Condition and prospects of development of integrated modular … · 2012. 11. 19. · Integrated IMA/SDR – system of navigation and landing Crates #1 Crates #2 Crates #3 Crates

Международная конференция по модульной авионике

Moscow, 29-30 October 2012 г.

International conference

Condition and prospects of development of

integrated modular avionics

Международная конференция по модульной авионикеМеждународная конференция по модульной авионике

Directions of development of aviation equipment

Flight control systemAircraft equipmentbased on the IMA

Complexof multifunctional

mono sensors

New functional SWInformation-controlled

field of the cockpit

Information-computing environment on the basis of the IMA of the second

Network fault-tolerant architecture of avionics

on the unified components


open fault-tolerant an adaptable networkarchitecture;

perspective interfaces (Ethernet,

ibre Channel, RapidIO, Wi-Fi, SpaceWire);

unification and integration of modules andcomponents;

an effective means of self-control and diagnostics;

used the “System on the Chip – SoC”

Directions of the development of architecture of

Targets and means of its achievement

Increase in productivity

Increase of reliability and fault tolerance

Cost reductionof avionics

Decrease ofмассогабаритных

characteristics

Creationof dynamic structures

Decrease of the nomenclature of the element base

Decreaseof terms of

development

Unattendedavionics


Unattended onboard avionics suite

Self-recovery between the service period

Controlled redundancy

Reconfiguration: software; hardware; functional

Active safety system: Improved algorithms of the built-in

control; automatic diagnostics based

on model-oriented approach

Aircraft equipmentAvionics


ARINC 664 AFDX Switched Network

IMA core

Cockpit

IMA Core

RTOS (A653)

Hub

AFDX SwitchAFDX Switch

AFDX Switch

Hub

Video interface(А818)

IMA system 1

Network fault-tolerant architecture of

INS

RA

Air Data

Sensors

Computing wireless communication crates

RTOS (A653)

Communication functions

HUB

IMA system 2

Aircraft system

CAN

Aircraft system

Remote hub

Aircraft system

Remote hubRemote hub

Aircraft system

Remote hub

RF modules

A429, Discretes,

Analog

A429, A708, Discretes, Analog

IMA system n

FFE

AFCSOMS

FMS

Aircraft systemfunctions

Avionicsfunctions

Aircraft systems on the IMA platform

IMA platform of the second generation and applications of

software

New functions and functionality of the

cabin

Multifunctional, fully integrated software-configurable radio –

CNS radio


Unification of module avionics

Standard interchangablemodules: 1. Processor2 . AFDX switch3. Power Supply4. Optical converter

3U Crates 6U Crates

Mezzanine3U Module

6U Module

Standard interchangable mezzanine:1. Graphic controller

2. Mass storage

3. Interfaces(ARINC 429, ARINC 825 Mil1553B)

4. Analog and discrete signals I/O

Unified components:

On the basis of standards VITA 42, 46,

48, 60, 65

PerspectiveStandards

microVPX VITA 75

• System crates• Concentrator crates• Concentrator crates for critical

operating conditions


New technologic decisions of the IMA

Process modulesOn the basis of multicoremicroprocessor with high

productivity and low power consumption

Graphic modules, ensuringformation of 3D- graphic pictures

with the size not less than1920x1200x60 hz

Network commutatesWith high reliability and low

power consumption

Power packWith the compensation of

the interruptions of power supply

Using of lightweight composite materials for

interchangeable modules andcrates

Research of the effective ways of cooling the modules in

crates and blocks ARINC 600

Effective ways of cooling the modules with the high power consumption on the basis of

standard ANSI\VITA 48.5

New structural decisions of modules, crates and blocks of the IMA

New circuit decisions of functional modules


RTOS ARINC 653

Hub

AFDX SwitchAFDX Switch

Hub

Remote Hub for critical operating conditions

Function

Aircraft system(t0,05 c)

Air conditionersystem

Remote Hub for critical operating conditions

Translation

Aircraft system(t>0,1 c)

Digital sensors

Actuatingsystems

Digital sensors

Actuatingsystems

Examples for the realization of the crisp and slow response system

FFEAFCSOMS

FMSAircraft systemfunctions

Avionicsfunctions

IMA CoreTargets:

Equipment unification and minimization;

Optimization of the complex topology andcritical reduction of the feeder weight;

Unification of the equipment and ITtechnologies, providing certification and cost reduction;

Optimization of the system administration;

Functional aircraft safety increase

Remote Hub withstandard modules

Breakingsystem


Fully electrified aircraft

The main elements of FEA

System of distributionof electric power

with program management

Air condition systemwith electriccompressor

Electo-mechanical drive

management bodies

Electrohydro-Mechanical

drive TLU

Systemmanagement

drive

New power element base

The function of managementof the electric power complex

on the IMA platform(electricity supply system function)


The creation of the unifiedradio system IMA/SDR/CNS

Integrated IMA/SDR –system of navigation

and landing

Crates #1 Crates #2 Crates #3 Crates #4

Integrated IMA/SDR communication

Integrated IMA/SDR –system of surveillance

To IMA Core: AFDX network

Rad

io f

req

uen

cym

od

ule

s

To IMA Core: AFDX network

Pro

cess

cra

tes

Crates #1 Crates #2

To IMA Core: AFDX networkDigital Voice & Data

Crates #1 Crates #2

Крейт #2

AFDX / VITA 49 (signal samples)

DSP #1

DSP #2

Data Proc #1

Data Proc #2

AFDX/IP

Power

DSP #1

DSP #2

Data Proc #1

Data Proc #2

AFDX/IP

Power

DSP #1

DSP #2

Data Proc #1

Data Proc #2

AFDX/IP

Power

Крейт #1 Крейт #3

#1To IMA core and others airborne systems: AFDX networks

#2 #3

#N

United radio system IMAwith CNS/ATM functions


Perspective information-controlled field of cabin

The transition from the instrumenttype of flight data to visual presentationof information on the widescreen ;

Introduction of more effective ways of control, which use the graphic interface,and the device of control of course(touch panel, joystick, trackball);

Introduction of new functionsof information support of crew

Source: project ALISIA


Aviation systems of improved visionThe improved visionThe view trough the glazing of the cabin

The main technologies:

The improved vision: visual improving of the pictures;

interconnecting of pictures of different ranges

Integrated vision: automatic connection and visual combination of improved

picture and vector graphic images of flight2D-sensor

New functionality of


Systems of synthesize and integrated vision

The main technologies: Photogrammetric treatment of 2D and 3D date

for creation of digital models of area Picture synthesis on the basis of integration of navigation

information and information from data bases of terrain andobstacles;

Reciprocal linking and integration of sensory and geospatial information;

The man-machine communication with the use of interfaces,based on the technologies of virtual and augmented reality

Synthesize vision


Integrated vision

Improved image

Synthesize image

Layer of the obstacles

Layer of the relief

Navigation information



Observation functionThe procedure of rerouting

Horizontal plane

Detection conflicts board system

Superior visual overview

Conflict detection

Vertical plane


Directions of the developmentof flight control systems

Increase of security of flightThe unloading of the crew, increased

of operating comfort

Simplification of maintenanceservice

Realization of function flight control based on IMA;

Deep integration of components, including auto-throttle system;

Creation of active control systems;

The use of electromechanical and combined drives;

Automation of management with use of information from the advanced functions of monitoring regimes;

The introduction of the concept of reconfiguration of control in case of failure

Improvement of environmental performance


Requirements to the technologies

Compliance with the common world scientific and technical documentation, certificatability;

Generally accepted among the leading aircraft companiesof the world system of specifications with tracing of the requirements;

Automation and the fullness of the development processes;

Openness


Creation of through automated technologies of the development of onboard avionics suite

Development of means for complex automation for model designing of onboard avionics suite , the identification of system requirements and automatically generate of configuration data

Design automation of onboard avionics suite

IMA SYSTEMDATABASEAutomated

ConfigurationData Gathering

Avionics architecture models

Syst

em

Re

qu

ire

me

nts

UPPER LEVELAVIONICSARCHITECTURE• avionics systemsand its interactions

AVIONICS INTERFACES’MODEL• avionics components’ dataexchange model

AVIONICS ARCHITECTURE MODEL• avionics system decomposition;• intersystem information flows

model;• reliability requirements model;• functional failure model

FAIL-SAFETY ANALYSIS

INTERFACES HARMONIZATION

MODELS OF FUNCTIONS: •interface•resources required

EQUIPMENT MODELS: •interfaces•specifications•performance AIRCRAFT

SYSTEMSCENTRAL CRATES HUBS DISPLAYS/

CONSOLESAVIONICS

AIRCRAFTSYSTEMS

COMMUNI-CATIONS

MAIN-TENANCE

AUTOPILOT,AUTO- THRUST

FLIGHT MANAGEMENT

SYSTEM

NETWORK LOAD ANALYSISINTERFACES HARMONIZATION

MISSION PROFILE CHECKRESOURCE ALLOCATION CHECK

ELECTRONICDISPLAY

AND ALARMSYSTEM


Integration of onboard avionics suite

TRACEABILITY AND INTRODUCTION CHANGE OF PROBLEMSAUDIT AND EXAMINATION OF MATERIALS SUPPLIERS OF EQUPMENT BY CUSTOMER IN ALL PLACES OF DEVELOPMENT

INTEGRATED TESTINGOF STAFF SET

OF ONBOARD AVIONICS

TEST BENCH «ELECTRONIC BIRD»

ONBOARD INTEGRATION BENCHOF SEVERAL FUNCTIONS OF

SUPPLIERS


Bench equipment

Subsystem bench for developing of electronic indication for the МС-21 airplane

Integrated bench


Thank you!

Questions?

International conference

Moscow, 29-30 October 2012 г.

Documents

Condition and prospects of development of integrated modular … · 2012. 11. 19. · Integrated IMA/SDR – system of navigation and landing Crates #1 Crates #2 Crates #3 Crates