Design and Simulation of Satellite Formation Flying Reconfiguration Controlling Method

被引：0

作者：

Li Yibo ^{[1
]}

Liu Yanmei ^{[1
]}

Song Qi ^{[1
]}

Xu Jin ^{[1
]}

机构：

[1] Shenyang Univ Aeronaut & Astronaut, Sch Automat, Shenyang, Peoples R China

来源：

2010 8TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA) | 2010年

关键词：

formation flying of satellites; Hill equations; linear-quadratic regulator; reconfiguration control;

D O I：

10.1109/WCICA.2010.5553752

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper investigated the problem of formation flying reconfiguration control of satellite. A simulation method based on STK and Matlab for the satellites formation reconfiguration control was introduced. Control strategy using linear-quadratic regulator techniques was presented. Relative dynamical models of formation flying were introduced, and based on the circular reference orbit, Hill equations were deduced. At last, Linear-quadratic regulator was adopted to perform the formation flying reconfiguration. The simulation results verified the validity of the model and the controller.

引用

页码：3410 / 3413

页数：4