Jean-Luc Ferrato

Development of embedded control, guidance and navigation algorithms for medium and long-range missiles. The missions also include the design of ground-based aircraft-to-missile alignement process analysis.

Design of Navigation, Control and Guidance systems for a low cost air-to-ground missile. Main aspects concern the design and the performance comparisons of navigation systems leading on robust Kalman filters based on gyrometer and magnetometer measurements. Design of robust guidance and control loops

As part of the NH90 integration team (CORE and FCS benchtests) I was in charge of the development of a software (in java) interpreting and plotting data coming from avionic data bus acquisition cards (MIL 1553 and ARINC 429) for PC (with treatment of ACCESS databases) and SUN Platform (with treatment of ORACLE databases). My mission also included validation tests for the NH90 flight by wire system