Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1989-12-20
1991-06-04
Barefoot, Galen
Aeronautics and astronautics
Spacecraft
Attitude control
364434, 364459, 244164, 244 32, B64G 128
Patent
active
050207458
ABSTRACT:
A reaction-wheel stabilized spacecraft reduces attitude errors at wheel reversals by application of a dither component to the wheel torque command signal.
REFERENCES:
patent: 3350033 (1967-10-01), Goldberg
patent: 3424401 (1969-01-01), Maurer
patent: 3493194 (1970-02-01), Kurzhals
patent: 3591108 (1971-07-01), Perkel et al.
patent: 3866025 (1975-02-01), Cavanagh
patent: 3968352 (1976-07-01), Andeen
patent: 3998409 (1976-12-01), Pistiner
patent: 3999729 (1976-12-01), Muhlfelder et al.
patent: 4071211 (1978-01-01), Muhlfelder et al.
patent: 4211452 (1980-07-01), Poubean
patent: 4272045 (1981-06-01), Phillips
patent: 4361073 (1982-11-01), Oelrich et al.
patent: 4470562 (1984-09-01), Hall et al.
patent: 4521855 (1985-06-01), Lehner et al.
patent: 4567564 (1986-01-01), Bittner et al.
patent: 4752884 (1988-06-01), Slafer et al.
patent: 4767084 (1988-08-01), Chan et al.
Barefoot Galen
General Electric Company
Meise William H.
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