Optimal low-thrust orbital transfers in a central gravity field

被引：0
|
作者：
B. N. Kiforenko
机构：
[1] Taras Shevchenko National University,
来源：
International Applied Mechanics | 2005年 / 41卷
关键词：
spacecraft; optimal control; multirevolution trajectory; averaging method;
D O I：
暂无
中图分类号：
学科分类号：
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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