Abstract
Research on aircraft takeoff taxiing model has a great significance upon evaluation of aircraft performance, design of airport runway and warfare simulation. Because the aircraft takeoff taxiing is a complex nonlinear process, existing numerical calculation models are ordinarily based on the energy method or assumption of moment equilibrium, which leads to complex modeling process and low precision. In this paper, we establish a takeoff taxiing model by numerical integration method which is easy to implement, and obtain the parameters of running distance calculation formula based on Lagrange interpolation algorithm [1]. At the end of this paper, we use the characteristic parameters of a specific aircraft as model inputs to validate the correctness and accuracy of this model by comparing the model output and actual flight data.
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References
Berrut, J.-P., Trefethen, L.N.: Barycentric Lagrange interpolation. SIAM Rev. 46(3), 501–517 (2004)
Gu, H.-B.: Dynamic model of aircraft ground handling. Acta Aeronautica Astronautica Sinica 22(2), 163–167 (2001)
Rolfe, J.M., Staples, K.J.: Flight Simulation, pp. 56–89. Cambridge University Press, Cambridge (1986)
Li, X.-y., Xing, X.: Design & implementation of civil transport takeoff performance program. J. Civil Aviation Univ. China 26(1), 8–13 (2008)
Hua, Z.: Research on aircraft engine modeling for flight simulation. Nanjing University of Aeronautics and Astronautics (2010)
Shui, Q.-c., Wang, Q.-h.: A mathematical model used to calculate the takeoff performance for an aircraft. Flight Dyn. 19(4), 70–74 (2001)
Fang, Z.-p.: Aircraft Flight Dynamics, p. 6. Beijing University of Aeronautics and Astronautics Press, Beijing (2005)
Johnson, S.A.: A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring. NASA Technical Memorandum 4240 (1990)
Song, H.-y., Cai, L.-c., Zheng, R.-h.: Numerical value integral improvement algorithm of aircraft take-off running distance. J. Traffic Transp. Eng. 7(2), 24–28 (2007)
Xiao, B., Zhang, H., Zhang, C.-z., Heng, J.: Multi-dimension interpolation algorithm and its simulation application. J. Syst. Simul. (2008)
Waters, M., Anthony, M.G.: Propulsion System Modeling and Takeoff Distance Calculations for a Powered-Lift Aircraft with Circulation-Control Wing Aerodynamics. AIAA-2009-1258 (2009)
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Zhang, M., Yao, Y., Wang, H. (2016). Aircraft Takeoff Taxiing Model Based on Lagrange Interpolation Algorithm. In: Zhang, L., Song, X., Wu, Y. (eds) Theory, Methodology, Tools and Applications for Modeling and Simulation of Complex Systems. AsiaSim SCS AutumnSim 2016 2016. Communications in Computer and Information Science, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-10-2666-9_11
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DOI: https://doi.org/10.1007/978-981-10-2666-9_11
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