Finite-Time Super Twisting Disturbance Observer-Based Backstepping Control for Body-Flap Hypersonic Vehicle

被引:1
|
作者
Liu, Daiming [1 ,2 ]
Min, Changwan [1 ,2 ]
Cui, Jiashan [1 ,2 ]
Li, Fei [3 ]
Feng, Dongzhu [1 ,2 ]
Dai, Pei [1 ,2 ]
机构
[1] Xidian Univ, Sch Aerosp & Technol, Xian 710071, Peoples R China
[2] Minist Educ, Key Lab Equipment Efficiency Extreme Environm, Xian 710126, Peoples R China
[3] China Acad Launch Vehicles, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
body-flap hypersonic vehicle; super twisting algorithm; disturbance observer; backstepping control; SLIDING MODE CONTROL;
D O I
10.3390/math11112460
中图分类号
O1 [数学];
学科分类号
0701 ; 070101 ;
摘要
This paper investigates the attitude control problem for underactuated body-flap hypersonic vehicles (BFHSVs) with mixed disturbances. First, the control-oriented model for BFHSV is introduced. Then, an improved finite-time super twisting disturbance observer (STDO) is designed. Finite-time convergence of estimate error and smoother inputs are achieved. Meanwhile, a parametric command method is introduced to calculate the differential of inputs which can enhance the dynamic response of the closed-loop system. Subsequently, the virtual control signal is derived by a second-order filter to avoid the differential explosion problem. The overall stability of the closed-loop system is demonstrated by applying the Lyapunov stability theory. Finally, the performance of the proposed control scheme is evaluated through extensive and comparative numerical simulations under multiple disturbances.
引用
收藏
页数:14
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