Information and control systems for multipurpose aircraft

Abstract

The present invention relates to the field of aeronautical instrumentation, and in particular to composite facilities for controlling and indicating the status of aircraft (AC). The proposed Information and Control System (ICS) consists of the following elements: 1 – Television Signal Conversion Unit (TSCU), 2 – External Storage Device (ESD), 3 – Information and Control Field (ICF), 4 – Signal Concentrator Unit ( SCU), 5 – Onboard Digital Computing System (ODCS), 6 – Information Interchange Channel (IIC), 7 – Input / Output and Interchange Control Unit (IOICU), 8 – Indication Data Generation Unit (IDGU), 9 – Aircraft Equipment Control Unit (AECU), 10 – Navigation Computing Unit (NCU), 11 – Electronic Countermeasures Control Unit (ECCU), 12 – Flight Plan Database (IADB), 13 – Low Altitude Flight Unit (LHFU), 14 – Formation Air Navigation Unit ( GANU), 15 - Aircraft Control Unit (ACCU), 16 - Unit for controlling the recording of the flight recorder (UCRFR), 17 - Combat Use Unit (CUU), 18 - Mode Control Unit (MCU), 19 - Digital Position Map Unit (DLUM), 20 – Electromagnetic Compatibility Unit (EMCU), 21 – Television Signal Conversion Control Unit (TSCCU), 22 – Technical Service Unit (TSU), 23 – Status Monitoring and Indicator Unit (SMIU), 24 – Interface Equipment (IE), 25 - Switching Unit (SU), 26 - Network Based Information Exchange Channel (NIIC).

Description

Technical field [0001] The present invention relates to aviation instrument manufacturing, and more specifically, to a system for controlling and indicating the status of an aircraft (AC, aircraft). Background technique [0002] There are multifunctional vehicle-based and land-based aircraft based targeting and navigation systems (RU 2,276,328), including a set of multi-purpose indicators, head-up displays, external viewing TV cameras, work controls, target targeting devices, and flight navigation The device, the portable initial data carrier, the countermeasure control system, and the computing system are all interconnected via input / output and information exchange channels; the computing system includes: an integrated database computing logic module; used to generate flight navigation parameters and generate Flight and aiming parameters, generation of displayed information, calculation logic modules for input / output and information exchange management, they are all interconnect...

AI Technical Summary

Problems solved by technology

[0011] - The problem of provision of electromagnetic compatibility of aircraft equipment important for modern multifunctional aircraft is not resolved

Images