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

机译:再入阶段可重复使用运载火箭的有限时间自适应终端滑模控制器设计

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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.
机译:针对具有外部干扰和参数不确定性的再入RLV的6-DOF模型,提出了一种新型的有限时间自适应终端滑模控制器。首先,根据多个时标特征,将姿态运动的动力学分为姿态角子系统和姿态角速率子系统。通过使用自适应定律估计干扰和不确定性的上限,可以设计每个子系统的控制器。此外,证明了每个子系统的状态都可以在有限的时间内到达滑动表面。通过仿真说明了该控制器的有效性。

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