Aeronautics and astronautics – Spacecraft – Attitude control
Reexamination Certificate
2006-04-11
2006-04-11
Keith, Jack (Department: 3663)
Aeronautics and astronautics
Spacecraft
Attitude control
C244S158700
Reexamination Certificate
active
07025307
ABSTRACT:
A method and an apparatus for controlling the attitude and momentum of a spacecraft while deploying an appendage from the spacecraft. The method uses solar tacking and similar techniques to produce differential solar torques that are used to control the momentum and attitude of the spacecraft during the appendage deployment.
REFERENCES:
patent: 4325124 (1982-04-01), Renner
patent: 4949922 (1990-08-01), Rosen
patent: 5816540 (1998-10-01), Murphy et al.
patent: 5906339 (1999-05-01), Basuthakur et al.
patent: 6032903 (2000-03-01), Fowell et al.
patent: 6076773 (2000-06-01), Salvatore
patent: 6463365 (2002-10-01), Anagnost et al.
patent: 6484973 (2002-11-01), Scott
patent: 0780296 (1997-06-01), None
G.A. Kyroudis, “Survey of Solar-Sailing Configurations For Satellite Attitude Control,” AAS 91-486 pp. 815-838.
Fowell Richard A.
Ih Che-Hang C.
Wang Hanching Grant
Gates & Cooper LLP
Keith Jack
Palabrica R
The Boeing Company
LandOfFree
Method and apparatus for solar tacking momentum maintenance... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Method and apparatus for solar tacking momentum maintenance..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for solar tacking momentum maintenance... will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3548467