Design of an attitude control system by multi objective optimization considering practical operation of spacecraft equipped with control moment gyros

Ai Noumi, Takuya Kanzawa, Misuzu Haruki, Masaki Takahashi

研究成果: Conference contribution

フィンガープリント 「Design of an attitude control system by multi objective optimization considering practical operation of spacecraft equipped with control moment gyros」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

Physics & Astronomy

Engineering & Materials Science

Earth & Environmental Sciences