Constraint Based Design of Multipole Field Electromagnetic Launcher using Gauss Method
Srichandan Kondamudi1, Mallikarjuna Rao Pasumarthi2
1Srichandan Kondamudi, Department of Electrical Engineering, Andhra University, Visakhapatnam (Andhra Pradesh), India.
2MallikarjunaRao Pasumarthi, Department of Electrical Engineering, Andhra University, Visakhapatnam (Andhra Pradesh), India.
Manuscript received on 15 September 2019 | Revised Manuscript received on 24 September 2019 | Manuscript Published on 10 October 2019 | PP: 907-911 | Volume-8 Issue-6S2, August 2019 | Retrieval Number: F12210886S219/19©BEIESP | DOI: 10.35940/ijeat.F1221.0886S219
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: Initiatives in electromagnetic propulsion all over the world are aimed at the development of electromagnetic launchers. This paper presents the constraint based design of Multipole Field Electromagnetic Launcher (MFEL). A design algorithm is developed based on Gauss iterative method. Muzzle velocity is considered as the objective function and the length, diameter and thickness of the accelerating coil are considered as constraints. The results for hexapole, octapole, decapole, dodecapole and hexadecapole cases are compared and tabulated.
Keywords: Electromagnetics, Flux Distribution, Lorentz Force, Electromagnetic Launcher.
Scope of the Article: Artificial Intelligent Methods, Models, Techniques