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EW Suite Controller:
Developed in association with DRDO Lab, Manages CDU, CMDS, Flight Data Recorder, Interfaces with Transmitter, Central Receiver & Processor Unit. Based on COM 1GHZ Mobile Pentium Technology, MIL-STD-1553B interface, 512MB Flash for Data Recorder, 2 Port Ethernet channel. Audio output, Quad UART Channel - RS422. |
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Loop Back Tester:
Tester for GO/NOGO and Intermediate level, Portable, easy to use Tester for field-testing applications, Uses Loop Back Concept utilizing the LRU resources for testing. Detailed testing / diagnostics through PC Interface. |
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Exciter Controller :
Motorola Power Quice II Series (Processor MPC8280), 256MB Data Memory interface with host, Parallel 32 bit interface with DRFM, 10/100MBPS Ethernet, USB 2.0 |
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cPCI Main Controller:
Ruggedised for extended temperature operation, 6U footprint, COM 1GHz Pentium Mobile Technology, 1GB SDRAM, 8GB Flash, 2 Dual redundant MIL-STD-1553B Channels, gigabit and fast Ethernet, USB 2.0 quad channels, Virtex-4 FPGA for Reconfigurable I/O Capability, Audio Output. |
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IF Digital Receiver
8 Channel IF Digital Receiver Module on VME 64x
6U Form Factor
VME64x slave module
IF channel digitized using ADC with 100 Msps
Synchronized with external clock input
2 channels of synthesized waveform outputs |
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EW Simulator Interface Box
Standalone IO Interface and Simulator unit for EW Simulator Testing. Interfaces to Aircraft, Display Units, Break Box, Desktop PC and EW Simulator.
Facilities selection of Signal Source Aircraft/Simulator. Internally generates all blank signals for EW simulator in Simulator Mode.
Provision to change the Pulse Width and PRI of blanking pulse. LED Display of Pulse Width and Frequency for monitoring.
Routes 1553B bus connections either from Aircraft/RIG to EW Simulator. Communicates to Host PC using USB, RS232 and Ethernet Ports.
Converts RS422 signals to RS232 signals. Connects to Break Box for easy access and monitoring of all the IO signals. Uses 230VAC/1PH as supply.
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