2109 多目的遺伝的アルゴリズムを用いたイプシロンロケットの軌道最適化(乗り物・交通・リサイクル)

Abstract

DESTINY is injected to long elliptical orbit by Epsilon rocket launcher. If the apogee altitude of the injected orbit is high enough, it is achieved to ease the requirements for design and operation of the spacecraft. This paper investigates the ability of trajectory injection by means of 4-stage Epsilon rocket using the method of multi objective optimization under several flight constraints.