Hover flight control of helicopter using optimal control theory

This paper represents the optimal control theory and its application to the full scale helicopters. Generally the control of a helicopter is a hard task, because its system is very nonlinear, coupled and sensitive to the control inputs and external disturbances which might destabilize the system. As...

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Bibliographic Details
Main Authors: Ahmed ABOULFTOUH, Gamal EL-BAYOUMI, Mohamed MADBOULI
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2015-09-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/aboulftouh_elbayoumi_madbouli_vol_7_iss_3.pdf