Comparison of Electromagnetic Coil Launcher Model with Real-Device Characteristics

Author:

Kondratiuk Mirosław1,Gosiewski Zdzisław1

Affiliation:

1. Bialystok University of Technology

Abstract

In this paper we describe a numerical model and a construction of an electromagnetic launcher (EML) consisting of ten copper coils located serially. The solenoids were mounted on the pipe-shaped slideway, inside which, the ferromagnetic core was moved driven by the coils magnetic force. The paper presents the model of an EML based on circuit approach involving lumped parameters which were obtained by means of a finite element methods (FEM). The numerical representation contained a mechanical part with introduced friction coefficients. In the article we proposed an algorithm which enabled us to fit the numerical model to the constructed device by selection of these friction parameters values. Thus, we were able to compare the signals from computer simulations and measurements which were taken during laboratory tests.

Publisher

Trans Tech Publications, Ltd.

Subject

Condensed Matter Physics,General Materials Science,Atomic and Molecular Physics, and Optics

Reference14 articles.

1. Z. Gosiewski, M. Kondratiuk: Introductory investigations of unmanned aerial vehicles (UAV) coil launcher, Scientific Proceedings of Riga Technical University, Series 6, Transport and Engineering. Transport. Aviation Transport, N27, Ryga, (2008).

2. Gosiewski Z., Kondratiuk M.: Selection of Coils Parameters in Magnetic Launchers, Solid State Phenomena Vols. 147-149, (2009).

3. Z. Gosiewski, M. Kondratiuk: Modelling of electromagnetic coil with mobile core for designing motion control in electromagnetic launchers, Transfer of Innovation to the Interdisciplinary Teaching of Mechatronics for an Advanced Technology Needs, Eds. E. Macha and G. Robak, Opole University of Technology, Opole, (2009).

4. Z. Gosiewski, L. Ambroziak, Formation Flight Control Scheme for Unmanned Aerial Vehicles, Lecture Notes in Control and Information Science, vol. 422, pp.331-340, Springer Verlag, (2012).

5. L. Ambroziak, Z. Gosiewski, Preliminary UAV Autopilot Integration and In-Flight Testing, Solid State Phenomena, vol. 198, 2013, pp.232-237.

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