Fuzzy Logic-Based Models of Transport Aircraft in Avoidance of Runway Excursion
- 10.2991/amsm-16.2016.52How to use a DOI?
- internal functions; membership function; fuzzy-logic modeling (FLM); flight data recorder (FDR)
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.
- © 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/).
Cite this article
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 -