Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1974-01-25
1976-02-10
Pendegrass, Verlin R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244169, B64C 1500
Patent
active
039374238
ABSTRACT:
A system for controlling the attitude of a vehicle along three-axes is provided with a simple momentum wheel of one degree of freedom and several jets so as to enable correction of attitude error and dampen nutation action of the vehicle. The jets are controlled by means of a two channel control circuit terminating in logic gates that select the particular jet required to make the error correction. One of the channels is responsive to the polarity or sign of a voltage provided as input thereto whereas the other channel is responsive to threshold voltage levels provided to it, both channels being responsive to inputs from a low pass filter. The threshold voltage levels are adjusted by feedback correction paths provided in that particular portion of the control circuit.
REFERENCES:
patent: 3189299 (1965-06-01), Garner et al.
patent: 3365147 (1968-01-01), Wolfe
patent: 3511452 (1970-05-01), Smith et al.
patent: 3624367 (1971-11-01), Hamilton et al.
patent: 3643897 (1972-02-01), Johnson
patent: 3813067 (1974-05-01), Mork
Gerry Martin E.
Hughes Aircraft Company
MacAllister W. H.
Pendegrass Verlin R.
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