Guidance law to improve the accuracy of tactical missiles

Details Guidance law to improve the accuracy of tactical missiles Guidance law to improve the accuracy of tactical missiles

1983-04-01

1985-09-17

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

045415919

ABSTRACT:
A missile guidance system in a canard controlled airframe with means to mure the angle of attack as well as the pursuit angle by the use of a two degree of freedom roll-free reference gyroscope or other inertial reference device so as to move the canard control surfaces, where the canards direct the missile to the target.

REFERENCES:
patent: 3206143 (1965-09-01), Von Munchhofen
patent: 3905563 (1975-09-01), Nagoshi
patent: 4189116 (1980-02-01), Ehrich et al.
patent: 4231533 (1980-11-01), Durig
patent: 4264907 (1981-04-01), Durand, Jr. et al.
patent: 4288050 (1981-09-01), Gauggel

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