| Simulators
& Embedded Systems |
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Simulator for RADAR |
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Simulation for multiple RADARs Option to select
RADAR from which output is desired, data transfer
over Ethernet
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Simulator for Flight control System |
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Design and development of real time graphic
simulator for aircraft flight control system
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1553 Bus Protocol Simulator |
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Ability to accept raw data - pressure, GPS
position, radar data, etc., and transmit to
remote terminals
Porting of BSP, Writing boot code, Design
and Implementation of simulator
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Automated test equipment (ATE) for Mission
computer |
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Requirement - Testing for Mission Computer
(MC) and Display units (DU) Design of 1553B
and ARINC 429 interface boards
Board/FPGA design and testing Testing of MC
and DU
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Flash card interface for MC |
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Protocol definition between Flash card and
Mission computer (MC)
Implementation of software for communication
between Flash card and MC
Application development to activate sub-systems
based on data from Flash card Implementation
of fault tolerance on MC .
More |
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Cockpit Display Unit development |
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Ability to take input from different sub-systems
from the bus controller
Process the data and display in specific formats
Intelligent LCD units with dual processor
architecture to support redundancy
Multiplexed keyboard system to control other
systems .
More |
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| Embedded
Systems |
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12 Channel GPS receiver |
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Development of 12 Channel airborne GPS receiver
SCAT-1 landing capability
RTOS run time environment
Porting of air navigation software onto RTOS
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More |
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| 1553
Bus Manager |
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Capable of handling multiple 1553B buses Able
to send and receive messages from/to multiple
LRUs Send loop, poll and broadcast messages
Handle communication between LRUs .
More |
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Long range warning/tracking System |
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Processing and display of information from
RADAR in graphical and text formats Commander
and Automatic decision controls
Tracking using processed information Implemented
as distributed processor system
More |
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Software for Arinc |
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Integration and testing of Arinc card onto
68030 based VME System
Development of device drivers
communication over Arinc-429, RS-232 and RS-485
Development of Libraries and Diagnostics .
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Flight commander System |
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Process data received from RADAR
Display results in required formats
End use - at flight take off and landing
System design & development
Development of test software for validation
More |
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Controller and Independent limiter for
engine |
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Software for main controller and independent
limiter for aircraft engine Requirement analysis
and defining of specifications as per 80025A/2167A
standard
Design/development/testing for specific modules
- task initialization, interrupt handling,
control law software for startup and override
schedule of main engine fuel flow, interface
routines for communication on 1553 bus .
More |
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Air
Navigation Software |
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Enhancement to air navigation software for
performance in dynamic conditions Implementation
of multi-tasking module for background user
event processing
Improving efficiency of interrupt handling
routines.
More |
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Development of Mission Computer |
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Development of navigation, guidance functions
and MMI functions Process inputs from Pilot
and generation of warnings
Interface with Flight Control System, Environmental
System and Inertial Navigation System. .
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| Testing
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IVV of Flight Control System Software |
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System for flight control system reconfiguration
New reconfiguration approach based on fault
detection and system parameter estimation
Artificial intelligent techniques
Successful System modeling and testing in
a simulated environment .
More |
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Engine Testing |
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Full Authority Digital Electronic Computer
(FADEC) for TRENT 500, TRENT 700 Rolls Royce
engines and TAY engine for Gulfstream aircraft.
Dual channel. Control based on either channel.
Engine controller ARIINC 429 TESTED LEVEL-A
SW .
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Mission computer test software |
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486 based mission computer with 1553, Arinc
429 & discrete I/O controllers Design
and development of inbuilt instrument drivers
& test cases. Provision for test execution
in different modes Implementation using LabWindows
CVI with Test Executive and SQL Toolkit
More |
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Test Suite for Cockpit Display System |
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I960 based Display system with one Head-up
Display and two multi-function display surfaces
Static and Dynamic analysis of Display processor
software
Test cases and test suites for black box and
white box testing .
More |
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