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contributor authorSun Zhao-wei
contributor authorDeng Hong
contributor authorZhong Wei-chao
contributor authorWu Xian-de
date accessioned2017-05-08T21:33:49Z
date available2017-05-08T21:33:49Z
date copyrightJanuary 2012
date issued2012
identifier other%28asce%29as%2E1943-5525%2E0000110.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56254
description abstractIn the space attack defensive system, a satellite is usually used to attack another satellite. To approach the target satellite successfully, path planning is very important for the attacking satellite, especially when the defensive system of the target satellite is composed of formation flying small satellites. This paper presents an environment model that is established on the relative orbit model of small satellites and changed into a static model for path planning. A genetic algorithm is used to find the optimal path. The coding rules, fitness function, and three genetic operators are designed in turn. The fitness function is found by considering region constraint, safe constraint, shortest length constraint, and crooked degree constraint. The simulation results show that the optimal path can be found with good stability and convergence, and the optimal path could satisfy requirements of security and the shortest path well.
publisherAmerican Society of Civil Engineers
titleAttacking Satellite Path Planning Based on Genetic Algorithm
typeJournal Paper
journal volume25
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000110
treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001
contenttypeFulltext


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