z-logo
open-access-imgOpen Access
Aircraft parameter identification for application within a fault-tolerant flight control system
Author(s) -
Kerri Phillips
Publication year - 2011
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.33915/etd.3049
Subject(s) - flight control surfaces , stability derivatives , actuator , control theory (sociology) , engineering , aerodynamics , control engineering , mathematical model , system identification , control system , flight dynamics , computer science , aerospace engineering , data modeling , control (management) , artificial intelligence , electrical engineering , software engineering , physics , quantum mechanics

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom