Autors: Georgieva, H. I., Serbezov, V. S.
Title: Mathematical model of aircraft ground dynamics
Keywords: aircraf ground dynamics, aircraft ground movement modelling, aircraft weigt distrubution, aircraft center of gravity, steering angle

Abstract: This paper presents a mathematical model with 3 degrees of freedom developed in Matlab/Simulink environment for numerical simulation of aircraft ground dynamics. As a reference aircraft Airbus A319 midsize commercial passenger aircraft has been chosen. The model takes into account the forces and moments generated by the aircraft (aerodynamics and thrust) and the forces generated in the landing gear tires. The model was validated against a simplified takeoff run model derived from aircraft flight records. For qualitative model assessment two cases of curvilinear aircraft ground motion were simulated and analyzed. In these simulations the aircraft weight and center of gravity position were varied as a parameter of operational relevance.


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Цитирания (Citation/s):
1. Dai, Y., Song, J., Yu, L., Lu, Z., Zheng, S., & Li, F. (2019). The lateral control during aircraft-on-ground deceleration phases. Aerospace Science and Technology, 95, 105482. - 2019 - в издания, индексирани в Scopus или Web of Science
2. Sadien, E., Roos, C., Birouche, A., Carton, M., Grimault, C., Romana, L. E., & Basset, M. (2020). A simple and efficient control allocation scheme for on-ground aircraft runway centerline tracking. Control Engineering Practice, 95, 104228. - 2020 - в издания, индексирани в Scopus или Web of Science
3. Theuma, K., Chircop, K., Gauci, J., & Zammit-Mangion, D. (2019). Implementation and Evaluation of a Multimodel Filter for Aircraft Ground Operations. Journal of Air Transportation, 27(4), 153-163. - 2019 - в издания, индексирани в Scopus или Web of Science
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Вид: публикация в международен форум, публикация в реферирано издание, индексирана в Scopus