Spacecraft gyro calibration system

Aeronautics and astronautics – Spacecraft – Attitude control

Reexamination Certificate

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Reexamination Certificate

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10723782

ABSTRACT:
A method of calibrating a gyro (42) of a spacecraft (14) may include determining a yaw attitude residual of the spacecraft. Roll gyro bias residual is determined in response to the yaw attitude residual. The gyro (42) is calibrated in response to the roll gyro bias residual. A method of calibrating a gyro (42) of a spacecraft (14) may alternatively include disabling gyro calibration, gain scheduling, or resetting attitude and gyro bias covariance, for selective axes, for a yaw transient period. The gyro (42) is calibrated in a nominal fashion after completion of the yaw transient period.

REFERENCES:
patent: 3242744 (1966-03-01), Fischel
patent: 4094479 (1978-06-01), Kennedy, Jr.
patent: 4303978 (1981-12-01), Shaw et al.
patent: 4732354 (1988-03-01), Lievre
patent: 5140525 (1992-08-01), Shankar et al.
patent: 5205518 (1993-04-01), Stetson, Jr.
patent: 5400033 (1995-03-01), Hablani
patent: 5402341 (1995-03-01), Liubakka et al.
patent: 5452869 (1995-09-01), Basuthakur et al.
patent: 5527003 (1996-06-01), Diesel et al.
patent: 5574650 (1996-11-01), Diesel
patent: 5826828 (1998-10-01), Fowell et al.
patent: 6260805 (2001-07-01), Yocum et al.
patent: 6421622 (2002-07-01), Horton et al.
patent: 6647352 (2003-11-01), Horton
patent: 6804986 (2004-10-01), Patouraux
patent: 6853947 (2005-02-01), Horton
patent: 6863244 (2005-03-01), Fowell et al.
patent: 6921049 (2005-07-01), Fowell
patent: 2002/0116993 (2002-08-01), Patouraux
patent: 2004/0113020 (2004-06-01), Wang et al.
patent: 2004/0117074 (2004-06-01), Wang et al.
patent: 2005/0027407 (2005-02-01), Holt et al.
patent: 2005/0049764 (2005-03-01), Wang et al.
patent: 2005/0108884 (2005-05-01), Wang et al.
patent: 2005/0178874 (2005-08-01), Wang et al.
M. Annadurai, “Innovations in Satellite Mission Management”, pp. 1-10 (and wayback attachment), Nov. 23, 2004.

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