Flight control system for a remote-controlled missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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F41G 728

Patent

active

043836615

ABSTRACT:
A ground station forming part of a system for controlling the flight of a missile comprises two cascaded computers, the first of these computers generating guidance instructions on the basis of initially available data while the second computer converts these instructions into control signals transmitted to the missile. A receiver aboard the missile translates these control signals into operating commands for missile-borne actuators affecting its course, e.g. motors controlling yaw and pitch through the positioning of aerodynamic surfaces; the responses of the actuators to the operating commands are monitored by negative-feedback loops including error-correcting networks.

REFERENCES:
patent: 2352308 (1944-06-01), Bailey
patent: 2603434 (1952-07-01), Merrill
patent: 3156435 (1964-11-01), Norton et al.
patent: 3168264 (1965-02-01), Sendles
patent: 3360214 (1967-12-01), Stcherbatcheff
patent: 3450373 (1969-06-01), Richards
patent: 3998406 (1976-12-01), Smith et al.
patent: 4097007 (1978-06-01), Fagan et al.

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