DocumentCode :
176508
Title :
Robust fault tolerant control of under-actuated VTOL aircraft
Author :
Jiang Yuanqing ; Yang Hao ; Jiang Bin
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2014
fDate :
May 31 2014-June 2 2014
Firstpage :
3196
Lastpage :
3201
Abstract :
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.
Keywords :
actuators; aircraft control; asymptotic stability; control system synthesis; entry, descent and landing (spacecraft); fault diagnosis; fault tolerant control; feedback; linearisation techniques; nonlinear control systems; observers; optimal control; reduced order systems; robust control; trajectory optimisation (aerospace); actuator fault; asymptotic stability; asymptotic trajectory tracking; cascade observer; close loop system; coordinate transformation; decoupled reduced order observer design; decoupled tracking subsystem; fault estimation; faulty system; feedback linearization; nonlinear nonminimum phase VTOL aircraft; nonlinear robust fault tolerant control scheme; robust optimal feedback controller design; subsystem stabilization; underactuated VTOL aircraft; unknown disturbance estimation; vertical take-off and landing; Aircraft; Educational institutions; Fault diagnosis; Fault tolerance; Fault tolerant systems; Observers; Robustness; Disturbance Observer; Fault Diagnosis; Fault Tolerant Control; Non-minimum Phase; Vertical Take-off and Landing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
Type :
conf
DOI :
10.1109/CCDC.2014.6852725
Filename :
6852725
Link To Document :
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