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A method and device for precise control of and controller design for aircrafts consisting of at least one spinning part and at least one non-spinning part is provided. The required torques for control of the spinning parts and for the non-spinning parts are continuously and individually calculated....

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	EGEBERG MELLEM, GEIR MORTEN, SANDBERG, PÅL HAGH, MUREN, PETTER, MARTON, TRYGVE FREDERIK
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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