首页 | 本学科首页   官方微博 | 高级检索  
     检索      

太阳帆航天器行星际轨道转移优化算法
引用本文:钱航,郑建华.太阳帆航天器行星际轨道转移优化算法[J].空间控制技术与应用,2012,38(1):18-22,28.
作者姓名:钱航  郑建华
作者单位:1. 中国科学院空间科学与应用研究中心,北京100190;中国科学院研究生院,北京100190
2. 中国科学院空间科学与应用研究中心,北京,100190
基金项目:太阳帆民用航天资助项目
摘    要:研究基于遗传算法的太阳帆行星际转移轨道的全局优化问题.通过极小值原理推导了太阳帆全局优化控制律,并以太阳帆飞行时间最短为优化目标函数,运用遗传算法对发射时间、到达时间和协态变量初值进行参数优化设计.为了解决轨道转移这一多约束优化问题,在遗传算法中加入动态罚函数.在此理论基础上作了从地球同步轨道出发到火星同步轨道转移和从地球出发与火星交会两个算例,仿真结果表明了该方法在太阳帆转移轨道全局优化中的有效性.

关 键 词:太阳帆  全局优化  遗传算法  转移轨道  罚函数

Optimization Algorithm for Interplanetary Transfer Trajectories of Solar-Sail Spacecraft
QIAN Hang , ZHENG Jianhua.Optimization Algorithm for Interplanetary Transfer Trajectories of Solar-Sail Spacecraft[J].Aerospace Contrd and Application,2012,38(1):18-22,28.
Authors:QIAN Hang  ZHENG Jianhua
Institution:1(1.Center for Space Science and Applied Research,Chinese Academy of Sciences,Beijing 100190,China; 2.Graduate University of Chinese Academy of Sciences,Beijing 100190,China)
Abstract:Minimum-time orbit transfers for solar sail spacecraft base on genetic algorithm(GA) are explored.The optimal control law is derived from the maximum principle,minimum time consumption is chosen as the optimization objective,and the launch date,the arrive date and the initial guess of the co-states are optimized by using GA.In order to deal with the design of transfer orbit with many constraints,the penalty function is introduced into the GA.Orbit transfers for solar sail from Earth’s synchronous heliocentric orbit to Mars’ synchronous heliocentric orbit and from Earth to Mars have been designed and simulated as examples.Results of simulation show correctness and practicability of proposed orbit transfer algorithm.
Keywords:solar sail  global optimization  genetic algorithm(GA)  transfer orbit  penalty function
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号