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Approaches for a Tether-Guided Landing of an Autonomous Helicopter

机译:自主直升机的系绳引导着陆方法

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摘要

In this paper, we address the design of an autopilot for autonomous landing of a helicopter on a rocking ship, due to rough sea. A tether is used for landing and securing a helicopter to the deck of the ship in rough weather. A detailed nonlinear dynamic model for the helicopter is used. This model is underactuated, where the rotational motion couples into the translation. This property is used to design controllers which separate the time scales of rotation and translation. It is shown that the tether tension can be used to couple the translation of the helicopter to the rotation. Two controllers are proposed in this paper. In the first, the rotation time scale is chosen much shorter than the translation, and the rotation reference signals are created to achieve a desired controlled behavior of the translation. In the second, due to coupling of the translation of the helicopter to the rotation through the tether, the translation reference rates are created to achieve a desired controlled behavior of the attitude and altitude. Controller A is proposed for use when the helicopter is far away from the goal, while Controller B is for the case when the helicopter is close to the ship. The proposed control schemes are proved to be robust to the tracking error of its internal loop and results in local exponential stability. The performance of the control system is demonstrated by computer simulations. Currently, work is in progress to implement the algorithm using an instrumented model of a helicopter with a tether.
机译:在本文中,我们讨论了自动驾驶仪的设计,该设计可在波涛汹涌的海上自动将直升机降落在摇摆船上。系绳用于在恶劣天气下将直升机降落并固定在船甲板上。使用了直升机的详细非线性动力学模型。该模型驱动不足,旋转运动耦合到平移中。此属性用于设计将旋转和平移时间刻度分开的控制器。结果表明,系链张力可用于将直升机的平移与旋转耦合。本文提出了两种控制器。首先,选择旋转时间标度比平移短得多,并创建旋转参考信号以实现所需的平移受控行为。第二,由于直升飞机的平移与通过系绳的旋转耦合,因此创建了平移参考速率以实现所​​需的姿态和高度受控行为。建议在直升机远离目标时使用控制器A,而控制器B用于在直升机靠近船舶的情况下使用。实践证明,所提出的控制方案对于其内部回路的跟踪误差具有鲁棒性,并导致局部指数稳定性。控制系统的性能通过计算机仿真得到证明。当前,正在进行使用带有绳索的直升机的仪器模型来实现算法的工作。

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