Neural Network-Based Spacecraft Leader-Follower Trajectory Tracking Control

N. Zhou, Xuanxuan Zhao, Kuibao Zhu
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引用次数: 0

Abstract

In this paper, the problem of leader-follower formation tracking with multiple rigid spacecraft is studied. Considering the leader directed graph case, the goal is to drive all spacecraft to precisely track the desired trajectory. Firstly, the multi-spacecraft cooperative trajectory tracking problem is transformed into each spacecraft’s trajectory tracking problem by a distributed control algorithm. Second, the position controller is developed for position tracking under a hierarchical control framework. An applied force and a nonsingular desired attitude are calculated from the command force. Then, an adaptive neural network controller is used to approximate the applied force and ensure that the spacecraft’s attitude reaches a point of balance. Finally, numerical examples prove the utility of the algorithm.
基于神经网络的航天器Leader-Follower轨迹跟踪控制
研究了多刚体航天器的leader-follower编队跟踪问题。考虑领头有向图情况,目标是驱动所有航天器精确地跟踪期望轨迹。首先,利用分布式控制算法将多航天器协同轨迹跟踪问题转化为单个航天器的轨迹跟踪问题;其次,在层次控制框架下,开发了用于位置跟踪的位置控制器。由指挥力计算出施加力和非奇异期望姿态。然后,利用自适应神经网络控制器对载荷进行逼近,保证航天器姿态达到一个平衡点;最后,通过数值算例验证了该算法的实用性。
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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