Passive missile tracking and guidance system

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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244 311, F41G 730

Patent

active

055605672

ABSTRACT:
A method and apparatus for passive tracking and guidance in missile systems is disclosed. The system is utilized in conjunction with a target acquisition system such as a scanning infrared detection system. The target and missile are sensed and the measured displacement therebetween is utilized in conjunction with calculated nominal trajectory data to generate guidance control signals. In a preferred embodiment of the present invention, the guidance control signals are transmitted to a receiver on the missile utilizing a radar frequency transmitter.

REFERENCES:
patent: 3567163 (1971-03-01), Kepp et al.
patent: 4220296 (1980-09-01), Hesse
patent: 4274609 (1981-06-01), Ferrier et al.
patent: 4397429 (1983-08-01), Fouilloy
patent: 4406429 (1983-09-01), Allen

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