Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1990-08-16
1992-03-17
Sotomayor, John B.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
244 315, F41G 722, F41G 734, F42B 1501
Patent
active
050961390
ABSTRACT:
In a launcher control system (12), a missile interface unit (29) for controlling a ground launched active radar guided missile (GLA) which is modular in construction. The missile interface unit (29) provides target position information and control signals for test and launch of the GLA, and power for activating the GLA, as well as determining the status of the GLA. It employs a plurality of cards (56-70), each card having a specific function and being interconnected by a backplane bus system (55) which also couples the cards (56-70) to other components of the launcher control system (12).
REFERENCES:
patent: 4470562 (1984-09-01), Hall et al.
patent: 4530476 (1985-07-01), Thurber et al.
patent: 4553718 (1985-11-01), Pinson
patent: 4705237 (1987-11-01), Goldfeld et al.
patent: 4899956 (1990-02-01), King et al.
Feld Charles M.
Griggs Darrin C.
Humm Larry A.
Brown C. D.
Denson-Low W.
Heald R. M.
Hughes Aircraft Company
Sotomayor John B.
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