A method of generating the trajectory of in-orbit assembly of large space structures using the algorithms of optimization on graphs

被引：0
|
作者：
Glumov, VM [1 ]
Krutova, IN [1 ]
Sukhanov, VM [1 ]
机构：
[1] Russian Acad Sci, Trapeznikov Inst Control Sci, Moscow, Russia
来源：
AUTOMATION AND REMOTE CONTROL | 2005年 / 66卷 / 09期
基金：
俄罗斯基础研究基金会;
关键词：
6;
D O I：
10.1007/s10513-005-0178-y
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A formalism of matrix description of the trajectory of in-orbit erection of large space structures was proposed. The objective functions that can be minimized to establish the optimal erection trajectory guaranteeing the least impact of the basic control on the flexible-structure dynamics were formulated. A software package for computer-aided support of the procedure generating a set of feasible erection trajectories of the large space structures and using the well-known approach to optimization on graphs to specify the optimal trajectory was developed.
引用
收藏
页码：1371 / 1383
页数：13
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