Ideal trajectory shaping for anti-armor missiles via time optima

Details Ideal trajectory shaping for anti-armor missiles via time optima Ideal trajectory shaping for anti-armor missiles via time optima

1978-05-30

1980-04-15

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F42B 1502

Patent

active

041980158

ABSTRACT:
A missile system in which a missile is guided in a predetermined trajectory rom launch or shortly thereafter in yaw by proportional navigation and in pitch first by a pitch programmer until said missile reaches a predetermined angle between a line of sight of a seeker of the missile and a centerline of the missile, then in pitch by a time optimal controller to direct the missile at a predetermined angle toward a target and finally by proportional navigation in pitch of the missile to the target.

REFERENCES:
patent: 2821349 (1958-01-01), Sohn
patent: 2951658 (1960-09-01), Jones, Jr. et al.
patent: 3088034 (1963-04-01), Jones, Jr. et al.
patent: 3097816 (1963-07-01), Berry
patent: 3695555 (1972-10-01), Chadwick
patent: 4123019 (1978-10-01), Amberntson

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