Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1995-09-05
1997-05-06
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
244173, B64G 124
Patent
active
056263155
ABSTRACT:
A satellite embodying at least one surface intended mainly for exposure to solar radiation and extending away from the satellite in a predetermined direction (Y), an onboard computer having connected thereto an attitude sensing system, an orbit control system for imparting thrust to the satellite along predetermined axes, and an attitude control system. The satellite further embodies a device for controlling the tilt of the surface in parallel with a plurality of planes containing the predetermined direction; and, therefore, particularly in parallel with the plane of a solar panel forming the surface. The tilt control device is controlled by the onboard computer. The tilting can generate a moment of pitch or relocate the center of gravity onto the axis of the orbit control system.
REFERENCES:
patent: 4262867 (1981-04-01), Piening
patent: 4591116 (1986-05-01), Guenther et al.
patent: 4747567 (1988-05-01), Johnson et al.
patent: 4759517 (1988-07-01), Clark
patent: 5310144 (1994-05-01), Salvatore et al.
Brunet Pierre
Flament Patrick
Perdu Michel
Portier Jean
Aerospatiale - Societe Nationale Industrielle
Barefoot Galen L.
LandOfFree
Apparatus controlling the pitch attitude of a satellite by means does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Apparatus controlling the pitch attitude of a satellite by means, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Apparatus controlling the pitch attitude of a satellite by means will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2126897