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A Study on Earth-Moon Transfer Orbit Design

No, Tae-Soo;Lee, Ji-Marn;Jeon, Gyeong-Eon;Lee, Dae-Ro;Kim, Ghang-Ho

  • 투고 : 2011.12.10
  • 심사 : 2012.03.06
  • 발행 : 2012.03.30

초록

Optimal transfer trajectories based on the planar circular restricted three body problem are designed by using mixed impulsive and continuous thrust. Continuous and dynamic trajectory optimization is reformulated in the form of discrete optimization problem. This is done by the method of direct transcription and collocation. It is then solved by using nonlinear programming software. Two very different transfer trajectories can be obtained by the different combinations of the design parameters. Furthermore, it was found out that all designed trajectories permit a ballistic capture by the Moon's gravity. Finally, the required thrust profiles are presented and they are analyzed in detail.

키워드

Earth-Moon transfer;Three body problem;Optimization;Nonlinear programming

참고문헌

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피인용 문헌

  1. Fast and accurate analyses of spacecraft dynamics using implicit time integration techniques vol.14, pp.2, 2016, https://doi.org/10.5139/IJASS.2012.13.1.106
  2. Solution for Nonlinear Three-Dimensional Intercept Problem with Minimum Energy vol.2013, 2013, https://doi.org/10.5139/IJASS.2012.13.1.106

과제정보

연구 과제 주관 기관 : National Research Foundation of Korea (NRF)