Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1997-02-18
1999-11-30
Eldred, J. Woodrow
Aeronautics and astronautics
Spacecraft
Attitude control
244165, 244169, 244171, 244158R, B64G 124
Patent
active
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".
Gamble Donald W.
McLaren Mark D.
Takahashi Marc
Eldred J. Woodrow
Space Systems Loral, Inc.
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