Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1989-10-16
1990-09-25
Barefoot, Galen
Aeronautics and astronautics
Spacecraft
Attitude control
B64G 126
Patent
active
049587889
ABSTRACT:
A system for controlling the orbit of a satellite by operating a plurality of thrusters is disclosed. In the system, an actual attitude of the satellite is sensed, an evaluation is set up on the basis of the sensed attitude and compared with a threshold which is adequately changing, and the ON-OFF condition of the firing of the thrusters is based on the relationship between the evaluation value and the threshold.
REFERENCES:
patent: 3643897 (1972-02-01), Johnson, Jr.
patent: 4386750 (1983-06-01), Hoffman
patent: 4537375 (1985-08-01), Chan
Namera Takakazu
Ogura Naoto
Barefoot Galen
NEC Corporation
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