Aircraft pitch control tracking with sliding mode control
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 fl...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Science Publishing Corporation
2018
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| Online Access: | http://psasir.upm.edu.my/id/eprint/73070/ http://psasir.upm.edu.my/id/eprint/73070/1/PITCH.pdf |
| _version_ | 1848857234149212160 |
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| author | Mohmad Rouyan, Nurhana Varatharajoo, Renuganth Eshghi, Samira Abdullah, Ermira Junita Suzuki, Shinji |
| author_facet | Mohmad Rouyan, Nurhana Varatharajoo, Renuganth Eshghi, Samira Abdullah, Ermira Junita Suzuki, Shinji |
| author_sort | Mohmad Rouyan, Nurhana |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | 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. |
| first_indexed | 2025-11-15T11:54:18Z |
| format | Article |
| id | upm-73070 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T11:54:18Z |
| publishDate | 2018 |
| publisher | Science Publishing Corporation |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-730702021-02-28T17:45:43Z http://psasir.upm.edu.my/id/eprint/73070/ Aircraft pitch control tracking with sliding mode control Mohmad Rouyan, Nurhana Varatharajoo, Renuganth Eshghi, Samira Abdullah, Ermira Junita Suzuki, Shinji 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. Science Publishing Corporation 2018 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/73070/1/PITCH.pdf 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 https://www.sciencepubco.com/index.php/ijet/article/view/21330/10092 10.14419/ijet.v7i4.13.21330 |
| spellingShingle | Mohmad Rouyan, Nurhana Varatharajoo, Renuganth Eshghi, Samira Abdullah, Ermira Junita Suzuki, Shinji Aircraft pitch control tracking with sliding mode control |
| title | Aircraft pitch control tracking with sliding mode control |
| title_full | Aircraft pitch control tracking with sliding mode control |
| title_fullStr | Aircraft pitch control tracking with sliding mode control |
| title_full_unstemmed | Aircraft pitch control tracking with sliding mode control |
| title_short | Aircraft pitch control tracking with sliding mode control |
| title_sort | aircraft pitch control tracking with sliding mode control |
| url | http://psasir.upm.edu.my/id/eprint/73070/ http://psasir.upm.edu.my/id/eprint/73070/ http://psasir.upm.edu.my/id/eprint/73070/ http://psasir.upm.edu.my/id/eprint/73070/1/PITCH.pdf |