Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI

Stefano Campagnola,Javier Hernando-Ayuso,Kota Kakihara,Yosuke Kawabata,Takuya Chikazawa,Ryu Funase,Naoya Ozaki,Nicola Baresi,Tatsuaki Hashimoto,Yasuhiro Kawakatsu,Toshinori Ikenaga,Kenshiro Oguri,Kenta Oshima

IEEE Aerospace and Electronic Systems Magazine（2019）

引用 28|浏览11

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摘要

OMOTENASHE and EQUULEUS are two 6-U CubeSats by JAXA and The University of Tokyo to be launched in 2019 onboard of NASA's Exploration Mission 1. This paper presents the nominal trajectories and an overview of the mission analysis work and approaches. EQUULEUS trajectory exploits the Earth -Sun -Moon dynamics to capture the spacecraft into a libration orbit around the Earth -Moon L2 point, using on...

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关键词

CubeSat,Moon,Space vehicles,Trajectory,Orbits

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