Adaptive nonlinear control of spacecraft near Sun-Earth L2 lagrange point

被引：0

作者：

Wong, H ^{[1
]}

Kapila, V ^{[1
]}

机构：

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

来源：

PROCEEDINGS OF THE 2003 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2003年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper, an adaptive control algorithm is presented to enable a spacecraft to track desired trajectories near the L-2 Lagrange point in the Sun-Earth system. An adaptive full-state feedback control law, designed using a Lyapunov-type analysis, exhibits globally asymptotic position tracking in the presence of the unknown spacecraft mass. The control law is simulated for a Lyapunov orbit in the vicinity of the L-2 Lagrange point as the periodic reference trajectory.

引用

页码：1116 / 1121

页数：6

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