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Concept of the magnetic launcher for medium class unmanned aerial vehicles designed on the basis of numerical calculations

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents a concept of a magnetic coil launcher for unmanned aerial vehicles of mass up to 25 kg. The idea is not new, nevertheless in the paper, an innovative application of magnetic launcher technology for selected class of unmanned aerial vehicles is presented. So far, at Bialystok University of Technology, a magnetic coil launcher for micro aerial vehicles of mass up to 2.5 kg has been investigated. In the article, simulations of a conceptual multi-coil launcher with a magnetic core system are presented. The finite element method has been used in calculations. Moreover, in the paper, the concept of a magnetic support for transmission of mechanical power from the magnetic core to the launched payload is proposed. The applied methodology, computational results and potential technical difficulties of practical applications are also widely discussed.
Rocznik
Strony
163--177
Opis fizyczny
Bibliogr. 20 rys., rys.
Twórcy
  • Faculty of Mechanical Engineering, Bialystok University of Technology (BUT), Białystok, Poland
autor
  • Faculty of Mechanical Engineering, Bialystok University of Technology (BUT), Białystok, Poland
Bibliografia
  • 1. Arnold Magnetic Technologies Co., 2014, www.arnoldmagnetic.com (15.06.2014)
  • 2. Gosiewski Z., Ambroziak L., 2012, Formation flight control scheme for unmanned aerial vehicles, Lecture Notes in Control and Information Science, 422, 331-340
  • 3. Gosiewski Z., Cieśluk J., Ambroziak L., 2011, Vision-based obstacle avoidance for Unmanned Aerial Vehicles, 4th International Congress on Image and Signal Processing, P. Qiu, Y. Xiang, Y. Ding, D. Li, L. Wang (Edit.), IEEE, 2053-2058
  • 4. Kolm H., Mongeau P., Williams F., 1980, Electromagnetic launchers, IEEE Transactions on Magnetics, Mag-16, 5, 719-721
  • 5. Kondratiuk M., 2013, Designing and investigating of the magnetic coil launcher with controlled acceleration of the launching object (in Polish), PhD thesis, BUT
  • 6. Kondratiuk M., Gosiewski Z., 2013a, Laboratory stand of an electromagnetic multi-coil launcher for micro aerial vehicles, Mechatronic Systems and Materials IV, Z. Gosiewski, Z. Kulesza (Edit.), Durnten-Zurich, Trans-Tech Publications, Solid State Phenomena, 334-339
  • 7. Kondratiuk M., Gosiewski Z., 2013b, Simulation model of an electromagnetic multi-coil launcher for micro aerial vehicles, Mechatronic Systems and Materials IV, Z. Gosiewski, Z. Kulesza, Durnten-Zurich, Solid State Phenomena, 406-411
  • 8. Kondratiuk M., Gosiewski Z., 2014, Comparison of electromagnetic coil launcher model with real-device characteristics, Solid State Phenomena, 214, 58-66
  • 9. Kownacki C., 2013, Successful application of miniature laser rangefinders in obstacle avoidance method for fixed wing MAV, International Journal of Robotics and Automation, 28, 3, 292-298
  • 10. Ładyżyńska-Kozdraś E., Falkowski K., Sibilska-Mroziewicz A., 2014a, Physical model of the cart of an UAV catapult using Meissner effect (in Polish), [In:] Mechanika w Lotnictwie, ML-XVI 2014, t. II, K. Sibilski (Edit.), PTMTS Warsaw, 231-241
  • 11. Ładyżyńska-Kozdraś E., Falkowski K., Sibilska-Mroziewicz A., 2014b, Vibration analysis of a levitating cart of a magnetic catapult (in Polish), [In:] Mechanika w Lotnictwie, ML-XVI 2014, t. II, K. Sibilski (Edit.), PTMTS Warsaw, 243-250
  • 12. McNab I., 2007, A research program to study airborne launch to space, IEEE Transactions on Magnetics, 43, 1, 486-490
  • 13. Mystkowski A., 2013, Piezo-stack vortex generators for boundary layer control of a delta wing micro-aerial vehicle, Mechanical Systems and Signal Processing, 40, 783-790
  • 14. Mystkowski A., 2014, Implementation and investigation of a robust control algorithm for an unmanned micro-aerial vehicle, Robotics and Autonomous Systems, 62, 1187-1196
  • 15. Patterson D., Monti A., Brice C., Dougal R., Pettus R., Srinivas D., Dilipchandra K., Bertoncelli T., 2002, Design and simulation of an electromagnetic aircraft launch system, Industry Applications Conference, 37th IAS Annual Meeting, 1950-1957
  • 16. Perkowski W., 2008, Pneumatic launcher for unmanned aerial vehicles, Transport and Engineering, 27, 181
  • 17. Sibilski K., Falkowski K., Olejnik A., 2014, Magnetic take-off and landing system of airplanes – project GABRIEL (in Polish), [In:] Mechanika w Lotnictwie, ML-XVI 2014, t. II, K. Sibilski (Edit.), PTMTS Warsaw, 216-229
  • 18. Tomczuk B., Schroder G., Waindok A. ¨ , 2007, Finite element analysis of the magnetic field and electromechanical parameters calculation for a slotted permanent magnet tubular linear motor, IEEE Transactions on Magnetics, 43, 7, 3229-3236
  • 19. Tomczuk B., Waindok A., 2009, 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, 343-360
  • 20. Tomczuk B., Waindok A., Wajnert D., 2012, Transients in the electromagnetic actuator with the controlled supplier, Journal of Vibroengineering, 14, 1, 39-44
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniajacą naukę.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-52f16eba-8429-421a-8b63-1aa4b37648a0
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