Designed Aircraft Structure Health Monitoring Solution for a US-Based Aerospace Company

US based company providing structural health monitoring for aircrafts, bridges, machinery and more.

• The client wanted to stabilize their existing solution to real-time monitor the structure health of an aircraft and comply it with stringent, military standard certifications

• Designed heterogeneous acquisition board to achieve time synchronization between data set of multiple sensors like piezoelectric, resistance temperature detectors, strain gauge for detecting composite damage, crack and impact that occur on aircraft structure
• Designed and developed firmware application to read the sensor data of Piezoelectric, Temperature, RTD, Strain Gauge sensors
• Supported high data acquisition speed up to 30kS/s
• Conducted pre-compliance tests for FCC class B, MIL-S-901, MIL-STD-167-1
• Performed functional validation of all the interfaces (SPI, UART, SDIO) with the hardware platform

• FCC, Military standard compliant (MIL-S-901, MIL-STD-167-1) rugged board design helped client to extend its solution reach to military applications