Point navigation guidance for small unmanned helicopter under predicting future position

Jangho Lee, Jindeog Chung
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Abstract

Following the path of an autonomous, an agile vehicle in a dynamic environment is a very complex problem, especially one is required to use its full maneuvering capabilities facing crosswind condition. To resolve this issue, using bank angle to change direction of helicopter is the new trend of the current researches. This paper introduces a new point navigation guidance law which is useful for the control of the unmanned helicopter. Predicting the future position, generating the guidance law and commanding the heading are used as means of input. The suggested method differs from the conventional guidance law which is directly used the reorienting logic in the direction of flight velocity instead of directly applying bank angle. Results of simulation show that the proposed law correctly guides an unmanned helicopter along the path within a given area. Also the flight test verified the effectiveness and performance of the proposed guidance law. The proposed guidance law can be extended to the collision avoidance with a minor tuning of law.
预测未来位置的小型无人直升机点导航制导
动态环境下的敏捷车辆跟随自动驾驶汽车的路径是一个非常复杂的问题,特别是在侧风条件下需要充分发挥其机动能力。为了解决这一问题,利用倾斜角度改变直升机的方向是当前研究的新趋势。本文提出了一种新的点导航制导律,用于无人直升机的控制。以预测未来位置、生成制导律和指挥航向为输入方式。该方法不同于传统制导律直接采用飞行速度方向的重定向逻辑,而不是直接应用倾斜角。仿真结果表明,该算法能正确地引导无人直升机在给定区域内沿路径飞行。飞行试验也验证了所提制导律的有效性和性能。所提出的导引律可以通过对导引律进行微调而推广到避碰问题中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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