Finite-time adaptive terminal sliding mode controller design for reusable launch vehicle in reentry phase

Chen Liu, Chaoyang Dong, Weilai Jiang
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引用次数: 3

Abstract

This paper proposed a novel finite-time adaptive terminal sliding mode controller for 6-DOF model of reentry RLV with external disturbance and parameters uncertainty. First, according to the multiple time scale features, the dynamics of attitude motion are divided into attitude angle subsystem and attitude angular rate subsystem. By estimating the upper bound of disturbance and uncertainty with an adaptive law, the controller for each subsystem can be designed. Also, the states of each subsystem can reach sliding surface in finite time is proved. The validity of this controller is illustrated by simulation.
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可重复使用运载火箭再入段有限时间自适应终端滑模控制器设计
针对存在外部干扰和参数不确定性的再入RLV六自由度模型,提出了一种新的有限时间自适应末端滑模控制器。首先,根据多时间尺度特征,将姿态运动动力学分为姿态角子系统和姿态角速率子系统;利用自适应律估计扰动和不确定性的上界,设计各子系统的控制器。并证明了各子系统的状态可以在有限时间内到达滑动面。仿真结果表明了该控制器的有效性。
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