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MAGYCO

Mems based Appliance for GYro Compassing in general aviation and unmanned aircraft applications

Total Cost €

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EC-Contrib. €

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Partnership

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 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.

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

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

 Partnership

Take a look of project's partnership.

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

Map

 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.

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

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