First steps towards the design of an active pitch link loads reduction system using novel control techniques

31st European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages

  Voskuijl, Mark ^a   Manimala, B ^a   Walker, D J ^a   Kureemun, R ^a  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL EQUIPMENT; FLIGHT DYNAMICS; MANEUVERABILITY; SPEED CONTROL; STRUCTURAL LOADS;

DYNAMIC STALL COMPONENT; HIGH-SPEED FLIGHT; LONGITUDINAL MANOEUVRES; ROTORCRAFTS;

ROTORS;

EID: 33746640496     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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