首页> 外文会议>Autonomic and Autonomous Systems, 2009. ICAS '09 >Autonomous Unmanned Helicopter Landing System Design for Safe Touchdown on 6DOF Moving Platform
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Autonomous Unmanned Helicopter Landing System Design for Safe Touchdown on 6DOF Moving Platform

机译:6自由度移动平台上安全着陆的自主无人直升机着陆系统设计

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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:在这项研究中,设计了一种自适应控制系统,用于在6自由度移动平台上的无人直升机着陆阶段进行安全着陆。在本文中,着陆阶段分为进近阶段和着陆阶段。在第一个阶段,直升机尝试减弱初始位置和方向误差,在第二阶段,跟踪平台的姿态以实现安全着陆。所提出的控制系统的分层结构包括监督和跟踪级别。监控层识别着陆阶段,跟踪层控制并基于SDRE(状态相关的Riccati方程)方法补偿误差。在不同情况下,通过计算机仿真评估着陆系统的鲁棒性和性能。结果表明,在移动平台上着陆阶段,设计的控制系统的跟踪性能令人满意。

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