Previous attempts to identify aircraft stability and control derivatives from flight test data, suffer from the disadvantage that the coupling between the longitudinal and lateral-directional dynamics has been ignored. Hierarchical system identification theory is used to reduce the computational effort involvec. Computational considerations and comparison with the unhierarchically structured problem are presented.
Identification of aircraft stability and control parameters using hierarchical state estimation
Die Bestimmung von Flugzeugstabilitaet und Regelungsgroessen mittels hierarchischer Zustandsabschaetzung
IEEE Transactions on Aerospace and Electronic Systems ; 10 , 2 ; 255-273
1974
19 Seiten, 6 Bilder, 3 Tabellen, 18 Quellen
Aufsatz (Zeitschrift)
Englisch