Aeronautics and astronautics – Spacecraft – Attitude control
Reexamination Certificate
2005-07-26
2005-07-26
Barefoot, Galen (Department: 3644)
Aeronautics and astronautics
Spacecraft
Attitude control
C244S168000, C244S173300
Reexamination Certificate
active
06921048
ABSTRACT:
A method and system for minimizing the solar array sun tracking disturbance is disclosed. The method separates the North solar array wing stepping and South solar array wing stepping in time, and use the disturbance caused by one solar array wing to cancel the disturbance caused by the other solar array wing. It separates the step times of these two solar arrays by a half cycle of the array frequency excited by the solar wing drive stepping. Because of the symmetry between the North and South solar arrays, their disturbances cancel each other out.
REFERENCES:
patent: 4843294 (1989-06-01), Bhat et al.
patent: 5520359 (1996-05-01), Merhav et al.
patent: 5610848 (1997-03-01), Fowell
patent: 6003817 (1999-12-01), Basuthakur et al.
patent: 6311929 (2001-11-01), Kazimi et al.
patent: 6311931 (2001-11-01), Smay
Barefoot Galen
Gates & Cooper LLP
The Boeing Company
LandOfFree
Method and apparatus for minimizing solar array sun tracking... 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 minimizing solar array sun tracking..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for minimizing solar array sun tracking... will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3421856