月軟着陸簡易問題の解法と最適軌道計算<I>

概要

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The purpose of this paper is to learn and understand the definition and solution of the minimal fuel control problem and time-optimal control problem about the linear motion of an object. The terminal phase of Lunar Soft Landing by a space flying body is used as the subject, and the solutions can be obtained analytically on the simple problems. Further, the optimal trajectory and the kinematic behavior were computed numerically from the analytic solutions, and the consideration was given to these synodic problems.
岐阜工業高等専門学校の論文
2000-03-01