INFORMATION AND CONTROL SYSTEM FOR A MULTIFUNCTIONAL AIRCRAFT

The invention relates to the field of aerospace instrument making, specifically to complexes for controlling and indicating the state of an aircraft (AC). The proposed information and control system (ICS) comprises the following elements: 1 - a television signal conversion unit (TSCU), 2 - an extern...

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Bibliographische Detailangaben
Hauptverfasser:	STRELETS, MIHAIL YURIEVICH, BARANOV, ALEKSANDR SERGEEVICH, POGOSYAN, MIHAIL ASLANOVICH, GRIBOV, DMITRIY IGOREVICH, DAVIDENKO, ALEKSANDR NIKOLAEVICH, POLYAKOV, VIKTOR BORISOVICH, BOBROV, SERGEY VIKTOROVICH
Format:	Patent
Sprache:	eng ; fre ; rus
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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Beschreibung
Zusammenfassung:	The invention relates to the field of aerospace instrument making, specifically to complexes for controlling and indicating the state of an aircraft (AC). The proposed information and control system (ICS) comprises the following elements: 1 - a television signal conversion unit (TSCU), 2 - an external storage device (ESD), 3 - an information and control field (ICF), 4 - a signal concentrator unit (SCU), 5 - an on-board digital computation system (ODCS), 6 - an information interchange channel (IIC), 7 - an input/output and interchange control unit (IOICU), 8 - an indicative data generation unit (IDGU), 9 - an airplane-wide equipment control unit (AECU), 10 - a navigational calculations unit (NCU), 11 - an electronic countermeasure control unit (ECCU), 12 - a flight plan database (IADB), 13 - a low-altitude flight unit (LHFU), 14 - a groupwise aerial navigation unit (GANU), 15 - an aircraft control unit (ACCU), 16 - a unit for controlling the recording of the flight recorder (UCRFR), 17 - a combat use unit (CUU), 18 - a mode control unit (MCU), 19 - a digital location map unit (DLMU), 20 - an electromagnetic compatibility unit (EMCU), 21 - a television signal conversion control unit (TSCCU), 22 - a technical services unit (TSU), 23 - a state monitoring and indicator unit (SMIU), 24 - interfacing equipment (IE), 25 - a switching unit (SU), 26 - a network-based information interchange channel (NIIC). L'invention concerne la fabrication d'instruments pour l'industrie aérospatiale et notamment des ensembles d'indication de l'état d'un aéronef. Le système d'informations et de commande (SIC) comprend les éléments suivants: (1) unité de conversion de signaux télévisés (UCST), (2) dispositif mémoire externe (DME), (3) champ de contrôle et d'informations (CCI), (4) unité de concentration de signaux (UCS), (5) système de calcul numérique embarqué (SCNE), (6) canal d'échange d'informations (CEI), (7) unité entrée/sortie et unité de commande d'échange (UESUCE), (8) unité de génération de données d'indication (UGDI), (9) unité de commande de l'équipement général de l'avion (UCEGA), (10) unité de calcul de navigation (UCN), (11) unité de contre-mesures électroniques (UCME), (12) base de données de plan de vol (BDPV), (13) unité de vol à basse altitude (UVBA), (14) unité de pilotage en groupe (UPG), (15) unité de commande d'aéronef (UCA), (16) unité de commande de l'enregistrement sur des moyens de contrôle objectif (UCEMCO), (17) unité de combat (UC), (18) unité de comman