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Fault reconstruction method based on PD (Proportional Differential) type learning observer

A technology of fault reconstruction and observer, which is applied in the direction of instruments, adaptive control, control/regulation systems, etc., and can solve problems such as missed faults

Inactive Publication Date: 2019-07-09
CIVIL AVIATION UNIV OF CHINA
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  • Application Information

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Problems solved by technology

However, for early micro-faults and slow-changing faults, the above method is prone to fault under-reporting.

Method used

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  • Fault reconstruction method based on PD (Proportional Differential) type learning observer
  • Fault reconstruction method based on PD (Proportional Differential) type learning observer
  • Fault reconstruction method based on PD (Proportional Differential) type learning observer

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Embodiment Construction

[0083] The preferred embodiments of the present invention will be described below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0084] The invention provides a fault reconstruction method based on a PD-type learning observer. The fault reconstruction method uses a robust PD-type iterative learning observer. By introducing a robust performance index, the designed iterative learning observer has a Interference and measurement noise are robust, and a systematic gain matrix solution method is given by using the linear matrix inequality technique, and when this fault reconstruction method is applied to the actuator fault reconstruction problem of the UAV longitudinal control system, its beneficial effect will be Especially notable.

[0085] Such as figure 1 as shown, figure 1 It is a schematic ...

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Abstract

The invention discloses a fault reconstruction method based on a PD (Proportional Differential) type learning observer. The method comprises the following steps that: taking an unmanned aerial vehicleas a rigid body, ignoring the inertia product of the unmanned aerial vehicle, and selecting a corresponding state variable to construct the state-space equation of the longitudinal flight control system of the unmanned aerial vehicle; on the basis of the constructed state-space equation, constructing a PD-type iterative learning observer; defining a state estimation error, an output estimation error and a fault reconstruction error, and according to the constructed state-space equation and the constructed PD-type iterative learning observer, obtaining a corresponding error equation; setting the infinite norm of an executor fault matrix to be bounded, utilizing the PD-type iterative learning observer to reconstruct executor additive faults, and according to the error equation, enabling thestate estimation error and the fault reconstruction error to be stabilized in a preset interval, wherein the output estimation error meets a preset standard. By use of the method, a purpose of constructing the PD-type iterative learning observer to realize accurate fault reconstruction is realized, and the accuracy of accurate reconstruction is improved.

Description

technical field [0001] The invention relates to the technical field of fault reconstruction, in particular to a fault reconstruction method based on a PD type learning observer. Background technique [0002] As an effective method to improve system security and reliability, Fault Diagnosis and Fault Tolerant Control (FTC) technology has attracted widespread attention from experts and scholars at home and abroad. Fault diagnosis mainly includes: fault detection, fault separation, and fault reconstruction. Its main tasks are: judging whether a fault occurs, locating the location and type of the fault, and determining the size and change trend of the fault. The model-based fault detection and isolation (FDI) method mainly detects and isolates system faults by designing a residual generator and comparing the residual with a threshold. However, for early micro-faults and slowly-varying faults, the above method is prone to fault under-reporting. Contents of the invention [00...

Claims

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Application Information

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IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 王蕊王成杰孙辉
Owner CIVIL AVIATION UNIV OF CHINA
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