Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1974-10-10
1976-06-22
Wilbur, Maynard R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 313, 23515027, 343112CA, F41G 700, F42B 1502, G06F 1550
Patent
active
039646955
ABSTRACT:
An apparatus mounted in an intercept or seeker missile for computing during the flight of the intercept missile toward a target, such as another or target missile, a continuous estimate of the "time to go" to the point of closest approach of the intercept missile to the target and producing a control signal which varies in accordance with the "time to go" and which may be used for such purposes as arming a warhead of the intercept missile, controlling the navigational system of the intercept missile, and the like.
REFERENCES:
patent: 3698811 (1972-10-01), Weil
Blum T. M.
Wilbur Maynard R.
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