Robust Fault Tolerant Control of Under-actuated VTOL Aircraft

被引:0
|
作者
Jiang Yuanqing [1 ]
Yang Hao [1 ]
Jiang Bin [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
关键词
Non-minimum Phase; Fault Diagnosis; Vertical Take-off and Landing; Disturbance Observer; Fault Tolerant Control; NONMINIMUM-PHASE SYSTEMS; TRACKING CONTROL; STABILIZATION; INVERSION; OBSERVER;
D O I
暂无
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 paper presents a nonlinear robust fault tolerant control scheme to force the faulty system to asymptotically track a given desired trajectory via cascade observers. Focusing on the external disturbance and actuator faults of the nonlinear non-minimum phase vertical take-off and landing aircraft, two decoupled reduced order observers are designed to estimate the unknown disturbance and fault. By using the coordinate transformation and feedback linearization, two decoupled tracking subsystem are decomposed from the overall system, then two robust optimal feedback controllers are designed respectively to stabilize the two subsystems. And on this basis, the robust fault tolerant controller is proposed by using the fault estimation, which can make the overall close-loop system asymptotically stable. The effectiveness of the presented method is demonstrated by simulation results.
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页码:3196 / 3201
页数:6
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