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2021 | OriginalPaper | Chapter

3. Identification of Aircraft Longitudinal Derivatives

Authors : Majeed Mohamed, Vikalp Dongare

Published in: Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation

Publisher: Springer Singapore

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Abstract

This chapter focuses on the application of neural networks to the problem of aircraft aerodynamic modeling and parameter estimation. The neural modeling and neural partial differentiation (NPD) method, which are presented in Chap. 2, are directly applied here to estimate the longitudinal dynamics of an aircraft system. Since the model of an aircraft system is established through the neural network, extends the use of NPD to multi-input and multi-output (MIMO) system ensures online estimation of each aircraft aerodynamics derivatives.

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previous chapter Neural Modeling and Parameter Estimation

next chapter Identification of Aircraft Lateral-Directional Derivatives

G. Chowdhary, R. Jategaonkar, Aerodynamic parameter estimation from flight data applying extended and unscented kalman filter. Aerosp. Sci. Technol. 14(2), 106–117 (2010)CrossRef

V. Klein, E.A. Moreli, Aircraft System Identification Theory and Practice, AIAA, Education Series (American Institute of Aeronautics and Astronautics, Reston, VA, 2006)CrossRef

M. Majeed, Aircraft System Identification and Control (LAP LAMBERT Academic Publishing, Saarbrücken, 2014)

M. Majeed, V. Dongare, Neural partial differentiation based aircraft parameter estimation from flight data, in Indian Control Conference (2015), pp. 397–402

M. Majeed, I.N. Kar, Aerodynamic parameter estimation using adaptive unscented kalman filter. Int. J. Aircr. Eng. Aerosp. Technol. 85(4), 267–279 (2013)CrossRef

M. Sinha, R.A. Kuttieri, S. Chatterjee, Nonlinear and linear unstable aircraft parameter estimations using neural partial differentiation. J. Guid. Control Dynam. 36(4), 1162–1176 (2013). https://doi.org/10.2514/1.57029

S. Singh, A.K. Ghosh, Estimation of lateral-directional parameters using neyral networks based modified delta method. Aeronaut. J. 111(3150), 659–667 (2007)

Title: Identification of Aircraft Longitudinal Derivatives
Authors: Majeed Mohamed
Vikalp Dongare
Publisher: Springer Singapore
Book: Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation
Print ISBN: 978-981-16-0103-3

Electronic ISBN: 978-981-16-0104-0

Copyright Year: 2021
DOI: https://doi.org/10.1007/978-981-16-0104-0_3

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