Comparison of Electromagnetic Coil Launcher Model with Real-Device Characteristics

Mirosław Kondratiuk; Zdzisław Gosiewski

doi:10.4028/www.scientific.net/SSP.214.58

Paper Titles

Influence of the Electrodeposition Cathodic Potential on the Composition and Magnetic Properties of CoNi Nanowires
p.32

Modeling the Electrical Behavior of Lithium-Ion Batteries for Electric Vehicles
p.40

Identification of Static Unbalance Wheel of Passenger Car Carried out on a Road
p.48

Comparison of Electromagnetic Coil Launcher Model with Real-Device Characteristics
p.58

Engine Control Unit Testing by Hardware-in-the-Loop Simulation
p.67

Technique for Analysis of the Spatial Field Distribution in Tapered Wire Medium
p.75

Introduction to the Conception of Combustion Process Onboard Monitoring System
p.83

Mechatronic Design of an Integrated Vehicle Dynamics Control for an Energetic Optimized Battery Electric Vehicle
p.94

HomeSolid State PhenomenaSolid State Phenomena Vol. 214Comparison of Electromagnetic Coil Launcher Model...

Comparison of Electromagnetic Coil Launcher Model with Real-Device Characteristics

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.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Solid State Phenomena (Volume 214)

Pages:

58-66

DOI:

https://doi.org/10.4028/www.scientific.net/SSP.214.58

Citation:

Cite this paper

Online since:

February 2014

Authors:

Mirosław Kondratiuk*, Zdzisław Gosiewski

Keywords:

Coil Launcher, Electromagnetic Launcher, Finite Element Method in Magnetic Calculations, Unmanned Aerial Vehicles Catapult

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[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.

Google Scholar

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

DOI: 10.4028/www.scientific.net/ssp.147-149.438

Google Scholar

[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.

Google Scholar

[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.

DOI: 10.1007/978-1-4471-2343-9_28

Google Scholar

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

DOI: 10.4028/www.scientific.net/ssp.198.232

Google Scholar

[6] B. Tomczuk, A. Waindok: Linear Motors in Mechatronics – Achievements and Open Problems, Transfer of Innovation to the Interdisciplinary Teaching of Mechatronics for the Advanced Technology Needs, Opole University of Technology, Opole, 2009, pp.358-377.

Google Scholar

[7] B. Tomczuk, A. Waindok: A coupled field-circuit model of a 5-phase permanent magnet tubular linear motor, Archives of Electrical Engineering, Vol. 60, no. 1, 2011, pp.5-14.

DOI: 10.2478/v10171-011-0001-z

Google Scholar

[8] A. Waindok, G. Mazur: Mutual Inductances in a Mathematical Model of the Three-Stage Reluctance Accelerator, 3rd International Students Conference on Electrodynamics and Mechatronics (SCE III), October 6-8, 2011, Opole, Poland, pp.115-118.

DOI: 10.1109/sce.2011.6092136

Google Scholar

[9] B. Reck, "First Design Study of an Electrical Catapult for Unmanned Air Vehicles in the Several Hundred Kilogram", IEEE Transaction on Magnetics, Vol. 3, No 1, p.15–64, 2003.

DOI: 10.1109/tmag.2002.805921

Google Scholar

[10] W. Dengwu,L. Shaoke, L. Zhenxiang: Study of a Rail-Coil Hybrid Electromagnetic Launcher, Electrical Machines and Systems, 2008, pp.944-947.

Google Scholar

[11] M. Kondratiuk, Z. Gosiewski: Simulation Model of an Electromagnetic Multi-Coil Launcher for Micro Aerial Vehicles, Solid State Phenomena, Vol. 198, pp.406-411, Switzerland, 2013.

DOI: 10.4028/www.scientific.net/ssp.198.406

Google Scholar

[12] M. Kondratiuk, Z. Gosiewski: Laboratory Stand of an Electromagnetic Multi-Coil Launcher for Micro Aerial Vehicles, Solid State Phenomena, Vol. 198, pp.334-339, Switzerland, 2013.

DOI: 10.4028/www.scientific.net/ssp.198.334

Google Scholar

[13] J. F. Gieras, Z. J. Piech, B. Z. Tomczuk: Linear Synchronous Motors: Transportation and Automation Systems, 2nd Edition, Taylor & Francis, 2012.

DOI: 10.1201/b11105

Google Scholar

[14] COMSOL Multiphysics, AC/DC Module User's Guide, COMSOL AB, October, 2011.

Google Scholar