Spacecraft earth-pointing attitude acquisition method

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244171, B64G 124, B64G 136

Patent

active

050803077

ABSTRACT:
A method for acquiring Earth-pointing attitude of a three-axis, body-stabilized spacecraft orbiting the Earth in a prescribed orbit plane, e.g. a geosynchronous communications satellite, including the steps of aligning the roll axis of the spacecraft with the sun line (which is the vector directed from the spacecraft to the Sun); then, orienting the spacecraft such that the angle formed between the yaw axis and the sun line is equal to the Earth-Sun angle (which is the angle formed between the sun line and a vector directed from the origin of the spacecraft internal coordinate system to the Earth); then, orienting the spacecraft such that the yaw axis is aligned with the center of the Earth; and finally, rotating the spacecraft about its yaw axis until its pitch axis is oriented at a desired attitude relative to the orbit plane, e.g., normal to the orbit plane, to thereby complete acquisition of the Earth-pointing attitude.

REFERENCES:
patent: 4306692 (1981-12-01), Kaplan et al.
patent: 4358076 (1982-11-01), Large et al.
patent: 4752884 (1988-06-01), Slafer et al.
patent: 4909460 (1990-03-01), Mouve et al.
patent: 4927101 (1990-05-01), Blancke

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