Launcher for an optically guided, wire-controlled missile with i

Details Launcher for an optically guided, wire-controlled missile with i Launcher for an optically guided, wire-controlled missile with i

1986-10-16

1987-11-10

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244 311, F41G 732

Patent

active

047052376

ABSTRACT:
Launcher for a tube-launched, optically guided wire controlled missile. In he electronic circuitry that forms part of a feedback servomechanism there are provided pitch and yaw channels with time variable gains having different transfer functions. Optionally there are further provided at least two different generators of signals for gravity bias with automatic means for selecting between them in accordance with the physical characteristics of the missile.

REFERENCES:
patent: 3233847 (1966-02-01), Girsberger
patent: 3366346 (1968-01-01), McKnight et al.
patent: 3711046 (1973-01-01), Barhydt et al.
patent: 4406429 (1983-09-01), Allen
patent: 4474343 (1984-10-01), Zwirn et al.

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