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Identification of Aircraft Longitudinal Derivatives

Authors
  • Mohamed, Majeed
  • Dongare, V
Publication Date
Jan 01, 2021
Source
National Aerospace Laboratories Institutional Repository
Keywords
License
Unknown

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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