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Finite-Time Reentry Attitude Control Based on Adaptive Multivariable Disturbance Compensation

机译:基于自适应多变量扰动补偿的有限时间再入姿态控制

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摘要

The finite-time tracking control for reusable launch vehicle with unmatched disturbance is investigated. An adaptive-multivariable-disturbance-compensation scheme is proposed to provide the estimation for external disturbances where the bounds of the perturbations are not known. Based on the estimation, a continuous multivariable homogeneity second order sliding mode controller is designed to ensure that the attitude tracking is achieved in finite time. A proof of the finite-time convergence of the closed-loop system under the integrated controller and disturbance observer is derived using the Lyapunov technique. The features of the proposed control scheme are that it does not require any information on the bounds of the disturbance and its gradient except for their existence. At the same time, the finite-time convergence, nominal performance recovery, and chattering alleviation are guaranteed. Finally, some simulation tests are provided to demonstrate the effectiveness of the proposed control scheme.
机译:研究了无匹配干扰的可重复使用运载火箭的有限时间跟踪控制。提出了一种自适应多变量扰动补偿方案,以提供扰动范围未知的外部扰动的估计。基于该估计,设计了一个连续的多变量同质二阶滑模控制器,以确保在有限的时间内完成姿态跟踪。利用Lyapunov技术推导了集成控制器和扰动观测器下闭环系统的有限时间收敛性的证明。所提出的控制方案的特征在于,除了存在扰动及其梯度之外,它不需要任何有关扰动范围及其梯度的信息。同时,保证了有限时间的收敛,名义性能的恢复和抖动的减轻。最后,提供了一些仿真测试以证明所提出的控制方案的有效性。

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