月軟着陸簡易問題の解法と最適軌道計算<II>

概要

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