Optimal Collision Avoidance Maneuver Control for Formation Flying Satellites Using Linear Programming

被引：0

作者：

Hu Min ^{[1
]}

Zeng Guoqiang ^{[2
]}

Yao Hong ^{[1
]}

Liu Yanbo ^{[1
]}

机构：

[1] Acad Equipment Command & Technol, Beijing 101416, Peoples R China

[2] Nation Univ Def Technol, Inst Aerosp & Mat Engn, Changsha 410073, Hunan, Peoples R China

来源：

PROCEEDINGS OF THE 29TH CHINESE CONTROL CONFERENCE | 2010年

关键词：

Collision Avoidance; Formation Flying; Configuration Safety; Optimization; Linear Programming;

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：

The safety of the close formation flying satellites in the cross-track plane is studied. Based on the description of the geometry of formation configuration in the cross-track plane, the target formation configuration is expressed by the parameters of the safe ellipse which remains out of the avoidance region, and is optimized by Newton method. The problem to control the satellites to reach the safe ellipse is solved in the framework of linear programming algorithms. A numeric simulation is given to validate the effectiveness of the proposed method.

引用

页码：3390 / 3393

页数：4

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