À propos de cet article

Citez

[1] Chen, H., Q. Wang, H. Ho-Ching Iu, Acceleration Closed-Loop Control on a Switched Reluctance Linear Launcher, IEEE Trans. on Plasma Science, vol. 41, no. 5, May 2013, pp. 1131-1137. Search in Google Scholar

[2] K. Baoquan, L. Liyi, and Z. Chengming, Analysis and optimization of thrust characteristics of tubular linear electromagnetic launcher for space-use, IEEE Trans. Magn., 2009, 45(1), 250–254. Search in Google Scholar

[3] L. Li, H. Xuzhen, P. Donghua, and C. Jiwei, Magnetic Field of a Tubular Linear Motor With Special Permanent Magnet, IEEE Trans. Plasma Sc., 2011, 39(1), 83–86. Search in Google Scholar

[4] S. Barmada, A. Musolino, M. Raugi, and R. Rizzo, Analysis of the performance of a multi-stage pulsed linear induction launcher, IEEE Trans. Magn., 2001, 37(1), 111–115. Search in Google Scholar

[5] J. A. Andrews and J. R. Devine, Armature design for coaxial induction launchers, IEEE Trans. Magn., 1991, 27(1), 639–643 Search in Google Scholar

[6] N. Bianchi, S. Bolognani, D. Dalla Corte, and F. Tonel, Tubular Linear Permanent Magnet Motors: An Overall Comparison, IEEE Trans. Ind. Appl., 2003, 39(2), 466–47 Search in Google Scholar

[7] A. Crăciunescu, S. Grigorescu, I Potarniche, L.C. Codreanu, M.C. Gheamalinga, Electric motor and equipment for launching of investigation and intervention drones. Patent proposal no. A/00890 of 25.11.2015 Search in Google Scholar