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

页码：269 / 283

页数：15

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