CONTROL SYSTEM DESIGN AND SIMULATION OF SPACECRAFT FORMATIONS VIA LEADER-FOLLOWER APPROACH

被引：0
|
作者：
Reyhanoglu, Mahmut [1 ]
机构：
[1] Embry Riddle Aeronaut Univ, Dept Phys Sci, Daytona Beach, FL 32114 USA
来源：
SPACEFLIGHT MECHANICS 2009, VOL 134, PTS I-III | 2009年 / 134卷
关键词：
ATTITUDE-CONTROL; MULTIPLE; COORDINATION; SCHEME;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents an effective leader-follower based control scheme for spacecraft formations. Modifying earlier established control design techniques, passivity-based feedback laws are constructed to control translational and rotational motion of a group of spacecraft. Computer simulations are carried out to illustrate the effectiveness of the control laws. The ephemeris and attitude data generated through the simulations are used to create 3D visualizations.
引用
收藏
页码：141 / 152
页数：12
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