Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1982-10-27
1993-08-03
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 728
Patent
active
052321827
ABSTRACT:
A method of guiding an air-to-air missile launched from a penetrating aircraft at a target aircraft having a search radar therein is shown. The missile changes from a passive antiradiation homing mode to an active seeker mode when the missile is detected and the search radar is shutdown. The active seeker uses a synthetic aperture radar that is squinted at the target aircraft. At the handover point when the search radar is shutdown, the missile executes a turn away from the target aircraft to bring the target aircraft within the synthetic aperture radar coverage. The amount of turn is within preselected limits based on several parameters.
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patent: 4264907 (1981-04-01), Durand, Jr. et al.
patent: 4274609 (1981-06-01), Ferrier et al.
Collier Stanton E.
Jordan Charles T.
Singer Donald J.
The United States of America as represented by the Secretary of
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