Launcher control system for surface launched active radar missil

Details Launcher control system for surface launched active radar missil Launcher control system for surface launched active radar missil

1989-12-07

1992-01-14

Steinberger, Brian S.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244 314, F41G 700

Patent

active

050803000

ABSTRACT:
In a weapon system 10 incorporating a target position sensor (14), an information system (16), a power source (24), a launcher (20), and an airborne vehicle (18), a launcher control system (12) incorporates a communications interface (26) for coupling the information system (16) and the target position sensor (14) to a launcher (20) and an airborne vehicle (18). The communications interface (26) receives target position information and launch and control orders and provides launcher and airborne vehicle status. A airborne vehicle interface (28) couples the launcher (20) and the airborne vehicle (18) to the information system (16) and a power source (22). A transmitter (30) communicates updated target position information to the airborne vehicle after launch. A power control means (32) converts and regulates power from different power sources (22) to be used by the launcher control system (12). The launcher (20) with launcher control system (12) is preferably modular in construction and is separate from the information system (16) and target position sensor (14).

REFERENCES:
patent: 3962537 (1976-06-01), Kerns et al.
patent: 4093153 (1978-06-01), Bardash et al.
patent: 4705237 (1987-11-01), Goldfield et al.

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