CONTROL SYSTEM OF FLIGHT VEHICLE ARMAMENT

FIELD: aviation, in particular, control systems of the flight vehicle armament having the functions of group cooperation. SUBSTANCE: the system has a panel of tuming and selection of the guidance channel, airborne digital computer system, airborne radar, guidance equipment, complex of radio telemetr...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MIKHALEV V.I, DROBYSHEVSKIJ V.G, FEDOTCHENKO A.I, PANKOV V.KH, SHUSER V.S, KOSTRUBSKIJ EH.K
Format: Patent
Sprache:eng ; rus
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Beschreibung
Zusammenfassung:FIELD: aviation, in particular, control systems of the flight vehicle armament having the functions of group cooperation. SUBSTANCE: the system has a panel of tuming and selection of the guidance channel, airborne digital computer system, airborne radar, guidance equipment, complex of radio telemetry communication and target distribution and a guidance mode selection panel connected by their inputs-outputs to the respective inputs of the above equipment, one of the outputs of the guidance mode selection panel is connected to the respective inputs of the complex of radio telemetry communication and target distribution. The control system of the flight vehicle armament provides for control of group actions of flight vehicles, having armament control systems differing from it, i.e. complexes of radio telemetry communication and target distribution differing from it, or having no radio telemetry communication and target distribution complexes at all. The novelty in the system is the fact that it is provided with a "Cooperation" channel made in the form of an encoder of the "Cooperation" channel and a complex of transceiving communication equipment of the "Cooperation" channel, and a "Cooperation" selector switch; the inputs of the complex of transceiving communication equipment of the "Cooperation" channel are connected to the outputs of the panel of tuning and selection of the guidance channel respectively and of the "Cooperation" channel encoder, whose input is connected to the respective output of the airborne digital computer system, and the "Cooperation" selector switch is connected to the respective input of the guidance mode selection panel. EFFECT: provided control of group actions of flight vehicles. 1 dwg