Guidance system for a projectile

Details Guidance system for a projectile Guidance system for a projectile

1973-08-10

1986-02-04

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

045680396

ABSTRACT:
Guidance is provided for a spinning projectile by measuring the magnitude of the angle between the spinning projectile and a target. This information is processed in conjunction with a body rate sensor to deduce the angular rate of the line of sight between projectile and the target. A means is provided for reducing the line of sight angular rate to zero, thus ensuring that the projectile will intercept the target.

REFERENCES:
patent: 3021096 (1962-02-01), DeMott
patent: 3065931 (1962-11-01), Dixon et al.
patent: 3504869 (1970-04-01), Evans et al.

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