Paper information

Paper code

IAC-14,C1,5,12,x26813

Order

12

Room

801A

Title

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

abstract

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Session

5. Guidance, Navigation and Control (1)

symposium

C1. ASTRODYNAMICS SYMPOSIUM

congress

IAC-14

Type of presentation

oral

Main author

Ms. Ai Noumi, Keio University, Japan

Co-authors

Mr. Takuya Kanzawa, Japan Aerospace Exploration Agency (JAXA), Japan;

Ms. Misuzu Haruki, Japan Aerospace Exploration Agency (JAXA), Japan;

Dr. Masaki Takahashi, Keio University, Japan;