Optimal low-thrust orbital transfers in a central gravity field

被引:0
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作者
B. N. Kiforenko
机构
[1] Taras Shevchenko National University,
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关键词
spacecraft; optimal control; multirevolution trajectory; averaging method;
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摘要
The results of studying some problems of optimization of low-thrust transfers between arbitrary elliptic orbits in a Newtonian gravity field are expounded. An approximate solution obtained by the averaging method is presented. Analytical solutions of the averaged equations are given for a wide class of maneuvers. The problem of constructing numerical solutions to the exact equations of motion of a spacecraft between high orbits is discussed
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页码:1211 / 1238
页数:27
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