Satellite beam steering reference using terrestrial beam steering terminals
AssigneeGlobalstar L.P.
InventorRobert A. Wiedeman
Life of this patent
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AssigneeGlobalstar L.P.
InventorRobert A. Wiedeman
Estimating the term…
A satellite communication system has at least one satellite (1) with an antenna that generates a moving beam pattern on the surface of the earth. The beam pattern (3) is comprised of a plurality of sub-beams (4). A method of this invention determines an attitude correction signal for the satellite by the steps of: (a) providing at least one reference transmitter (10) at a known location on the surface of the earth; (b) transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams; (c) receiving the at least one signal with the satellite antenna and transponding the received at least one signal to a ground station (8). A next step of the method (d) receives the transponded at least one signal with the ground station; (e) determines a gain of the received at least one signal; (f) compares the determined gain to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and (g) and determines a difference between the determined gain and the expected gain to derive a correction signal indicative of an attitude error of the satellite. The method further includes the steps of transmitting the correction signal to the satellite; and correcting the attitude of the satellite in accordance with the correction signal.
In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining an attitude correction signal for the satellite comprising the steps of:
In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a satellite attitude correction system comprising:
In a satellite communication system comprising at least one satellite having a steerable antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining an antenna pointing correction signal for the satellite comprising the steps of:
In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:
In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:
In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:
Dependencies are inferred from the claim text.