ATE & Test Systems
Data Patterns Pvt. Ltd. (Data Patterns Pvt. Ltd.)
Data Patterns' core business for over 20 years has been the development of Automated Test Equipment for critical aerospace requirements. Data Patterns developed a Multi Programmer with associated test automation software in 1994. Christened the DP-800 this product was adopted for the implementation of test rigs for Navigation Platform Test Benches, Engine Test Bed Automation, Cable Harness Test Systems, etc. This product was effectively utilized in the development of test benches required by Indian Space Research Organisation (ISRO) for the Polar Satellite Launch Vechicle (PSLV) and Geo Stationary Launch Vehicle (GSLV). Based on this foundation, the next generation test benches were developed in the cPCI architecture. Presently, Data Patterns develops cPCI based test systems for Laboratory applications as well as VME based test systems for challenging environmental conditions. Examples of test solutions built by Data Patterns are indicated below.
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Avionics Suite Tester
Based on order from the Navy, Data Patterns developed the complete Automated Test Equipment required for validating all the Line Replaceable Units (LRUs) utilized in the Seaking Helicopter. The upgrade was carried out at multiple Naval bases in India.
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Brahmos Checkout
Data Patterns designed and built the BrahMos Missile Checkout Equipment based on the requirements and support of DRDO and BrahMos. This unit validates the complete performance of the Missile through interfacing with it's umbilical and maintenance connections. The shelter mounted checkout equipment is utilized to test the articles on the field during it's life cycle, thus ensuring readiness for launch on demand.
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Digital Flight Control Computer
The Digital Flight Control Computer is a Quadruple Redundant Flight Control Computer designed by DRDO and ADE and manufactured by Bharat Electronics Limited. Data Patterns has designed and manufactured the Automated Test Equipment required for the validation of this DFCC.
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Go No Go Testers
Go No Go Testers are developed in portable formats. Typically these are utilized at 'I' Level and 'O' Level test requirements and clear the aircraft LRU for flight.
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Power Module Tester
The Power Module Checkout ATE is developed for testing DC-DC Power modules typically utilized in India's space program. The DC-DC converters are exhaustively tested for all design parameters including supply voltage range, line and load regulation, efficiency, ripple, noise, transient response and so on. Special power sources and loading mechanisms are deployed to enable testing of various types of power modules.
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Generic RF ATE Test
The Generic RF ATE is developed to test the Radar and Radar Subsystems. The ATE is primarily built using an instrumentation control, precision RF routing systems and rack mounted test instruments. Generic RF ATE system enables measurement of parameters of Radar equipment such as Local Oscillators, Waveform Generators, Up and Down Converters, Analog Receivers, Array Group Receiver Units, TR Modules. The ATE is configured to test the Radars upto 18GHz frequency range.
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Cable Harness Test System
Data Patterns has built high reliability Cable Harness Test Systems for large installations. These are primarily used in launch vehicle aircraft and missile level cable harness test validation. Installations with upto 20,000 lines test capability at a single location have been supplied by Data Patterns. Portable version capable handling of as small as 384 points have also been addressed.
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Bus Management Test System
Solution to test redundant Architecture of BMUComprehensive test system performing tests of > 3000 I/O's Special test circuits using hybrid / ceramic components to operate in Thermovac chamber Tests various subsystem functionalities like, AOCS, Sensor Electronics, Telemetry, Tele-command with Self test and application test software
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Count Down Test System
The Second Launch Pad Count Down system is implemented using VXI hardware designed by Data Patterns specific to the application requirements, featuring a redundant system handling upto 14000 I/O points.
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Instrument Test Unit
Instrument Test Unit For Advanced Inertial Sensors (INTU) is used for testing and evaluation of Ring Laser Gyro (used in GSLV/PSLV launch vehicles), that detects the angular displacement during rotation. The INTU receives displacement signals from the sensor (RLG) to evaluate the sensor characteristics and also generates signals required towards initiating the action of the sensor.
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Redundant Strap down INS ATE Test Station
Redundant Strap down Inertial Navigation System (RESINS) checkout test station comprises of cPCI chassis with various functional I/O modules like ADC, DAC, DIO, VFC, Relay matrix, MIL 1553, GPIB, Serial communication interfaces and Custom Built System interface adaptor.
