M. Renard, C. Migeon, F. Tristant, F. Terrade, J.P. Moreau, M. Poncon, S. Guillet, J.A. Rouquette, C. Girard, N. Gouedard, A. Guena, P. Lalande, P. Laroche, J.-P. Parmantier, I. Junqua, F. Issac, L. Guibert, R. Perraud, I. Revel, G. Peres, J.-P. Estienne, J. Aspas-Puertolas, M. Ridel, S. Houhou

The need for optimization in terms of time and costs in specification, development, qualification and through life processes of Aircraft submitted to various electromagnetic environments has led to classify operational and safety objectives into categories ranging from primordial to desirable. In order to quantify safety objectives, a probability of success is allocated for each of them. For all aircraft manufacturers the current hardening process of aircrafts mainly relies on development tests, normative equipment qualification tests, and aircraft qualification ground tests, repeated for each category of environmental electromagnetic threat. This procedure has several limitations such as the availability of test setting, aircraft and equipment and implies to deal with extensive tests that imperfectly simulate the real stress. The purpose of the MOVEA - Aircraft Electromagnetic Vulnerability Operative Model - is to optimize this process by enhancing aircraft manufacturers use of modelling with the help of a computer platform dedicated to the computation of the risk of failure for environmental envelopes enacted by certification or for a specific mission flown by an aircraft under electromagnetic environment conditions.

35th European Rotorcraft Forum 2009,

Conference Paper

englisch

21,0 x 29,7 cm, 13 Seiten

DGLR-Bericht, 2009, 2009-03, 35th European Rotorcraft Forum 2009 - Conference Proceedings; S.1-13; 2009; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

in getr. Zählung;

rotorcrafts, electromagnetic interference

Bestellbar

2009