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Fault diagnosis system and method for full fly-by-wire flight control

A diagnostic system and diagnostic method technology, applied in general control systems, control/adjustment systems, test/monitoring control systems, etc., can solve problems such as low accuracy, high technical level requirements for ground crews, and long time-consuming positioning, and achieve The calculation method is accurate, the statistics are comprehensive and accurate, and the effect of easy screening

Active Publication Date: 2022-05-10
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0004] In order to solve the above-mentioned technical problems, the present invention proposes a diagnostic system and method for all fly-by-wire flight control faults, which can automatically determine all possible fault causes of flight control faults, and give the corresponding fault probability and correlation of each fault cause. The circuit diagram solves the problems of time-consuming fault diagnosis and positioning of the existing flight control, low accuracy, and high technical requirements for ground crews

Method used

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  • Fault diagnosis system and method for full fly-by-wire flight control

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Embodiment 1

[0030] As the basic implementation mode of the present invention, the present invention includes a fault diagnosis system for full fly-by-wire flight control, including a fault query module, an expert knowledge base module, a fault database module and a fault record module.

[0031] The fault query module is used to provide a fault code input interface, the fault code corresponds to each fault cause, and the fault cause corresponds to the fault probability estimated by experts, the probability calculated by machine learning based on the fault database, and the recent statistics of the fault probability in the database , related circuit diagrams and troubleshooting measures to display the interface.

[0032] The expert knowledge base module is used to store technical expert knowledge, and the expert knowledge provides the failure causes of all failure codes, the expert estimated failure probability and the failure treatment method of each failure cause.

[0033] The fault datab...

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Abstract

The invention discloses a fault diagnosis system and method for a full-fly-by-wire flight control, including a fault query module, an expert knowledge base module, a fault database module and a fault record module; the invention can automatically determine the fault code according to the fault code recorded by the flight control computer All possible fault causes of the flight control fault are given, and the fault probability, fault handling measures and related circuit diagrams corresponding to each fault cause are given; the fault probability corresponding to the fault reason includes the fault probability estimated by experts, and the machine learning based on the fault database. Estimated probability and database statistics of failure probability in recent times. This method can effectively solve the problems of time-consuming fault diagnosis and positioning of the existing flight control, low accuracy, and high requirements for the technical level of ground personnel.

Description

technical field [0001] The invention belongs to the technical field of aircraft fault diagnosis, and in particular relates to a fault diagnosis system and method for a full fly-by-wire flight control. Background technique [0002] The flight control computer is the control core of the full fly-by-wire flight control system. The flight control computer receives the pilot's control commands and the electrical signals sent by the flight control sensors, and after comprehensive calculation, outputs control commands to the flight control actuators to drive the deflection of each rudder surface of the aircraft. Control the plane to fly safely. [0003] The flight control computer of the full fly-by-wire flight control system has an internal self-test function. When the flight control system fails, the flight control computer can detect the fault and record the fault for the aircraft ground maintenance personnel to diagnose the flight control fault. At present, the flight control ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0229
Inventor 徐光卫段飞杨纯宇贾鸿肖勇富源刘远东
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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