Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1977-01-14
1979-11-20
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
244 316, F41G 714, F41G 900, F41G 1100, G01S 100
Patent
active
041748182
ABSTRACT:
A missile is guided onto a target by means of a laser beam, so that the missile can determine and correct its displacement from the boresight of the laser beam. This leads to greater accuracy of guidance, and avoids the need for very narrow beams which could be lost by the missile.
REFERENCES:
patent: 3398918 (1968-08-01), Girault
patent: 3416751 (1968-12-01), Larson
patent: 3690594 (1972-09-01), Menke
patent: 3782667 (1974-01-01), Miller, Jr. et al.
patent: 4006356 (1977-02-01), Johnson et al.
patent: 4030686 (1977-06-01), Buchman
Elliott Brothers (London) Limited
Engle Samuel W.
Webb Thomas H.
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