Sensor and process noises reduction using a Luenberger state estimator with a stability augmentation system for a Hypersonic Transport Aircraft
This paper firstly, presents an autopilot strategy for a Hypersonic Transport Aircraft (HST) using a Stability Augmentation System (SAS) with a Luenberger estimator. The SAS is designed using Linear Quadratic Regulator (LQR) theory which, for HST, benefits the guaranteed robust dynamic stability pro...
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Main Author: | Zaludin, Zairil A. |
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Format: | Article |
Published: |
The Research Publication
2022
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Online Access: | http://psasir.upm.edu.my/id/eprint/103173/ https://armejournal.org/index.php/arme/article/view/3346 |
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