Time-fuel Optimal Pulse Traversal Method for Relative Orbit Spacecraft

被引：0

作者：

Gao, Yufeng ^{[1
]}

Sun, Yanchao ^{[1
]}

Li, Chuanjiang ^{[1
]}

Ban, Xiaojun ^{[1
]}

机构：

[1] Harbin Inst Technol, Harbin 150001, Heilongjiang, Peoples R China

来源：

PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017) | 2017年

关键词：

Relative orbit spacecraft; pulse traversal; time-fuel optimal; on-orbit service;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Relative orbit transfer and on-orbit target observation are important contents of spacecraft on-orbit service, and it is also required to conform the optimal control performance index. In this paper, a time-fuel optimal pulse traversal method is proposed. It divides the space around the target spacecraft into several spatial grids and the spacecraft traverses the subdivision grids under pulse control. The orbit optimal control and on-orbit observation tasks realize. Finally, the simulation is simulated and the performance indexes of different traversal order are compared.

引用

页码：6225 / 6230

页数：6

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