Mission Trajectory Design using Three-Body Dynamics

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概要

• 論文の詳細を見る

• 〓〓〓〓 〓〓〓 〓〓 〓〓 〓〓〓〓 〓〓 〓〓〓 〓〓〓 〓〓 〓〓 〓〓〓 〓〓〓〓〓 2 〓 〓〓 (two-body problem) 〓 〓〓〓 Hohmann transfer 〓 〓〓〓〓 〓〓 Patched Conic Approximation 〓〓 〓 〓〓 〓〓〓〓〓 〓〓. Hohmann transfer 〓 〓 〓〓〓〓 〓〓 〓 〓〓〓 〓〓〓 〓 〓〓 〓〓 〓〓〓 〓〓 〓〓〓〓〓, Patched Conic Approximation 〓 〓〓〓〓 〓〓 〓〓 2 〓 〓〓〓 〓〓〓〓 〓 〓 〓〓〓 2 〓 〓〓〓 〓〓〓 Hohmann 〓〓 〓〓〓 〓〓〓〓 〓〓〓〓〓〓 〓〓 〓〓 〓〓 〓〓〓 〓 〓〓〓 〓〓〓〓. 〓 〓〓〓 〓〓〓 〓〓〓〓 〓〓〓〓 〓, 〓 〓〓〓 〓〓〓〓〓 2 〓 〓〓〓 〓, 〓〓 〓〓〓〓 〓〓 〓〓〓〓 〓〓〓 〓〓 〓〓〓〓〓 〓〓 〓〓 〓〓 〓〓〓 〓〓 〓〓〓〓 〓〓. 〓〓〓, 〓〓 〓〓 〓〓〓 〓〓 〓〓〓〓〓 〓〓 〓〓〓 〓〓〓 〓〓 〓〓〓 〓〓〓〓 〓〓〓〓 〓〓 〓〓〓 Patched Conic Approximation 〓 〓〓〓〓 〓〓〓 〓〓 〓〓〓 〓〓 (conic) 〓〓〓 〓〓〓 〓〓 〓〓 〓〓〓 〓 〓〓〓 〓〓〓 〓〓〓〓 〓〓〓 〓〓〓〓 〓〓. 〓〓 〓〓 3 〓 〓〓〓〓 〓〓〓〓 〓〓 〓 〓〓〓 〓〓〓〓 〓〓〓〓〓 〓〓〓〓〓 〓〓〓〓〓. 〓〓〓〓〓〓 〓〓〓〓 〓〓〓 〓〓 〓〓 〓 〓〓〓 〓〓〓〓 〓〓 〓〓〓〓 〓〓〓 〓〓〓 〓 〓〓 〓〓〓〓. 〓 〓〓〓〓〓 2 〓〓〓 〓〓〓 〓〓 〓〓 〓〓 〓〓〓 〓〓〓〓〓 〓〓〓 〓〓〓〓 〓〓〓〓 〓〓 〓〓〓 〓〓〓〓.

• 2010-10-21

著者

• Chung Tae-Jin

  Satellite Technology Research Center, KAIST

• Lee Na-Young

  Department of KOMPSAT-3 Systems Engineering and Integration, KARI

• Lee Na-young

  Department Of Kompsat-3 Systems Engineering And Integration Kari

• Chung Tae-jin

  Satellite Technology Research Center Kaist

関連論文

• Mission Trajectory Design using Three-Body Dynamics

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