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Time-Optimal Trajectory Generation for Landing a Quadrotor Onto a Moving Platform

机译:将四旋翼飞机降落到移动平台上的时间最优轨迹生成

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摘要

We propose a time-optimal trajectory generation algorithm for landing a quadrotor onto a translating (heaving) and tilting (pitching) platform. The proposed algorithm exploits the differential flatness of the system dynamics and optimizes the trajectory in the space of system flat outputs, i.e., system states and their derivatives. This reformulation of the problem improves computational efficiency and can incorporate input and state constraints during the landing maneuver, such as collision avoidance and time-varying final state constraints. In order to verify the optimality of the solution obtained from the proposed algorithm, a switching time search mechanism is also proposed for a subclass of time-optimal trajectory generation problems. Experimental results demonstrating the landing of a quadrotor onto a moving platform are presented to verify the effectiveness of the proposed trajectory generation algorithm.
机译:我们提出了一种时间最优的轨迹生成算法,用于将四旋翼飞机降落到平移(升沉)和倾斜(俯仰)平台上。提出的算法利用了系统动力学的微分平坦度,并优化了系统平坦输出空间中的轨迹,即系统状态及其导数。问题的这种改进提高了计算效率,并且可以在着陆操作期间合并输入和状态约束,例如避免碰撞和时变的最终状态约束。为了验证从所提出的算法获得的解的最优性,还针对时间最优轨迹生成问题的子类提出了切换时间搜索机制。实验结果表明了四旋翼飞机着陆到移动平台上,以验证所提出的轨迹生成算法的有效性。

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