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