Aircraft System Identification Using Multi-Stage PRBS Optimal Inputs and Maximum Likelihood Estimator

A new method to discover open-loop, unstable, longitudinal aerodynamic parameters, using a ‘two-stage optimization approach’ for designing optimal inputs, and with an application on the fighter aircraft platform, has been presented. System identification of supersonic aircraft requires formulating o...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Muhammad Fawad Mazhar, Muhammad Wasim, Manzar Abbas, Jamshed Riaz, Raees Fida Swati
Format:	Article
Language:	English
Published:	MDPI AG 2025-01-01
Subjects:	aircraft system identification supersonic aircraft pseudo-random binary sequence input
Online Access:	https://www.mdpi.com/2226-4310/12/2/74