Fault Tolerant Control Design for the Longitudinal Aircraft Dynamics using Quantitative Feedback Theory
AIAA Guidance, Navigation, and Control Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Robust Longitudinal Control Design Using Dynamic Inversion and Quantitative Feedback Theory
Online Contents | 1997
|Fault-Tolerant Design of Feedback Control Systems
British Library Online Contents | 1996
|Design issues for fault tolerant-restructurable aircraft control
Tema Archiv | 1985
|