Improved Design and Implementation of Automatic Flight Control System (AFCS) for a Fixed Wing Small UAV

This paper presents an implementation of automatic flight control system (AFCS); analyzes and assures its performance during model in loop (MIL), software in loop (SIL), and processor in loop (PIL) stages. Based on both linear and analytic linear models with trimmed values of straight and leveling s...

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Bibliographic Details
Main Authors: A. E. A. Elbanna, T. H. M. Soliman, A. N. Ouda, E. M. Hamed
Format: Article
Language:English
Published: Spolecnost pro radioelektronicke inzenyrstvi 2018-08-01
Series:Radioengineering
Subjects:
Online Access:https://www.radioeng.cz/fulltexts/2018/18_03_0882_0890.pdf