LOAD ALLEVIATION IN TILT ROTOR AIRCRAFT THROUGH ACTIVE CONTROL; MODELLING AND CONTROL CONCEPTS
Annual forum; 59th, American Helicopter Society ; 2003 ; Phoenix, AZ
01.01.2003
19 pages
Also known as FORUM 59; See also same s/m vol 59 suppl 2003 for 3 separate papers
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Load alleviation in tilt rotor aircraft through active control: Modelling and control concepts
Online Contents | 2004
|Load Alleviation for a Tilt-Rotor Aircraft in Airplane Mode
Online Contents | 2006
|Novel Concepts for Active Load Alleviation
TIBKAT | 2022
|Novel Concepts for Active Load Alleviation
AIAA | 2022
|