Formation feedback control for multiple spacecraft via virtual structures

被引:209
作者
Ren, W [1 ]
Beard, RW [1 ]
机构
[1] Brigham Young Univ, Dept Elect & Comp Engn, Provo, UT 84602 USA
来源
IEE PROCEEDINGS-CONTROL THEORY AND APPLICATIONS | 2004年 / 151卷 / 03期
关键词
D O I
10.1049/ip-cta:20040484
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the virtual structure moves too fast for the spacecraft to track due to spacecraft control saturation or the total system must sacrifice convergence speed in order to keep the spacecraft in formation. The spacecraft may also get out of formation when the system is affected by internal or external disturbances. To overcome these drawbacks, an idea of introducing formation feedback from the spacecraft to the virtual structure is illustrated in detail. An application of these ideas to multiple spacecraft interferometers in deep space is given.
引用
收藏
页码:357 / 368
页数:12
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