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...
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| 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: | http://ir.uitm.edu.my/id/eprint/17621/1/AJ_TIAUW%20HIONG%20GO%20JME%2009.pdf http://ir.uitm.edu.my/id/eprint/17621/ https://jmeche.uitm.edu.my/ |
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