GYROWING

Highly integrated ultra-low-noise Gyrometer solution for Smart Fixed Wing Aircraft

 Coordinatore DOLPHIN INTEGRATION SA 

 Organization address address: Avenue du Granier 39
city: Meylan
postcode: 38242

contact info
Titolo: Mr.
Nome: Frédéric
Cognome: Masson
Email: send email
Telefono: +33 4 76 41 74 23
Fax: +33 4 76 90 29 65

 Nazionalità Coordinatore France [FR]
 Totale costo 765˙327 €
 EC contributo 573˙193 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2012-01
 Funding Scheme JTI-CS
 Anno di inizio 2012
 Periodo (anno-mese-giorno) 2012-12-01   -   2014-06-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    DOLPHIN INTEGRATION SA

 Organization address address: Avenue du Granier 39
city: Meylan
postcode: 38242

contact info
Titolo: Mr.
Nome: Frédéric
Cognome: Masson
Email: send email
Telefono: +33 4 76 41 74 23
Fax: +33 4 76 90 29 65

FR (Meylan) coordinator 573˙193.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

aircraft    electronic    gyrowing    asic    solution    performances    noise    voltage   

 Obiettivo del progetto (Objective)

'The GyroWing project is part of the global project “Smart Fixed Wing Aircraft” (SFWA), whose objectives address environmental issue (by increasing the performances of aircraft) and passenger comfort (in reducing noise level).

GyroWing represents an ASIC which aims at integrating the overall electronic control required for achieving the most miniaturized gyrometer.

After a specification phase and the system modelling, the project will enable the realization of this ASIC, including a high resolution electronic part, and its characterization after prototyping. GyroWing aims at providing high performances solutions, based on ultra-low noise analog front-end, with all its required peripherals (such as HF carrier, compensation paths, voltage reference, regulators, high voltage features…) for enabling the most integrated solution. This will result on a low volume, low weight and low bill of material final solution.

For achieving the highest TRL level for the ASIC, the project will be based on the experience of participant on avionics and inertial measurement units, but also on industrialization.'

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