Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1989-07-21
1992-01-21
Steinberger, Brian S.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
244 311, F41G 700
Patent
active
050821997
ABSTRACT:
A digital electronics unit (81), missile, and missile system for a tube-launched missile. The invention utilizes a positional status mechanism (10) to structure signals from the on-board gyro system (80) and a directional mechanism (11) to separate signals from an operator. These signals are handled by a digital micro-controller (12) to create the proper control signals for manipulation of the missile in the missile system.
REFERENCES:
patent: 4037202 (1977-07-01), Terkian
patent: 4662580 (1987-05-01), Nelron
patent: 4732349 (1988-03-01), Maurer
patent: 4899956 (1990-02-01), King et al.
Brown C. D.
Denson-Low W. K.
Heald R. M.
Hughes Aircraft Company
Steinberger Brian S.
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