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Conception d'un contrôleur linéaire robuste pour le contrôle d'attitude d'une fusée

Conception d'un contrôleur linéaire robuste pour le contrôle d'attitude d'une fusée

          
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About the Book

Le contrôle de l'attitude de la fusée est un grand défi en temps réel. Pour rendre la fusée stable face aux influences, ce livre a examiné les technologies de contrôle telles que le contrôle proportionnel intégral dérivé utilisant un mécanisme anti-enroulement et la théorie du régulateur linéaire quadratique basée sur le modèle mathématique du degré de liberté. Le comportement transitoire des deux contrôleurs n'est pas régulier et prend plus de temps à se stabiliser à l'endroit défini . Lerégulateur proportionnel intégral dérivé est combiné à un régulateur à logique floue pour surmonter les défauts du PID et du LQR. En conclusion, cet ouvrage compare l'analyse des performances des contrôleurs PID flous avec les régulateurs quadratiques linéaires et les contrôleurs à dérivée intégrale proportionnelle. Les résultats de la simulation indiquent que le contrôleur hybride Fuzzy-PID présente une amélioration remarquable en termes de dépassement et de temps de stabilisation, tout en réduisant l'erreur en régime permanent. Le contrôleur hybride Fuzzy-PID proposé élimine complètement le dépassement et produit une stabilité énorme pour le moteur dela fusée .


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Product Details
  • ISBN-13: 9786207182381
  • Publisher: KS Omniscriptum Publishing
  • Publisher Imprint: Editions Notre Savoir
  • Height: 229 mm
  • No of Pages: 164
  • Spine Width: 10 mm
  • Width: 152 mm
  • ISBN-10: 6207182383
  • Publisher Date: 20 Feb 2024
  • Binding: Paperback
  • Language: French
  • Returnable: N
  • Weight: 249 gr


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Conception d'un contrôleur linéaire robuste pour le contrôle d'attitude d'une fusée
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