DocumentCode :
231322
Title :
A real-time assessment approach to quadrotor flight control capability
Author :
Liu Bin ; Zhao Zhiyao ; Yang Binxian ; Quan Quan ; Cai Kai-Yuan
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
3112
Lastpage :
3117
Abstract :
To solve the problem for the online assessment of the quadrotor flight control capability, this paper proposes a novel definition of control capability, and an approach to assess the control capability online. A quadrotor fault model is presented firstly, and the real-time fault detection is implemented using an Extended Kalman filter. Then, the function fitting method is used to achieve real-time controlability calculation by obtaining the relation between the controllability and the estimated fault vector. Finally, the online assessment of control capability is achieved by the integration of the controllability and the performance factor of the control law. A simulation based on a quadrotor shows that the proposed approach can achieve an accurate online assessment of quadrotor flight control capability.
Keywords :
Kalman filters; autonomous aerial vehicles; controllability; fault tolerant control; helicopters; control law performance factor; controllability calculation; extended Kalman filter; fault vector estimation; function fitting method; quadrotor fault model; quadrotor flight control capability; realtime assessment approach; realtime fault detection; Aerospace control; Educational institutions; Electronic mail; Hafnium; Kalman filters; Monte Carlo methods; Real-time systems; Control Capability; Controllability; Extended Kalman Filter; Quadrotor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6895449
Filename :
6895449
Link To Document :
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