Earth based spacecraft orbit and attitude control using a look-a

Aeronautics and astronautics – Spacecraft – Attitude control

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244165, 244169, 244171, 244158R, B64G 124

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059927992

ABSTRACT:
A spacecraft ground loop controller (GLC), located on the Earth, interfaces with a satellite ground station receiving spacecraft telemetry from the downlink baseband equipment and automatically sending spacecraft commands through the command uplink baseband equipment to control the attitude of an orbiting spacecraft and achieve partial orbit control using commanded thruster firings and magnetic torquer polarity and magnitude. A cooperative approach of using all available thrusters, of both the primary and redundant strings, provides greater fuel savings.

REFERENCES:
patent: 3114517 (1963-12-01), Brown
patent: 3586261 (1971-06-01), Paine
patent: 4288051 (1981-09-01), Goschel
patent: 5248118 (1993-09-01), Cohen et al.
patent: 5803407 (1998-09-01), Scott
patent: 5862495 (1999-01-01), Small et al.
Journal of Guidance, Control and Dynamics, vol. 18, No. 2, Mar./Apr. 1995, Wash. D.C., pp. 256-263, XPOOO531533, H. Krishnan et al., "Attitude Stabilization of a Rigid Spacecraft Using Two Momentum Wheel Actuators".

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