Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1998-03-11
1999-12-21
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
B64G 128
Patent
active
060038187
ABSTRACT:
A system and method for slewing a spacecraft with a reaction wheel system including determining initial total momentum, determining maximum forward and reverse rates that can be realized within the reaction wheel system maximum storage capacity, determining a slew rate and slew direction from the maximum forward and reverse rates so as to minimize slew time for known slew angles or maximize slew rate for arbitrary slew angles, and slewing the spacecraft.
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patent: 5255879 (1993-10-01), Yocum et al.
patent: 5257802 (1993-11-01), Hablani
Bender Douglas J.
Shah Piyush R.
Uetrecht David S.
Barefoot Galen L.
Grunebach Georgann
Gudmestad Terje
Hughes Electronics Corporation
Sales Michael W.
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