OPTIMAL LOW-THRUST EARTH-MOON TRANSFERS WITH A SWITCHING FUNCTION-STRUCTURE

被引:0
|
作者
KLUEVER, CA [1 ]
PIERSON, BL [1 ]
机构
[1] IOWA STATE UNIV SCI & TECHNOL,DEPT AEROSP ENGN & ENGN MECH,AMES,IA 50011
来源
JOURNAL OF THE ASTRONAUTICAL SCIENCES | 1994年 / 42卷 / 03期
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
A new minimum-fuel, Earth-Moon trajectory problem is examined for a low-thrust spacecraft with engine thrust magnitude controlled by a switching function. The problem is solved in the context of the restricted three-body problem. A direct method is applied to predict the nature of the switching function and allow good initial guesses for the two-point boundary value problem solution. An iterative method is developed which effectively leads to the two-point boundary value problem solution. Several optimal planar Earth-Moon transfers are obtained for a range of fixed end-times. Results are presented for multiple-burn cases ranging from 2 burn/1 coast to 5 burn/4 coast solutions.
引用
收藏
页码:269 / 283
页数:15
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