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基于遗传算法的单站测速数据定初轨技术研究
引用本文:王西京,李栋林,马鹏斌,秋宏兴.基于遗传算法的单站测速数据定初轨技术研究[J].飞行力学,2004,22(4):53-56.
作者姓名:王西京  李栋林  马鹏斌  秋宏兴
作者单位:西安卫星测控中心,在轨卫星管理室,陕西,西安,710043
摘    要:只有单站测速数据的情况下,传统的定轨方法难以实现初轨确定.将遗传算法应用于定轨实践,实现了无初值条件下单站测速数据初始轨道确定,并能满足收敛要求,为缓解测控资源紧张提供了重要支持.在中巴“资源一号“卫星的长期测控任务中应用,证明了本方法的有效性.

关 键 词:初轨确定  测速数据  遗传算法
文章编号:1002-0853(2004)04-0053-04
修稿时间:2003年9月22日

Research of Initial Orbit Determination with Doppler Measurement Data of One TT&C Station Based on Genetic Algorithms
WANG Xi-jing,LI Dong-lin,MA Peng-bin,QIU Hong-xing.Research of Initial Orbit Determination with Doppler Measurement Data of One TT&C Station Based on Genetic Algorithms[J].Flight Dynamics,2004,22(4):53-56.
Authors:WANG Xi-jing  LI Dong-lin  MA Peng-bin  QIU Hong-xing
Abstract:It's hard to determine the initial orbit for traditional methods with Doppler measurement data of only one TT&C station. We introduce a genetic algorithm to determine the satellite's initial orbit. With the Doppler data of only one TT&C station, the new method can satisfy the requirement of constringency and get the initial orbit parameters. It has successfully been used to determine the initial orbit of the Chinese-Brazil resource of earth satellite for one year. Less equipment is needed than before to manage the satellites in orbit.
Keywords:initial orbit determination  measurement data  genetic algorithm
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