Database construction method used for fault detection of unmanned aerial vehicle flight control system

A flight control system and fault detection technology, applied in general control systems, control/regulation systems, testing/monitoring control systems, etc., can solve problems such as the difficulty in implementing UAV flight control systems and the inability to adapt to fault feature extraction. The effect of ensuring real-time characteristics, improving recall rate and correct rate, and reducing false alarm rate

Active Publication Date: 2017-05-10
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0009] The purpose of the present invention is to address the above-mentioned deficiencies in the background technology and provide a database construction method for the fault detection of the UAV flight control system, which realizes the fault detection database of the UAV flight control system by extracting normal data features online in real time The dynamic construction of the UAV flight control system solves the technical problem that the fault detection of the UAV flight control system cannot meet the needs of abnormal detection because it is difficult to extract each fault feature

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  • Database construction method used for fault detection of unmanned aerial vehicle flight control system

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Embodiment Construction

[0018] Combine below figure 1 The technical solution of the invention is described in detail. In order to solve the technical problem that the fault detection of the UAV flight control system cannot meet the requirements of abnormal detection because it is difficult to extract each fault feature, the present invention proposes a data-driven database for the fault detection of the UAV flight control system. The construction method is to train the historical database at each moment in real time to obtain the fault judgment rule at each moment and filter out the reference database composed of normal historical data at each moment, and use the fault judgment rule at each moment to process the fault judgment rule at the corresponding moment. Real-time observation data, integrate the normal data in the real-time flight control data of the UAV into the reference database and then update the historical database. By dynamically updating the reference database composed of normal histori...

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Abstract

The invention discloses a database construction method used for the fault detection of an unmanned aerial vehicle flight control system, and belongs to the technical field of the fault detection of an unmanned aerial vehicle. Normal unmanned aerial vehicle real-time flight control data screened through a judging rule is blended into historical data; whether unmanned aerial vehicle flight control data of an unknown fault at a future moment fails or not is judged through the judging rule trained according to the historical data; a reference database formed by normal historical data is dynamically updated so as to guarantee the real-time update of the judging rule and guarantee the real-time characteristic performance of the reference database formed by the normal historical data; and the judging rule which is dynamically updated can effectively detect various exceptional forms including isolated point exception, context exception, accumulation exception and the like in the unmanned aerial vehicle flight control data so as to effectively improve the recall ratio and the accuracy of fault detection and simultaneously lower a false alarm rate.

Description

technical field [0001] The invention discloses a database construction method for fault detection of a flight control system of an unmanned aerial vehicle, and belongs to the technical field of fault detection of unmanned aerial vehicles. Background technique [0002] In recent years, with the introduction of the concept of failure prediction and health management (PHM) to the integrated management system of UAVs, the demand for informationization and intelligence of UAV safety management is increasing. The core part of UAV safety management - safety monitoring and abnormal early warning, can comprehensively monitor the health status of UAVs, which is of great significance to improve UAV safety performance, ensure maintenance efficiency, and reduce life cycle. As the core component of the UAV, the flight control system of the UAV is composed of a variety of sensors, network links, execution devices and other subsystems. The flight control sensor measures the real-time flight...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/30G05B23/02
CPCG05B23/0243G06F16/21
Inventor 孙蕊张羽成胡明华
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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