals, 40-way (0A-20A) current signals and 114-way (0V-30V) voltage signals can be acquired, and the detection data can be sent to the external equipment through the RS-422 communication interface and the Ethernet interface on the test CPU board. In order to quickly understand the information of the equipment, the running state and the communication state can be observed from the state indicating lamp on the equipment panel.

Claims

1. An integrated transmission control system for controlling and detecting, comprising an online detection unit and a control unit, characterized in that: The online detection unit and the control unit are connected with the peripheral interface; The online detection unit comprises a test CPU connected with a CSAD module, the CSAD module is connected with an AD signal board and a CSDL module, and the AD signal board and the CSDL module are connected with the peripheral interface; The control unit comprises a control CPU connected with a COM module and a KIO module through a CAN bus, the KIO module is connected with an FKDY module, and the COM module, the KIO module and the FKDY module are connected with the peripheral interface; The control CPU receives and feeds back the control instructions between the control CPU and the peripheral interface through the CAN bus; The control CPU controls the COM module to complete 1-way synchronous clock input and 8-way full-duplex RS422 communication according to the communication protocol of the peripheral interface; The KIO module controls 90-way digital output and 56-way single-end input through the control CPU; The FKDY module receives the digital quantity of the KIO module and sends the transmission logic to the peripheral interface; The test CPU collects the digital quantity output by the FKDY and sends it to the peripheral interface.

Citation Information

Patent Citations

  • Control system based on meteorological detection rocket

    CN112783023A