Development for an inertial unit
We support our client in the development of an inertial unit hybridized with GPS and baro-altimetric data for civil aeronautics and based on a multi-mode Kalman filter. This project stems from R&D and aims to industrialize the product.
In this context, we support the project from preliminary design review to critical design review; Specifications and validation based on MBSE and High level of technical expertise.
