Adaptive Backstepping Control for Longitudinal Dynamics of Hypersonic Vehicle Subject to Actuator Saturation and Disturbance

被引:2
|
作者
Jia, Zhiqiang [1 ,2 ]
Li, Tianya [2 ]
Lu, Kunfeng [2 ]
机构
[1] Beijing Inst Technol, Sch Automat, Beijing, Peoples R China
[2] Beijing Aerosp Automat Control Inst, Beijing, Peoples R China
关键词
FLIGHT CONTROL; TRACKING CONTROL; CONTROL DESIGN; INVERSION; AIRCRAFT; OBSERVER;
D O I
10.1155/2019/1019621
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, an adaptive backstepping control strategy is presented to solve the longitudinal control problem for a hypersonic vehicle (HSV) subject to actuator saturation and disturbances. Small perturbation linearization transforms the dynamics to a seconded-order system at each trimming point, with total disturbance including unmodeled dynamics, parametric uncertainties, and external disturbances. The disturbance can be estimated and compensated for by an extended state observer (ESO), and thus the system is decoupled. To deal with the actuator saturation and wide flight envelope, an adaptive backstepping control strategy is designed. A rigorous proof of finite-time convergence is provided applying Lyapunov method. The effectiveness of the proposed control scheme is verified in simulations.
引用
收藏
页数:10
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