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Research Article | Open Access |

Application of Fuzzy Abduction Technique in Aerospace Dynamics

Author 1: Sudipta Ghosh Author 2: Souvik Chatterjee Author 3: Binanda Kishore Mondal Author 4: Debasish Kundu
International Journal of Advanced Computer Science and Applications (IJACSA) · Vol. 7, No. 5 · Published 2016

DOI: 10.14569/IJACSA.2016.070534

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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

How to Cite this Article

Ghosh, S., Chatterjee, S., Mondal, B. K., & Kundu, D. (2016). Application of Fuzzy Abduction Technique in Aerospace Dynamics. International Journal of Advanced Computer Science and Applications, 7(5). https://doi.org/10.14569/IJACSA.2016.070534

Ghosh, Sudipta, et al.. "Application of Fuzzy Abduction Technique in Aerospace Dynamics." International Journal of Advanced Computer Science and Applications, vol. 7, no. 5, 2016, https://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},
  volume    = {7},
  number    = {5},
  year      = {2016},
  publisher = {The Science and Information Organization},
  author    = {Sudipta Ghosh and Souvik Chatterjee and Binanda Kishore Mondal and Debasish Kundu},
  doi       = {10.14569/IJACSA.2016.070534},
  url       = {https://doi.org/10.14569/IJACSA.2016.070534}
}

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Volume 17 No. 11, November 2026
Paper Submission Due October 25, 2026
Review Notification November 15, 2026
Publication Date November 30, 2026
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