SSICM guidance and control concept

Details SSICM guidance and control concept SSICM guidance and control concept

1983-08-08

1985-09-24

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

045428700

ABSTRACT:
The guidance scheme utilizes wide beam width semi-active RF sensors, a prsion roll altitude reference, and a controlled grade pitch, yaw and roll rate gyros to deliver high quality homing guidance information to a spin stabilized controlled missile. A filtering system is utilized to eliminate errors caused by body roll signals generated due to the spin of the missiles. The nutational motion is used to calibrate the sensors. Impulsive maneuvers are utilized to intercept incoming ballistic targets.

REFERENCES:
patent: 3414215 (1968-12-01), Martin et al.
patent: 3740002 (1973-06-01), Schaefer
patent: 3897918 (1975-08-01), Gulick, Jr. et al.
patent: 4204655 (1980-05-01), Gulick et al.

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