Missile control system

Details Missile control system Missile control system

1966-01-28

1976-04-20

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

F41G 714

Patent

active

039513599

ABSTRACT:
Initial turn circuits for providing steering orders for a missile including first computer for providing a critical turn angle signal, a second computer for providing a difference turn angle signal and circuitry for combining these signals for providing a signal related to a turn angle which would prevent the missile from passing directly over the tracking radar antenna during an "over-the shoulder" firing.

REFERENCES:
patent: 3338534 (1967-08-01), Girsberger
patent: 3363858 (1968-01-01), Dobbins et al.
patent: 3374967 (1968-03-01), Plumley
patent: 3405888 (1968-10-01), Okamoto

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