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考虑碰撞避免的多航天器智能轨道相位控制

历鉴 张刚

南京航空航天大学学报(英文版)2022,Vol.39Issue(4):379-388,10.
南京航空航天大学学报(英文版)2022,Vol.39Issue(4):379-388,10.

考虑碰撞避免的多航天器智能轨道相位控制

Multi-spacecraft Intelligent Orbit Phasing Control Considering Collision Avoidance

历鉴 1张刚1

作者信息

  • 1. 哈尔滨工业大学卫星技术研究所,哈尔滨150080,中国
  • 折叠

摘要

Abstract

This paper proposes an intelligent low-thrust orbit phasing control method for multiple spacecraft by simultaneously considering fuel optimization and collision avoidance. Firstly,the minimum-fuel orbit phasing control database is generated by the indirect method associated with the homotopy technique. Then,a deep network representing the minimum-fuel solution is trained. To avoid collision for multiple spacecraft,an artificial potential function is introduced in the collision-avoidance controller. Finally,an intelligent orbit phasing control method by combining the minimum-fuel neural network controller and the collision-avoidance controller is proposed. Numerical results show that the proposed intelligent orbit phasing control is valid for the multi-satellite constellation initialization without collision.

关键词

轨道相位控制/小推力/深度神经网络/碰撞规避

Key words

orbit phasing control/low thrust/deep neural networks/collision avoidance

分类

航空航天

引用本文复制引用

历鉴,张刚..考虑碰撞避免的多航天器智能轨道相位控制[J].南京航空航天大学学报(英文版),2022,39(4):379-388,10.

基金项目

This work was supported in part by the National Natural Science Foundation of China(No.11772104),in part by the Key Research and Development Plan of Heilongjiang Province(No.GZ20210120),and in part by the Fundamental Research Funds for the Central Uni-versities. (No.11772104)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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