Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1989-08-18
1990-11-27
Steinberger, Brian S.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 700
Patent
active
049730134
ABSTRACT:
A seeker having a gyroscopic spin stabilized optical arrangement adapted to gimbal relative to a body in response to a current fed to a precession coil by a processor. Gimballing action of such optical arrangement within the body is measured by a voltage induced in a cage coil. The precession coil and cage coil are mounted adjacent to each other. The seeker includes a cage coil compensator comprising a differencing network and a differentiator. Changes in the current fed to the precession coil induces unwanted voltage in the adjacent cage coil. The differentiator is fed by the current in the precession coil to produce a voltage related to the rate of change in the current in the precession coil and hence, related to the undesired voltage induced in the cage coil. The differencing network is fed by the voltage produced by the differentiator and the total voltage induced in the cage coil to subtract from such total voltage the undesired portion thereof induced therein by the adjacent precession coil. With such arrangement, cancellation of the undesired voltage induced in the cage coil is provided by an electronic circuit thereby eliminating the requirement of an additional caging cancellation coil.
REFERENCES:
patent: 3504869 (1970-04-01), Evans et al.
patent: 3872308 (1975-03-01), Hopson et al.
patent: 4542870 (1985-09-01), Howell
Mofford Donald F.
Raytheon Company
Sharkansky Richard M.
Steinberger Brian S.
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