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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Bibliographic Details
Main Author: Zaludin, Zairil A.
Format: Article
Published: The Research Publication 2022
Online Access:http://psasir.upm.edu.my/id/eprint/103173/
https://armejournal.org/index.php/arme/article/view/3346
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