Optical boresight method for nutating system

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

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244 313, F41G 332, F41G 1100, F41G 100, F41G 154

Patent

active

041790855

ABSTRACT:
A method for eliminating boresight error in a beamrider missile guidance tem wherein moving parts may disrupt alignment of a nutated beam. Periodic strobing of a light emitting source directs beams of light to form an optical reticle which may function as either the boresight alignment check source or as the telescope aiming reticle.

REFERENCES:
patent: 2930894 (1960-03-01), Bozeman
patent: 3974383 (1976-08-01), Chapman
patent: 4038547 (1977-07-01), Hoesterey

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