Missile interface unit

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

Patent

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Details

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.

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