Robust Attitude Control of Near Space Vehicles with Time-varying Disturbances

被引:100
作者
Chen, Mou [1 ]
Jiang, Bin [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Backstepping control; disturbance observer; flight control; near space vehicles; robust control; TRACKING CONTROL; ACTUATOR DYNAMICS; FLIGHT CONTROL; SYSTEMS; OBSERVER;
D O I
10.1007/s12555-012-0237-4
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, the robust attitude control scheme is developed for near space vehicles (NSVs) with time-varying disturbances based on backstepping technique. To efficiently handle the time-varying disturbance and the system uncertainty, the disturbance observer is employed to estimate them. Using backstepping technique and the disturbance observer output, the robust attitude control is firstly developed for the NSV. And then, considering the actuator dynamics, another robust attitude control scheme is proposed for the NSV based on the disturbance observer. The uniformly ultimate boundedness of all closed-loop signals are guaranteed via Lyapunov analysis under both developed robust attitude control schemes. Finally, simulation results are presented to illustrate the effectiveness of the proposed attitude control schemes.
引用
收藏
页码:182 / 187
页数:6
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