EU H2020 Project "MAGYCO (Mems based Appliance for GYro Compassing in general aviation and unmanned..)": description, partecipants, costs and EC-fundings

#	Pagina
attuale pagina	/open-h2020/projects/211182/index.html

MAGYCO project word cloud

Explore the words cloud of the MAGYCO project. It provides you a very rough idea of what is the project "MAGYCO" about.

ga improvements community respect uav horizontal ownership mechanical function limit instability allowed safety perform determined planning will reference sensors traffic regarding autonomous communication grade unscheduled players micro aerospace technique magyco attitude small core nominal magnetometers performed sigma cns frame accelerometer gyrocompassing manufacturers levels innovative 1 electro consequence aircraft taxi deg pitch bias efficiency self accelerometers mems initialization earth inertial usually air services demand vibratory sensing aiding realized hour accurate compass local gyros miniaturized external accuracy commercial investments unmanned attain 15 capacity angles solutions initial rate aviation shift roll surveillance navigation security vehicles operations interference suffer performance northfinding fractional affordable heading charter

Project "MAGYCO" data sheet

The following table provides information about the project.

Coordinator	GMA GENERALE MECCATRONICA APPLICATA SRL Organization address address: VIA SALVATORE PICCOLO SNC city: GIUGLIANO IN CAMPANIA postcode: 80014 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Italy [IT]
Project website	http://www.gmagroup.it/en/progetto-magyco/
Total cost	71˙429 €
EC max contribution	50˙000 € (70%)
Programme	1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport) 2. H2020-EU.2.1.1. (INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies - Information and Communication Technologies (ICT)) 3. H2020-EU.2.3.1. (Mainstreaming SME support, especially through a dedicated instrument)
Code Call	H2020-SMEINST-1-2016-2017
Funding Scheme	SME-1
Starting year	2017
Duration (year-month-day)	from 2017-07-01 to 2017-10-31

#	participants	country	role	EC contrib. [€]
1	GMA GENERALE MECCATRONICA APPLICATA SRL	IT (GIUGLIANO IN CAMPANIA)	coordinator	50˙000.00

GMA GENERALE MECCATRONICA APPLICATA SRL

IT (GIUGLIANO IN CAMPANIA)

coordinator

50˙000.00

Project objective

In the future the demand for air traffic services will increase and will shift towards more unscheduled operations for air taxi, charter, fractional ownership, and on-demand small low-cost aircraft (A/C). Many players of the aviation community are planning to make significant investments in the specific Communication, Navigation and Surveillance (CNS) systems improvements over the next years, in order to enhance efficiency, safety, capacity and security. Inertial Systems, core component of CNS systems, are used to measure the attitude of an A/C with respect to local reference frame (heading, pitch, roll angles) and are composed by a set of inertial sensors called gyros and accelerometers. The existing commercial solutions perform aiding through non-inertial sensors, usually magnetometers, which can suffer from external interference that produce non-nominal performance in terms of accuracy. For pitch and roll angles self-initialization can be effectively realized by exploiting accelerometer measurement. Regarding the heading term, it can be estimated by sensing the local horizontal component of Earth Rate using gyros. This self-initialization technique is called “gyrocompassing” or “northfinding”, since the function of the compass is performed by gyros. Earth Rate is in the order of 15°/hour. As a consequence, very accurate gyros must be adopted. Recently, the development of miniaturized vibratory gyros, such as Micro Electro Mechanical Sensors (MEMS), allowed to attain a bias instability levels better than 1°/hour. However, this limit does not ensure that initial heading is determined with accuracy in the range 1°-0.1° (1σ). MAGYCO project aims at the development of an innovative aerospace grade Inertial Unit based on miniaturized vibratory gyros with autonomous northfinding capabilities that can be used to improve the overall navigation capabilities of General Aviation (GA) aircraft and Unmanned Aircraft Vehicles (UAV) at affordable costs for the manufacturers.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "MAGYCO" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

The information about "MAGYCO" are provided by the European Opendata Portal: CORDIS opendata.

More projects from the same programme (H2020-EU.3.4.;H2020-EU.2.1.1.;H2020-EU.2.3.1.)