Adaptive Dynamic Sliding Mode Control for Near Space Vehicles Under Actuator Faults

被引：24
作者：
Zhao, Jing [1 ]
Jiang, Bin [1 ]
Shi, Peng [2 ,3 ]
Liu, Hongtao [4 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China
[2] Victoria Univ, Coll Engn & Sci, Melbourne, Vic 8001, Australia
[3] Univ Adelaide, Sch Elect & Elect Engn, Adelaide, SA 5005, Australia
[4] Univ Toronto, Inst Aerosp Studies, Toronto, ON, Canada
来源：
CIRCUITS SYSTEMS AND SIGNAL PROCESSING | 2013年 / 32卷 / 05期
基金：
中国国家自然科学基金;
关键词：
Fault tolerant control; Actuator faults; Near space vehicles; Dynamic sliding mode; TOLERANT CONTROL; CONTROL DESIGN; ACCOMMODATION; TRACKING; SYSTEMS;
D O I：
10.1007/s00034-013-9572-9
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
A novel adaptive dynamic sliding mode (ADSM) fault-tolerant control (FTC) methodology is developed for near space vehicle attitude control systems with actuator faults in this paper. The proposed ADSM approach combines dynamic sliding mode with adaptive control strategies that can make the systems stable and accurately track the desired signals in the presence of external disturbances, model parameter uncertainties, and even actuator faults. Firstly, the attitude dynamic model of X-33 and its faulty model are introduced, then the ADSM control and fault-tolerant control laws are designed for outer-loop and inner-loop, respectively. Finally, in comparison with one existing approach, the simulation results are provided to show the effectiveness of the proposed FTC scheme.
引用
收藏
页码：2281 / 2296
页数：16
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