Sliding Mode Controller Based on Genetic Algorithm and Simulated Annealing for Assured Crew Reentry Vehicle

被引:1
|
作者
Vijay, Divya [1 ]
Jayashree, R. [1 ]
机构
[1] BS Abdur Rahman Crescent Inst Sci & Technol, Dept Elect & Elect Engn, Chennai 600048, Tamil Nadu, India
关键词
Attitude control system; Re-entry; Assured crew re-entry vehicle (ACRV); Quaternions; Genetic algorithm (GA); Simulated annealing (SA); Pulse width pulse frequency (PWPF) modulators; Thrusters; ATTITUDE-CONTROL SCHEMES; OPTIMIZATION; TRACKING; SYSTEMS;
D O I
10.1061/JAEEEZ.ASENG-4131
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A sliding mode (SM) re-entry control system is proposed for an assured crew re-entry vehicle (ACRV). The vehicle has a low lift/drag ratio (0.3). The trajectory controller drives the ACRV in a predefined track. The reference vectors for the attitude controller are generated by the trajectory controller and navigation system. The feedback SM controller is designed to accommodate the structural parametric uncertainties and environmental disturbances. The SM controller is optimized by both the genetic algorithm (GA) and the simulated annealing (SA) methods. A comparative study is done between both optimization methods and the efficiency of the SA method is proved. The system is subjected to a sensitivity study in terms of various thrust torque profiles. A robustness check is done by changing the system parameters. A pulse width pulse frequency (PWPF) modulator modulates the output torque dictated by the attitude controller. The simulation results demonstrate the proposed method's effectiveness in achieving the various required parameters.
引用
收藏
页数:23
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