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航天器交会远程快速自主制导方法

, PP. 1582-1586

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Abstract:

针对近地近圆轨道航天器交会任务,设计了基于经典轨道要素的远程快速自主制导算法.对于任意初始纬度幅角偏差的远程导引,通过建立纬度幅角偏差与半长轴偏差的关系,将远程导引段分为初始轨道飞行、调相轨道飞行和调整轨道飞行3个阶段.初始轨道飞行进行轨道共面修正和调相机动;在调相轨道飞行期间,进行自然调相以及调相轨道到调整轨道的机动;调整轨道飞行阶段进行追踪航天器的远地点高度和近地点高度的修正,以及再次共面修正.所有变轨机动都以制导脉冲的形式给出,并都在轨道特殊点执行.精确轨道仿真验证了远程快速自主接近制导算法的可行性.

References

[1]  Fehse W.Automated rendezvous and docking of spacecraft[M].New York:Cambridge Univ ersity Press,2003:8-28
[2]  Dufour F,Garcia J M,Bemussou J,et al.Hermes-space station phasing strategies optimization .IAF-91-345,1991
[3]  朱仁璋.航天器交会对接技术 [M].北京:国防工业出版社,2007 Zhu Renzhang.Rendezvous and docking techniques of spacecraft [M].Beijing:National Defense University Press,2007(in Chinese)
[4]  吴会英,陈宏宇,余勇,等.远距离轨道接近及绕飞控制技术研究[J].中国空间科学技术,2010,1(2):25-33 Wu Huiying,Chen Honyu,Yu Yong,et al.Study of long distance approaching and companion flying technology[J].Chinese Space Science and Technology,2010,1(2):25-33(in Chinese)
[5]  肖业伦.航天器飞行动力学原理[M].北京:宇航出版社,1995 Xiao Yelun.Concept of space craft flight dynamics[M].Beijing:Aerospace Publishing House,1995(in Chinese)
[6]  Vander V A,Forbrich D.Use of aerodynamic shape optimization for a large transonic aircraft .AA 97-2274,1997
[7]  Prussing J E.A class of optimal two-impulse rendezvous using multiple-revolution lambert solutions[J].Advances in the Astronautical Sciences,2000(106):17-39
[8]  陈统,徐世杰.基于遗传算法的最优Lambert双脉冲转移[J].北京航空航天大学学报,2007,33(3):273-277 Chen Tong,Xu Shijie.Optimal Lambert two-impulse transfer using genetic algorithm [J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(3):273-277(in Chinese)
[9]  彭坤,徐世杰,陈统.基于引导性人工免疫算法的最优Lambert变轨[J].北京航空航天大学学报,2010,36(1):6-9 Peng Kun,Xu Shijie,Chen Tong.Optimal Lambert transfer based on guiding artificial immune algorithm[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(1):6-9(in Chinese)
[10]  Carter T E.Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbit [J].Journal of Guidance Control and Dynamics,1984,7(6):710-716
[11]  Dufour F,Garcia J M,Bemussou J,et al.Hermes-space station phasing strategies optimization .IAF-91-345,1991
[12]  吴会英,陈宏宇,余勇,等.远距离轨道接近及绕飞控制技术研究[J].中国空间科学技术,2010,1(2):25-33 Wu Huiying,Chen Honyu,Yu Yong,et al.Study of long distance approaching and companion flying technology[J].Chinese Space Science and Technology,2010,1(2):25-33(in Chinese)
[13]  肖业伦.航天器飞行动力学原理[M].北京:宇航出版社,1995 Xiao Yelun.Concept of space craft flight dynamics[M].Beijing:Aerospace Publishing House,1995(in Chinese)

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