Adaptive synchronization control of multiple spacecraft formation flying

被引：34
|
作者：
Liu, Hong-Tao
Shan, Jinjun
Sun, Dong
机构：
[1] Univ Toronto, Inst Aerosp Studies, N York, ON M3H 5T6, Canada
[2] York Univ, Dept Earth & Space Sci & Engn, N York, ON M3J 1P3, Canada
[3] City Univ Hong Kong, Dept Mfg Engn & Engn Management, Hong Kong, Hong Kong, Peoples R China
来源：
JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME | 2007年 / 129卷 / 03期
关键词：
D O I：
10.1115/1.2719772
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
An adaptive nonlinear synchronization control approach is developed for multiple spacecraft formation flying with elliptical reference orbits. It can guarantee that both the tracking errors and the synchronization errors of the relative positions converge to zero globally, even in the presence of uncertain parameters. The generalized synchronization concept allows us to design various synchronization errors so that different synchronization performance can be obtained. Simulation results of a leader follower spacecraft pair and the maneuvering of multiple spacecraft in formation flying are presented to verify the effectiveness of the proposed control technique.
引用
收藏
页码：337 / 342
页数：6
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