A robust adaptive control system for high performance aircraft / Tiauw Hiong Go
The design of a longitudinal controller to enhance the maneuverability of a high performance aircraft is described. Since such aircraft is often required to fly outside the linear aerodynamic regimes, the design is based on the nonlinear equations of motion. The controller is of adaptive type and it...
| Format: | Article |
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| Language: | English |
| Published: |
Faculty of Mechanical Engineering and University Publication Centre (UPENA)
2009
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| Online Access: | https://ir.uitm.edu.my/id/eprint/17621/ |
| _version_ | 1848804315865546752 |
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| building | UiTM Institutional Repository |
| collection | Online Access |
| description | The design of a longitudinal controller to enhance the maneuverability of a high performance aircraft is described. Since such aircraft is often required to fly outside the linear aerodynamic regimes, the design is based on the nonlinear equations of motion. The controller is of adaptive type and it is robust with respect to unknown, but bounded uncertainties. The performance of the resulting controller is evaluated through simulations using hypothetical fighter aircraft parameters. The controller is demonstrated to be able to obtain good and consistent performances over a wide range of flight conditions. |
| first_indexed | 2025-11-14T21:53:12Z |
| format | Article |
| id | uitm-17621 |
| institution | Universiti Teknologi MARA |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T21:53:12Z |
| publishDate | 2009 |
| publisher | Faculty of Mechanical Engineering and University Publication Centre (UPENA) |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | uitm-176212017-08-17T03:37:20Z https://ir.uitm.edu.my/id/eprint/17621/ A robust adaptive control system for high performance aircraft / Tiauw Hiong Go jmeche The design of a longitudinal controller to enhance the maneuverability of a high performance aircraft is described. Since such aircraft is often required to fly outside the linear aerodynamic regimes, the design is based on the nonlinear equations of motion. The controller is of adaptive type and it is robust with respect to unknown, but bounded uncertainties. The performance of the resulting controller is evaluated through simulations using hypothetical fighter aircraft parameters. The controller is demonstrated to be able to obtain good and consistent performances over a wide range of flight conditions. Faculty of Mechanical Engineering and University Publication Centre (UPENA) 2009 Article PeerReviewed text en https://ir.uitm.edu.my/id/eprint/17621/1/AJ_TIAUW%20HIONG%20GO%20JME%2009.pdf UNSPECIFIED (2009) A robust adaptive control system for high performance aircraft / Tiauw Hiong Go. (2009) Journal of Mechanical Engineering (JMechE) <https://ir.uitm.edu.my/view/publication/Journal_of_Mechanical_Engineering_=28JMechE=29.html>, 6 (1). pp. 67-84. ISSN 1823-5514 ; 2550-164X https://jmeche.uitm.edu.my/ |
| spellingShingle | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title_full | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title_fullStr | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title_full_unstemmed | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title_short | A robust adaptive control system for high performance aircraft / Tiauw Hiong Go |
| title_sort | robust adaptive control system for high performance aircraft / tiauw hiong go |
| url | https://ir.uitm.edu.my/id/eprint/17621/ https://ir.uitm.edu.my/id/eprint/17621/ |