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Copyright Statement: This is an open access article licensed under a Creative Commons Attribution 4.0 International License, which permits unrestricted use, distribution, and reproduction in any medium, even commercially as long as the original work is properly cited.
Application of Fuzzy Abduction Technique in Aerospace Dynamics
Digital Object Identifier (DOI) : 10.14569/IJACSA.2016.070534
Article Published in International Journal of Advanced Computer Science and Applications(IJACSA), Volume 7 Issue 5, 2016.
Abstract: The purpose of this paper is to apply Fuzzy Abduction Technique in aerospace dynamical problem. A model of an aeroplane is proposed for consideration at different air density level of the atmosphere and at different speed of the plane. Different air density of the atmosphere, angle of wings and speed of the plane are selected as parameters to be studied. In this paper a method is developed to determine the angle of wings of the plane with respect to its axis at different air density level of the atmosphere and at different speed of the plane. Data are given to justify our proposed method theoretically.
Keywords: Fuzzy logic; Fuzzy abduction; Aerospace dynamics; Inverse Fuzzy relation
Sudipta Ghosh, Souvik Chatterjee, Binanda Kishore Mondal and Debasish Kundu, “Application of Fuzzy Abduction Technique in Aerospace Dynamics” International Journal of Advanced Computer Science and Applications(IJACSA), 7(5), 2016. http://dx.doi.org/10.14569/IJACSA.2016.070534
@article{Ghosh2016,
title = {Application of Fuzzy Abduction Technique in Aerospace Dynamics},
journal = {International Journal of Advanced Computer Science and Applications},
doi = {10.14569/IJACSA.2016.070534},
url = {http://dx.doi.org/10.14569/IJACSA.2016.070534},
year = {2016},
publisher = {The Science and Information Organization},
volume = {7},
number = {5},
author = {Sudipta Ghosh and Souvik Chatterjee and Binanda Kishore Mondal and Debasish Kundu}
}
