USE OF THE GRADIENT METHOD FOR SOLUTION OF CERTAIN SPACEFLIGHT DYNAMICS PROBLEMS.

被引:0
|
作者
Ponomareva, V.L.
机构
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The gradient method is applied to the problem of optimal parametric control with limited time for performance of a maneuver. As an example, the problem of obtaining maximum angle of rotation of the orbital plane of a satellite with limited reserve of characteristic velocity and specified time for performance of the maneuver is solved.
引用
收藏
页码:283 / 287
相关论文
共 50 条