Analytical Solution of the Problem on an Axisymmetric Spacecraft Attitude Maneuver Optimal with Respect to a Combined Functional

被引:0
作者
Ya. G. Sapunkov
A. V. Molodenkov
机构
[1] Institute for Problems of Precision Mechanics and Control,
[2] Russian Academy of Sciences,undefined
来源
Automation and Remote Control | 2021年 / 82卷
关键词
optimal control; spacecraft; axisymmetric rigid body; analytical solution;
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学科分类号
摘要
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页码:1183 / 1200
页数:17
相关论文
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