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.

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}
}