Manifold-to-manifold transfers using low-thrust acceleration

Yuri Hachiya, Yuki Kayama, Mai Bando, Shinji Hokamoto

研究成果: Contribution to journalConference article査読

抄録

This paper considers manifold-to-manifold transfers in the circular-restricted three-body problem enabled by low-thrust acceleration where an initial and target states lie on invariant manifolds associated to libration point orbits with different Jacobi constant. The basic idea is to utilize a family of stable and center manifolds that lie arbitrarily close to the target invariant manifold to reduce the cost of transfer. The linear quadratic regulator is used to design feedback control to transfer to the target manifold. Time invariant and time periodic controlleres are derived based on the linearized motion around the equilibrium point and periodic orbit respectively. The results show that the feedback controller can shape the linearized motion around manifold to be that around the equilibrium point or a periodic orbit. As a demonstration, transfer trajectories are designed to target the unstable manifold associated with an unstable Lyapunov orbit in the Earth-Moon system.

本文言語英語
論文番号IAC-19_C1_4_2_x50847
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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