Adaptive nonlinear control of satellite formation flying

被引：0

作者：

de Queiroz, MS ^{[1
]}

Kapila, V ^{[1
]}

Yan, Q ^{[1
]}

机构：

[1] Polytech Univ, Dept Mech Engn, Brooklyn, NY 11201 USA

来源：

AIAA GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, VOLS 1-3: A COLLECTION OF TECHNICAL PAPERS | 1999年

关键词：

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 considers the problem of relative position control for multiple satellite formation flying (MSFF). Specifically, the full nonlinear dynamics describing the relative positioning of MSFF are used to develop a Lyapunov-based, nonlinear adaptive control law that guarantees global asymptotic convergence of the position tracking error in the presence of unknown, constant or slow-varying satellite masses, disturbance forces, and gravity forces. Simulation results are included to illustrate the controller performance.

引用

页码：1596 / 1604

页数：9

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