Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1975-01-06
1976-07-20
Feinberg, Samuel
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
250203R, F41G 700
Patent
active
039702693
ABSTRACT:
A system for guiding a missile to a target is disclosed which includes a signal processor for generating error signals in response to a signal being received from the target. The processor includes four channels for receiving a target signal. An arithmatic circuit compares the amplitude of the target signal on each channel with the average amplitude of the other three channels and generates an error signal for guiding the missile.
REFERENCES:
patent: 3494576 (1970-02-01), Lamelot
patent: 3657547 (1972-04-01), Mansfield
Cardenas Rafael A.
Feinberg Samuel
Hughes Aircraft Company
MacAllister William H.
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