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Information and control system for a multifunctional aircraft

An information management system and aircraft technology, applied in the field of control and indication systems, can solve problems such as electromagnetic compatibility not being solved, and achieve the effects of improving work efficiency, enhancing functionality, and improving failsafety

Active Publication Date: 2014-10-15
OTKRYTOE AKTSIONERNOE OBSHCHESTVO OKB SUKHOGO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • Information and control system for a multifunctional aircraft

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Embodiment Construction

[0025] The information management system (IMS, information management system) according to the present invention includes the following components:

[0026] 1. TV signal conversion unit (TSCU, television signal conversion unit)

[0027] 2. External storage device (ESD, external storage device)

[0028] 3. Information management field (IMF, information management field)

[0029] 4. Signal concentrator unit (SCU, signal concentrator unit)

[0030] 5. Onboard digital computing system (ODCS, onboard digital computing system)

[0031] 6. Information exchange channel (IIC, information exchange channel)

[0032] 7. Input / output and exchange control unit (IOICU, input / output and exchange control unit)

[0033] 8. Indicative data generation unit (IDGU, indicative data generation unit)

[0034] 9. General aircraft equipment control unit (GAECU, general aircraft equipment control unit)

[0035] 10. Navigation computing unit (NCU, navigation computing unit)

[0036] 11. Electronic ...

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PUM

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Abstract

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).

Description

technical field [0001] The present invention relates to aeronautical instrumentation, and more particularly to a system for the control and indication of the status of an aircraft (AC, aircraft). Background technique [0002] There are known targeting and navigation systems (RU2,276,328) for multifunctional vehicle-based and land-based aircraft, including a set of multi-purpose indicators, a heads-up display, external viewing TV cameras, working controls, targeting devices, flight Navigation device, portable initial data carrier, countermeasure control system, computing system, all interconnected by input / output, via information exchange channels; said computing system comprising: a computing logic module of an integrated database; for generating flight navigation parameters, Computational logic modules for generating flight and aiming parameters, generating displayed information, for input / output and management of information exchange, all interconnected via input / output, v...

Claims

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Application Information

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IPC IPC(8): G05B19/00G05D1/00
CPCG05B19/00G05B15/02
Inventor 米哈伊尔·阿斯拉诺维奇·波戈相亚历山大·尼古拉耶维奇·达维坚科米哈伊尔·尤里耶维奇·斯特雷勒茨维克托·鲍里索维奇·波利亚科娃德米特里·伊戈列维奇·格里博夫亚历山大·谢尔盖耶维奇·巴兰诺娃谢尔盖·维克托罗维奇·博布罗夫
Owner OTKRYTOE AKTSIONERNOE OBSHCHESTVO OKB SUKHOGO
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