LQG Optimal Control for Space Launch Vehicle Thrust Vectoring
The present work proposes a thrust vector control (TVC) system for space launch vehicles, utilizing an optimal Linear-Quadratic-Gaussian (LQG) control framework. The proposed controller is synthesized by integrating a Linear-Quadratic Regulator (LQR) for optimal state feedback with a Kalman filter...
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| Autori principali: | , , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Laboratory of Signals and Systems
2026-06-01
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| Serie: | Algerian Journal of Signals and Systems |
| Soggetti: | |
| Accesso online: | https://ajss.dz/index.php/ajss/article/view/293 |
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