Paper information

Paper code

IAC-15,C1,6,10,x29702

Order

10

Room

Teddy B (ICC, lower level)

Title

Spacecraft Attitude and Total Power Optimal Control with Redundant Double-Gimbal Variable-Speed Control Moment Gyros

abstract

View PDF

Session

6. Attitude Dynamics (2)

symposium

C1. ASTRODYNAMICS SYMPOSIUM

congress

IAC-15

Type of presentation

oral

Main author

Mr. Takahiro Sasaki, Osaka Prefecture University, Japan

Co-authors

Prof. Takashi Shimomura, Osaka Prefecture University, Japan;