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应急轨道机动变轨方案快速设计算法
引用本文:石俊,韩潮.应急轨道机动变轨方案快速设计算法[J].北京航空航天大学学报,2007,33(4):388-391.
作者姓名:石俊  韩潮
作者单位:北京航空航天大学,宇航学院,北京,100083;北京航空航天大学,宇航学院,北京,100083
摘    要:为了满足应急轨道机动过程中测控约束和时间、燃料资源等各方面的要求 ,提出了一种变轨方案快速设计算法.给出了适用于变量搜索的轨道机动变轨模式,将变轨 方案快速设计问题转化成了约束优化问题;建立了完整的测控约束数学模型和对测控约束的 处理算法;然后利用遗传算法搜索出了同时满足测控约束条件和优化目标的变轨方案.算例 表明,利用此算法设计得到的变轨方案,能够满足应急轨道机动任务的需要.

关 键 词:轨道机动  优化  遗传算法  航天器
文章编号:1001-5965(2007)04-0388-04
收稿时间:2006-04-28
修稿时间:2006-04-28

Quick algorithm for designing emergency orbital transfer scheme
Shi Jun,Han Chao.Quick algorithm for designing emergency orbital transfer scheme[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(4):388-391.
Authors:Shi Jun  Han Chao
Institution:School of Astronautics, Beijing University of Aeronautics and As tronautics, Beijing 100083, China
Abstract:A quick algorithm for designing emergency orbital transfer scheme that can meet the requirements of measure,fuel and time during emergency orbital transfer was presented.The orbital transfer mode suitable for variable search was given.The question of designing orbital transfer scheme quickly was transformed into the question of restricted optimization.And the entire mathematics model of measure restrictions was established and the corresponding algorithm for measure restrictions was presented.Orbital transfer scheme,that is required not only to meet measure restrictions,but also to achieve optimal goal,was found by using genetic algorithm.Cases of calculation show that the orbital transfer schemes designed by using this quick algorithm can meet the need of emergency orbital transfer mission.
Keywords:orbital transfer  optimization  genetic algorithms  spacecraft
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