Coupled attitude and orbit control for relative motion of underactuated spacecraft

被引:0
|
作者
Wu, Jin-Jie [1 ]
Liu, Kun [1 ]
Han, Da-Peng [1 ]
Zhang, Feng [1 ]
机构
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
来源
Kongzhi yu Juece/Control and Decision | 2014年 / 29卷 / 06期
关键词
Nonlinear programming;
D O I
10.13195/j.kzyjc.2013.0463
中图分类号
学科分类号
摘要
引用
收藏
页码:969 / 978
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