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Aircraft pitch control tracking with sliding mode control


Citation

Mohmad Rouyan, Nurhana and Varatharajoo, Renuganth and Eshghi, Samira and Abdullah, Ermira Junita and Suzuki, Shinji (2018) Aircraft pitch control tracking with sliding mode control. International Journal of Engineering and Technology(UAE), 7 (4.13). 62 - 65. ISSN 2227-524X

Abstract

Sliding mode control (SMC) is one of the robust and nonlinear control methods. An aircraft flying at high angles of attack is considered nonlinear due to flow separations, which cause aerodynamic characteristics in the region to be nonlinear. This paper presents the comparative assessment for the flight control based on linear SMC and integral SMC implemented on the nonlinear longitudinal model of a fighter aircraft. The controller objective is to track the pitch angle and the pitch rate throughout the high angles of attack envelope. Numerical treatments are carried out on selected conditions and the controller performances are studied based on their transient responses. Obtained results show that both SMCs are applicable for high angles of attack.


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Additional Metadata

Item Type: Article
Divisions: Faculty of Engineering
DOI Number: https://doi.org/10.14419/ijet.v7i4.13.21330
Publisher: Science Publishing Corporation
Keywords: F18-HARV; Pitch control; Sliding mode control
Depositing User: Ms. Nuraida Ibrahim
Date Deposited: 28 Feb 2021 17:45
Last Modified: 28 Feb 2021 17:45
Altmetrics: http://www.altmetric.com/details.php?domain=psasir.upm.edu.my&doi=10.14419/ijet.v7i4.13.21330
URI: http://psasir.upm.edu.my/id/eprint/73070
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