Ing. Mohamed Lafi

Design and test of FPGAs for Avionics applications

Hardware Development and Process Assurance for FPGA and Boards projects DO-254 (DAL-A): - VHDL Design and Simulation of FPGA modules. - Components reliability calculation (MIL-HDBK217F, IEC-62380). - Hardware life cycle data reviews. - Transitions Reviews: Design Review, Implementation Review, Test Review. - Records of activities and follow up. - Change requests validation CCB. - Flash Audits. - COTS Analysis.

- Generation of custom Linux OS using Buildroot. - Development of sensors drivers. - Communication between sensors and RaspberryPi2 to build end node. - Communication between Lora shield and RaspberryPi2 to build both end node (transmitter) and the gateway (receiver). - Cross compilation from SVN. - Schematic and Layout design of "EndNode" board using NXP JN5168 communication module and magnatic sensor LSM303D from ST. - Perform electronics tests for validation.

Design and Test of FPGA for machine command and control: • PWM generator for 2 motors. • Period measurement and reporting interface. • Frequency and dephasing measurement interface. • Temperature and pressure measurement interface. • EBI interface for communication with processor ATMEL (AT91M40). • ADC interface with SPI interface (LTC1856). • DAC interface with SPI interface (LTC2604).

Design and verification of fpgas for critical avionic systems following do-254 standard.

Embedded systems