Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1981-01-09
1983-04-05
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 720
Patent
active
043789188
ABSTRACT:
An open loop reduction in gunner aiming error is provided by a rate gyro dback to the missile command electronics. The low frequency movements are filtered out of the feedback circuit; permitting tracking of low frequency crossing targets, while eliminating higher frequency gunner jitter inputs.
REFERENCES:
patent: 2944763 (1960-07-01), Grandgent et al.
patent: 3233847 (1966-02-01), Girsberger
patent: 3366346 (1968-01-01), McKnight et al.
patent: 3807658 (1974-04-01), Miller, Jr. et al.
McKelvy James W.
Miller, Jr. Walter E.
Edelberg Nathan
Gibson Robert P.
Jordan Charles T.
Sims Robert C.
The United States of America as represented by the Secretary of
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