MULTI-PURPOSE AIRCRAFT EQUIPMENT CONTROL SYSTEM

FIELD: aeronautical engineering; equipment for control of flying vehicles. ^ SUBSTANCE: proposed system includes two conversion and calculation units and monitoring and control unit. Each of conversion and calculation units includes analog signal reception modules, discrete signal reception modules,...

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Bibliographische Detailangaben
Hauptverfasser:	DEMCHENKO O.F, NIKITIN V.N, JUKOV A.V, KOZHEVNIKOV V.I, POPOVICH K.F, MAKAROV N.N, SHKOLIN V.P, KODOLA V.G, DEREVJANKIN V.P, KRJUKOV S.P
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: aeronautical engineering; equipment for control of flying vehicles. ^ SUBSTANCE: proposed system includes two conversion and calculation units and monitoring and control unit. Each of conversion and calculation units includes analog signal reception modules, discrete signal reception modules, processor module and input/output module which are connected with sensors of general-purpose aircraft equipment control system. Control and monitoring unit consists of functionally independent modules transmitting power commands to actuating mechanisms of general-purpose aircraft equipment and light indicator control modules. System is connected with multiplex information exchange channel and code communication lines. One conversion and calculation unit is reserve. Proposed system may operate in automatic and manual control modes. ^ EFFECT: enhanced controllability at reduced nomenclature of onboard equipment; reduced power requirements; low cost. ^ 10 cl, 2 dwg