Optimization of multiple-impulse minimum-time rendezvous with impulse constraints using a hybrid genetic algorithm

被引:51
作者
Luo, Ya-Zhong [1 ]
Tang, Guo-Jin [1 ]
Li, Hai-yang [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp & Mat Engn, Changsha 410073, Peoples R China
关键词
multiple-impulse rendezvous; minimum-time; impulse constraints; genetic algorithm; global optimization;
D O I
10.1016/j.ast.2005.12.007
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The minimum-time multiple-impulse rendezvous with impulse constraints is investigated in this paper. Based on the Clohessy-Wiltshire (C-W) equations, an optimization model including several different kinds of impulse constraints such as the maximum impulse magnitude, the total velocity change magnitude and the time of imposing impulse for multiple-impulse minimum-time rendezvous is established. A generalized inverse matrix solution for linear equation is applied to avoid handling the terminal equality constraints. In order to obtain the global solution efficiently, a hybrid optimizer combining the advantages of a floating-coded genetic algorithm and simplex method is employed. A low-earth orbit multiple-impulse rendezvous problem is used as an example. The influence of the number of impulses, the optimization variables and the constraints on the solution is analyzed, and the different optimization algorithms are compared. Results indicate our proposed model and approach is effective in designing linearized minimum-time rendezvous trajectory with impulse constraints. (C) 2006 Elsevier SAS. All rights reserved.
引用
收藏
页码:534 / 540
页数:7
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