Affordable Access

Conclusions and Future Work

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

Abstract

Neural partial differentiation (NPD) method is used for the parameter estimation. For this purpose initially, a neural model of multi-input and multi-output (MIMO) aircraft system is established. In addition to that, separate consideration of the longitudinal and lateral-directional dynamics simplifies the model considerably in terms of structure and the number of parameters.

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