Method of attitude reacquisition for three-axis stabilized satel

Details Method of attitude reacquisition for three-axis stabilized satel Method of attitude reacquisition for three-axis stabilized satel

1991-12-12

1994-01-11

Huppert, Michael S.

Aeronautics and astronautics

Spacecraft

Attitude control

244171, B64G 136

Patent

active

052773850

ABSTRACT:
To reacquire the attitude of a satellite wholly or partially stabilized on three axes a test is executed to determine if a terrestrial sensor is sensing the Earth (test 1) and if a star sensor is sensing a star whose magnitude is at least approximately equal to that of a given reference star (test 2).

REFERENCES:
patent: 5080307 (1992-01-01), Smay et al.

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