Fuel optimal propulsive maneuver of an experimental structure exhibiting spacelike dynamics

被引：15

作者：

Meyer, JL

Silverberg, L

机构：

[1] Mars Mission Research Center, North Carolina State University, Raleigh

[2] Mechanical and Aerospace Engineering, Mars Mission Research Center, North Carolina State University, Raleigh

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1996年 / 19卷 / 01期

关键词：

D O I：

10.2514/3.21591

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The implementation of four fuel-optimal methods for propulsive maneuver of space structures is described. Toward this end, an experimental structure that possessed spacelike dynamics was fabricated and used to test the previously mentioned fuel optimal methods. The results given highlight the differences among fuel optimal methods for propulsive maneuver of space structures, their relative strengths and weaknesses, and the sources of errors.

引用

页码：141 / 149

页数：9

共 28 条

[1]

BOSSI JA, 1986, 1986 P AM CONTR C, P1034

[2]

BROWN ME, 1983, THESIS MIT CAMBRIDGE

[3] ACTIVE VIBRATION ABSORBER FOR THE CSI EVOLUTIONARY MODEL - DESIGN AND EXPERIMENTAL RESULTS [J].