Attitude Stability of a Spinning Spacecraft During Appendage Deployment/Retraction
Symposium, Flight mechanics/estimation theory ; 1994 ; Greenbelt; MD
Flight mechanics/estimation theory ; 3265 ; 447-450
NASA CONFERENCE PUBLICATION ; 3265
1994-01-01
4 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2003
|The Attitude Control of Small Spacecraft with Movable Appendage
British Library Conference Proceedings | 2003
|