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...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2015-09-01
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Series: | INCAS Bulletin |
Subjects: | |
Online Access: | http://bulletin.incas.ro/files/aboulftouh_elbayoumi_madbouli_vol_7_iss_3.pdf |