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Trajectory and Correction Maneuver During the Transfer from Earth to Halo Orbit 被引量:8

Halo轨道转移及中途修正问题研究(英文)
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摘要 This article addresses the design of the trajectory transferring from Earth to Halo orbit, and proposes a timing closed-loop strategy of correction maneuver during the transfer in the frame of circular restricted three body problem (CR3BP). The relation between the Floquet multipliers and the magnitudes of Halo orbit is established, so that the suitable magnitude for the aerospace mission is chosen in terms of the stability of Halo orbit. The stable manifold is investigated from the Poincar6 mapping defined which is different from the previous researches, and six types of single-impulse transfer trajectories are attained from the geometry of the invariant manifolds. Based on one of the trajectories of indirect transfer which are ignored in the most of literatures, the stochastic control theory for imperfect information of the discrete linear stochastic system is applied to design the trajectory correction maneuver. The statistical dispersion analysis is performed by Monte-Carlo simulation, This article addresses the design of the trajectory transferring from Earth to Halo orbit, and proposes a timing closed-loop strategy of correction maneuver during the transfer in the frame of circular restricted three body problem (CR3BP). The relation between the Floquet multipliers and the magnitudes of Halo orbit is established, so that the suitable magnitude for the aerospace mission is chosen in terms of the stability of Halo orbit. The stable manifold is investigated from the Poincar6 mapping defined which is different from the previous researches, and six types of single-impulse transfer trajectories are attained from the geometry of the invariant manifolds. Based on one of the trajectories of indirect transfer which are ignored in the most of literatures, the stochastic control theory for imperfect information of the discrete linear stochastic system is applied to design the trajectory correction maneuver. The statistical dispersion analysis is performed by Monte-Carlo simulation,
作者 徐明 徐世杰
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2008年第3期200-206,共7页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (10702003) Innovation Foundation of Beijing University of Aeronautics and Astronautics for Ph.D. Graduates
关键词 libration point Halo orbit orbit design trajectory correction maneuver stochastic control theory Monte-Carlo simulation libration point Halo orbit orbit design trajectory correction maneuver stochastic control theory Monte-Carlo simulation
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