Manifold-based robust stationkeeping of libration-point orbit with navigational uncertainty

Y. Zhou, M. Bando, S. Hokamoto, P. L. Wu

研究成果: Contribution to journalConference article査読

抄録

This paper investigated the manifold-based robust stationkeeping approach for the halo orbit near the Earth-Moon L2 point in the ephemeris model. The well-known Hamiltonian structure-preserved (HSP) method is utilized to design the controller for stationkeeping. However, conventional HSP method is proposed under the ideal condition, where the equations of motion are constructed in the circular restricted three-body problem, and the navigational uncertainty is not considered as well. Actually, these uncertainties always exist and have significant influence on the performance of stationkeeping. To make the results more realistic, the dynamics in the ephemeris model is used to describe the motion of a spacecraft. A filtering structure-based navigation is incorporated in the stationkeeping, where the navigational uncertainty is introduced. In addition, the navigation filter is reformed to compensate for the control uncertainty. Simulation is performed to observe the influence of the control gain and the magnitude of the uncertainty on the stationkeeping performance.

本文言語英語
論文番号IAC-19_C1_9_10_x50194
ジャーナルProceedings of the International Astronautical Congress, IAC
2019-October
出版ステータス出版済み - 2019
イベント70th International Astronautical Congress, IAC 2019 - Washington, 米国
継続期間: 10 21 201910 25 2019

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 天文学と天体物理学
  • 宇宙惑星科学

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