Multi-model soft switching tracking control for near-space interceptor based on the disturbance observer

被引:1
|
作者
Guo, Chao [1 ]
Liang, Xiao-Geng [1 ,2 ]
Wang, Jun-Wei [3 ]
机构
[1] Northwestern Polytech Univ, Sch Automat, Xian, Peoples R China
[2] Luoyang Optoelectro Technol Dev Ctr, Luoyang, Peoples R China
[3] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
基金
中国国家自然科学基金;
关键词
Near-space interceptor; disturbance observer; soft switching; robust least-squares weighted control allocation; linear matrix inequalities; ROBUST AUTOPILOT DESIGN; CONTROL ALLOCATION; ATTITUDE TRACKING; NONLINEAR-SYSTEMS; RIGID SPACECRAFT; SLIDING MODES; MISSILE; REJECTION; GUIDANCE;
D O I
10.1177/0959651814565436
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A disturbance observer-based multi-model soft switching tracking control design is proposed for the near-space interceptor. Initially, based on the Takagi-Sugeno modeling approach, a slow-fast loop soft switching model is employed to approximately describe the nonlinear dynamics of the near-space interceptor. Subsequently, a disturbance observer is constructed to estimate the unknown disturbance. Based on the disturbance observer, a descriptor system approach is proposed to solve the multi-model soft switching tracking control design problem. The suggested controller can not only ensure the stability of the closed-loop near-space interceptor system but also provide an upper bound of the cost function. Moreover, a robust least-squares weighted control allocation algorithm is employed to distribute the virtual control command among the redundant actuators (the aerodynamic fins and reaction jets). Finally, simulation results demonstrate the effectiveness of the proposed control scheme.
引用
收藏
页码:1077 / 1092
页数:16
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