Simplified high accuracy guidance system

Details Simplified high accuracy guidance system Simplified high accuracy guidance system

1976-07-20

1979-03-27

Engle, Samuel W.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244 316, 244 319, F41G 316, F41G 322, F41G 710, F41G 900

Patent

active

041461967

ABSTRACT:
A simplified guidance system for air-to-air missiles where the pilot adjusts his helmet sight to compensate for missile errors and this information is fed to a computer which computes correction data from error information, aircraft position information and missile position information, correction data is then sent via a radio link to the missile control system which changes the flight path accordingly.

REFERENCES:
patent: 1387678 (1921-08-01), Anderson
patent: 3211045 (1965-10-01), Gerhardt
patent: 3617015 (1971-11-01), Kinder
patent: 3753538 (1973-08-01), Marsh et al.
patent: 4020324 (1977-04-01), Buscher et al.
patent: 4037202 (1977-07-01), Terzian
patent: 4040744 (1977-08-01), Schertz et al.

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