Fuzzy Logic-Based Models of Transport Aircraft in Avoidance of Runway Excursion

DOI

10.2991/amsm-16.2016.52How to use a DOI?

Keywords

internal functions; membership function; fuzzy-logic modeling (FLM); flight data recorder (FDR)

Abstract

The flight dynamic equations in mathematics for aircraft response to the crosswind effects during the landing are highly non-linear partial differential equations. The main objective of this paper is to present fuzzy-logic modeling (FLM) technique to establish flight control models with the function of nonlinear dynamic inversion based on the datasets from the flight data recorder (FDR) for the purpose to solve the mathematical problems in engineering and safety problems in aviation community. A twin-jet transport with the runway excursion event due to crosswind effects during the landing will be the study case. The non-linear multi-dimensional numerical analysis technique to be used to analyze the causes of this flight event, emphasis to be placed on finding observable parameters for pilots to make appropriate actions are presented in this paper.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Ray chung Chang
PY  - 2016/05
DA  - 2016/05
TI  - Fuzzy Logic-Based Models of Transport Aircraft in Avoidance of Runway Excursion
BT  - Proceedings of the 2016 International Conference on Applied Mathematics, Simulation and Modelling
PB  - Atlantis Press
SP  - 228
EP  - 232
SN  - 2352-538X
UR  - https://doi.org/10.2991/amsm-16.2016.52
DO  - 10.2991/amsm-16.2016.52
ID  - Chang2016/05
ER  -