Flight Evaluation of an LPV Sliding Mode Observer for Sensor FTC

被引:7
|
作者
Chen, L. [1 ]
Alwi, H. [2 ]
Edwards, C. [2 ]
Sato, M. [3 ]
机构
[1] Cranfield Univ, Sch Aerosp Transport & Mfg, Cranfield MK43 0AL, Beds, England
[2] Univ Exeter, Coll Engn Math & Phys Sci, Exeter EX4 4QF, Devon, England
[3] Japan Aerosp Explorat Agcy, Mitaka Ku, Tokyo 1810015, Japan
基金
欧盟地平线“2020”;
关键词
Fault detection and diagnosis (FDD); fault-tolerant control (FTC); flight test; sliding mode control; FAULT-DETECTION; PERTURBATIONS; SYSTEMS;
D O I
10.1109/TCST.2021.3096946
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This brief develops a sliding mode sensor faulttolerant control scheme for a class of linear parameter varying (LPV) systems. It incorporates a sliding mode observer that reconstructs the unknown sensor faults based on only the system inputs and outputs. The reconstructed sensor faults are used to compensate for the corrupted sensor measurements before they are used in the feedback controller. Provided accurate fault estimates can be computed; near nominal control performance can be retained without any controller reconfiguration. Furthermore, the closed-loop stability of the fault-tolerant control (FTC) scheme, involving both a sliding mode controller and a sliding mode observer, is rigorously analyzed. The proposed scheme is validated using the Japan Aerospace Exploration Agency's Multipurpose Aviation Laboratory (MuPAL-alpha) research aircraft. These flight tests represent the first validation tests of a sliding mode sensor FTC scheme on a full-scale aircraft.
引用
收藏
页码:1319 / 1327
页数:9
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