Research on collision prediction & avoidance strategy of formation flying

Zhenqi He, Ke Zhang, Meibo Lv, Jingyu Wang
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引用次数: 1

Abstract

In the satellite formation task, due to a satellite failure or formation task change, it is necessary to reconstruct the formation. In the process of reconfiguration of satellites, satellites anti-collision research is one of the most important links. In this paper, by collapsing the initial covariance matrix of the satellite, the collision probability density function is integrated in the region containing the satellite. The collision probability of formation satellites is obtained. When the collision probability is greater than the security threshold, two avoidance strategies (increase the long axis of the formation satellites and increase the track drift distance of the formation satellites) are proposed based on the Gaussian perturbation equation. The simulation experiments show that the method has great significance for the collision between satellites.
编队飞行碰撞预测与避碰策略研究
在卫星编队任务中,由于卫星故障或编队任务发生变化,需要对编队进行重构。在卫星重构过程中,卫星的抗碰撞研究是最重要的环节之一。本文通过折叠卫星的初始协方差矩阵,在包含卫星的区域内积分碰撞概率密度函数。得到了编队卫星的碰撞概率。当碰撞概率大于安全阈值时,基于高斯摄动方程,提出了增大编队卫星长轴和增大编队卫星航迹漂移距离两种避碰策略。仿真实验表明,该方法对卫星间碰撞具有重要意义。
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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