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Autonomous Unmanned Helicopter Landing System Design for Safe Touchdown on 6DOF Moving Platform

机译:自动无人直升机着陆系统设计,用于6dof移动平台的安全触控

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In this research, an adaptive control system is designed for a safe touchdown of an unmanned helicopter during its landing phase on a 6DOF moving platform. In this paper the landing phase is divided into the approach and touchdown stages. In the first stage, the helicopter tries to attenuate the initial position and direction errors and in the next stage, the platform's attitude is tracked for a safe touchdown. The hierarchical structure of the proposed control system includes supervisory and tracking levels. The supervisory level recognizes the landing stage and the tracking level controls and compensates the errors based on SDRE (State Dependent Riccati Equation) method. The robustness and performance of the landing system is evaluated by computer simulation in different scenarios. The results show satisfactory tracking performance of the designed control system during landing phase on a moving platform.
机译:在该研究中,自适应控制系统设计用于在6DOF移动平台上的着陆阶段期间安全触地达到无人直升机。在本文中,着陆阶段分为近视阶段。在第一阶段,直升机试图衰减初始位置和方向误差,并在下一个阶段,跟踪平台的态度以进行安全触地得分。所提出的控制系统的层次结构包括监督和跟踪水平。监督水平识别着陆阶段和跟踪级别控制,并根据SDRE(状态相关的Riccati方程)方法来补偿错误。在不同场景中的计算机模拟评估着陆系统的鲁棒性和性能。结果显示了在移动平台上的着陆阶段期间设计控制系统的令人满意的跟踪性能。

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