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A Ground Integrated Debugging and Verification Platform for Avionics Flight Control System

A technology of flight control system and verification platform, which is applied in general control system, control/adjustment system, test/monitoring control system, etc., can solve the problem of less research on joint debugging and test verification system, and improve the reliability of system testing. Visibility, improved operability, and improved real-time test response

Active Publication Date: 2021-07-13
国营芜湖机械厂
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AI Technical Summary

Problems solved by technology

However, there are few studies on the joint debugging and test verification system of the avionics system and the flight control system

Method used

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  • A Ground Integrated Debugging and Verification Platform for Avionics Flight Control System

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Embodiment Construction

[0037] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further elaborated below.

[0038] Such as figure 1 The system composition diagram shown:

[0039] A ground comprehensive debugging and verification platform for avionics flight control system, including an avionics test system 2 for testing, simulating, and emulation, a flight control test system 3 for simulating a real operating environment, and a test system for avionics testing 2. A cross-link control system 4 interactively connected to the flight control test system 3. The avionics test system 2 is connected to the flight control test system 3 with the object 1 under test.

[0040] The avionics testing system 2 includes centralized management equipment 21 , comprehensive testing equipment 22 , flight simulation module 23 , exciter and simulator 24 , avionics system simulator 25 , general and auxiliary equipm...

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Abstract

The invention relates to a ground comprehensive debugging and verification platform for an avionics flight control system, including an avionics test system for testing, simulating, and simulating, a flight control test system for simulating a real operating environment, and a test system for avionics testing The cross-link control system, which is interactively connected with the flight control test system, completes the comprehensive test of the avionics system and flight control system of the tested object. The invention can be used for testing and maintaining the avionics system and the flight control system of the aircraft, improves the comprehensive control and interactive control ability of the system, improves the operability of the verification platform, the real-time responsiveness of the test, and the visibility and interactivity of the test.

Description

technical field [0001] The invention relates to the technical field of aviation airborne equipment testing, in particular to a ground comprehensive debugging and verification platform for an avionics flight control system. Background technique [0002] New aircraft airborne systems usually consist of structure, avionics, flight control and weapon systems. As the "brain" and "nerve center" of the aircraft, the avionics system mainly completes the functions related to the flight mission; the flight control system, as the control system of the flight movement of the aircraft, mainly completes the functions related to the pilot's safe and effective control of the aircraft. The two occupy an important position in the airborne system. Joint debugging and joint testing is the last link in the entire testing and debugging process of airborne avionics and flight control systems. It is a systematic, interdisciplinary and integrated comprehensive test carried out on the basis of the c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0213
Inventor 吴传贵周章勇郑永龙胡伟许海朱维玮韩梁阚艳
Owner 国营芜湖机械厂
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