Cooperate control algorithm for spacecraft formation flying based on consensus theory

被引：0

作者：

Bi P. ^{[1
]}

Luo J.-J. ^{[1
]}

Zhang B. ^{[1
]}

机构：

[1] Northwestern Polytechnical University

来源：

Yuhang Xuebao/Journal of Astronautics | 2010年 / 31卷 / 01期

关键词：

Attitude control; Configuration control; Consensus problem; Spacecraft formation flying;

D O I：

10.3873/j.issn.1000-1328.2010.01.011

中图分类号：

学科分类号：

摘要：

In order to realize the cooperativity of the spacecraft formation flying, a spacecraft formation flying control algorithm based on consensus theory was proposed in this paper. Firstly, the consensus problem of the spacecraft formation flying was discussed. Secondly, the 6-DOF dynamics model of the spacecraft formation flying was established. Finally, a nonlinear control law was designed utilizing the consensus theory. The simulation result shows that the control algorithm is effective, which could also be applied to dynamic communication topology within the spacecraft formation flying.

引用

页码：70 / 74

页数：4

共 6 条

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[3] Chung S.J., Nonlinear control and synchronization of multiple lagrangian systems with application to tethered formation flight spacecraft, (2007)
[4] Wei R., Multi-vehicle consensus with a time-varying reference state, Systems & Control Letters, 56, 7-8, pp. 474-483, (2007)
[5] Long X.-L., Network-based multi-robot system research, (2007)
[6] Hassan K., Khalil, Nonlinear Systems, Third Edition, pp. 437-449, (2005)

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