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
收藏
页码：1116 / 1121
页数：6
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