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Markus Schneider  - - - 
Top co-authors See all
B. Tellini

36 shared publications

Department of Energy, Systems, Land and Constructions Engineering, University of Pisa, Pisa, Italy

R. Ciolini

17 shared publications

Department of Civil and Industrial Engineering, University of Pisa, Largo Lazzarino 1, Pisa I-56122, Italy

Caroline Gauthier-Blum

5 shared publications

The French-German Research Institute of Saint-Louis, F-68301 Saint Louis CEDEX, France;(M.S.);(C.G.-B.)

Guillaume Kock

5 shared publications

Institut d’Électronique et des Systèmes, Université de Montpellier, IES, F-34090 Montpellier, France;(P.C.);(M.T.);(A.G.)

Alessandra Petri

3 shared publications

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Distribution of Articles published per year 
(2008 - 2019)
Total number of journals
published in
 
6
 
Publications See all
Article 0 Reads 0 Citations Experimental and Numerical Study of a Thermal Expansion Gyroscope for Different Gases Guillaume Kock, Philippe Combette, Marwan Tedjini, Markus Sc... Published: 17 January 2019
Sensors, doi: 10.3390/s19020360
DOI See at publisher website PubMed View at PubMed ABS Show/hide abstract
A new single-axis gas thermal gyroscope without proof mass is presented in this paper. The device was designed, manufactured and experimentally characterized. The obtained results were compared to numerical simulation. The working principle of the gyroscope is based on the deflection of a laminar gas flow caused by the Coriolis effect. A bidirectional hot air flow is generated by alternating activation of two suspended resistive micro-heaters. The heated gas is encapsulated in a semi-open cavity and the gas expands primarily inside the cavity. The thermal expansion gyroscope has a simple structure. Indeed, the device is composed of a micromachined cavity on which three bridges are suspended. The central bridge is electrically separated into two segments enabling to set up two heaters which may be supplied independently from each other. The two other bridges, placed symmetrically on each side of the central bridge, are equipped with temperature detectors which measure variations in gas temperature. The differential temperature depends on the rotational velocity applied to the system. Various parameters such as the heating duty cycle, the type of the gas and the power injected into the heaters have been studied to define the optimal working conditions required to obtain the highest level of sensitivity over a measurement range of around 1000°/s. The robustness of the device has also been tested and validated for a shock resistance of 10,000 g for a duration of 400 µs.
Article 0 Reads 0 Citations Resonant Shield Concept as Alternative Solution in Railguns Mauro Bologna, Mirko Marracci, Roberto Micheletti, Markus Sc... Published: 01 May 2015
IEEE Transactions on Plasma Science, doi: 10.1109/tps.2015.2406393
DOI See at publisher website
PROCEEDINGS-ARTICLE 0 Reads 0 Citations Resonant shield concept as alternative solution in railguns M. Bologna, Mirko Marracci, R. Micheletti, Markus Schneider,... Published: 01 July 2014
2014 17th International Symposium on Electromagnetic Launch Technology (EML), doi: 10.1109/eml.2014.6920687
DOI See at publisher website
PROCEEDINGS-ARTICLE 0 Reads 0 Citations Distributed laboratory system for characterization of current distribution in electromagnetic rail launchers Bernardo Tellini, Mirko Marracci, Roberto Ferrero, Saulius B... Published: 01 October 2011
2011 IEEE International Workshop on Measurements and Networking Proceedings, doi: 10.1109/iwmn.2011.6088501
DOI See at publisher website
Article 0 Reads 1 Citation Characterization of EM Emission During the Operation of Solid and Plasma Armature Rail Launchers Giancarlo Becherini, Sebastiano Di Fraia, Gianluca Genovesi,... Published: 01 January 2011
IEEE Transactions on Plasma Science, doi: 10.1109/TPS.2010.2086493
DOI See at publisher website
PROCEEDINGS-ARTICLE 0 Reads 0 Citations The Use of Electronic Components in Railgun Projectiles Riccardo Ciolini, Markus Schneider, Bernardo Tellini Published: 01 June 2008
2008 14th Symposium on Electromagnetic Launch Technology, doi: 10.1109/elt.2008.124
DOI See at publisher website
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