CORDIS Project
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The project focuses on designing and testing a micro-electromechanical systems (MEMS) accelerometer for active control and health monitoring of wing structures. It aims to meet specific performance requirements for aerospace applications using advanced sensor technology.
The project aims at design and test of MEMS based accelerometer for wing structure active control and health monitoring.
The key requirements are: full scale of ±10 g; bandwidth >200 Hz; 1 year composite stability:
Bias:1.5 mg and SF: 1500 ppm; vibration rectification: 25 µg/g2; noise: <2 µg√Hz, warm-up transients: 10 µg/min, digital output and self test.
They will be achieved with a bulk micro-machined capacitive MEMS chip, Sigma Delta closed loop architecture with an analogue FE ASIC and an F…
Colibrys (Switzerland) Ltd
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