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...

Description complète

Enregistré dans:
Détails bibliographiques
Format: Livre
Publié: Faculty of Mechanical Engineering and University Publication Centre (UPENA), 2009.
Sujets:
Accès en ligne:Link Metadata
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!

Documents similaires