Adaptive Sliding Mode Backstepping Control System

Danni Wang, T. Chao, Song-yan Wang, Ming Yang
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Abstract

In order to solve the problem of stability control of moving mass reentry vehicle, a backstepping sliding mode control law based on standard backstepping control theoryis designed. Taking the perturbation of the aerodynamic parameters as the uncertain factors, the vehicle rolling angle and rolling angular velocity dual-loop sliding mode controllers are designed respectively. The virtual control of the angular velocity and the displacement command of sliding module are obtained. In the case which upper bound of the uncertainty is unknown, the adaptive method is used to design the approaching law parameters, in order to compensate for the uncertainty, and the stability of the closed-loop system is proved based on the Lyapunov function. The simulation results show that the method is effective and the tracking error is less than 0.4%.
自适应滑模反步控制系统
为了解决移动质量再入飞行器的稳定性控制问题,基于标准反步控制理论设计了一种反步滑模控制律。以气动参数的摄动为不确定因素,分别设计了飞行器滚转角和滚转角速度双环滑模控制器。得到了滑模角速度的虚拟控制和位移指令。在不确定性上界未知的情况下,采用自适应方法设计逼近律参数以补偿不确定性,并基于李雅普诺夫函数证明了闭环系统的稳定性。仿真结果表明,该方法是有效的,跟踪误差小于0.4%。
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