TY - GEN
T1 - Passive fault-tolerant flight controller design against actuator outages
AU - Yu, Xiang
AU - Zhang, Youmin
N1 - Publisher Copyright:
© 2014 IEEE.
PY - 2015/1/12
Y1 - 2015/1/12
N2 - A model to represent multiple actuator failure cases is developed by polytopic concept. The design of passive fault-tolerant control (FTC) with considerations of both normal and actuator failure cases is investigated, depending on the availability of actuator redundancies. By introducing the parameter dependent Lyapunov and slack methods, an improved algorithm to minimize the peak-to-peak gain of the closed-loop system is proposed. Numerical simulation studies subject to all elevon outages are conducted to illustrate the effectiveness of the designed approach to passive FTC.
AB - A model to represent multiple actuator failure cases is developed by polytopic concept. The design of passive fault-tolerant control (FTC) with considerations of both normal and actuator failure cases is investigated, depending on the availability of actuator redundancies. By introducing the parameter dependent Lyapunov and slack methods, an improved algorithm to minimize the peak-to-peak gain of the closed-loop system is proposed. Numerical simulation studies subject to all elevon outages are conducted to illustrate the effectiveness of the designed approach to passive FTC.
UR - https://www.scopus.com/pages/publications/84922575729
U2 - 10.1109/CGNCC.2014.7007384
DO - 10.1109/CGNCC.2014.7007384
M3 - 会议稿件
AN - SCOPUS:84922575729
T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
SP - 1276
EP - 1281
BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Y2 - 8 August 2014 through 10 August 2014
ER -