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
关键词
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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.
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收藏
页码:1116 / 1121
页数:6
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