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Control strategy of optimal deployment for spacecraft solar array system with initial state uncertai
[期刊论文] 作者:Xinsheng GE,Qijia YAO,Liqun CH,
来源:黑龙江科技学院学报 年份:2018
为探究吕家坨井田地质构造格局,根据钻孔勘探资料,采用分形理论和趋势面分析方法,研究了井田7...
Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral met
[期刊论文] 作者:Xinsheng GE,Zhonggui YI,Liqun CHEN,,
来源:Applied Mathematics and Mechanics(English Edition) 年份:2017
The attitude optimal control problem(OCP) of a two-rigid-body spacecraft with two rigid bodies coupled by a ball-in-socket joint is considered. Based on conserv...
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