Transition flight control of the quad-tilting rotor convertible MAV

2013 International Conference on Unmanned Aircraft Systems, ICUAS 2013 - Conference Proceedings

Volumn , Issue , 2013, Pages 789-794

  Flores, Gerardo ^a   Lozano, R ^b  

^a UNIVERSITÉ DE TECHNOLOGIE DE COMPIÈGNE   (France)

^b UNIVERSITÉ DE TECHNOLOGIE DE COMPIÈGNE   (France)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL LAWS; FLIGHT CONFIGURATIONS; LYAPUNOV DESIGN; NON LINEAR CONTROL; NUMERICAL RESULTS; TRANSITION FLIGHT; TRANSITION STAGE;

CONTROL THEORY; FIXED WINGS;

AIRCRAFT;

EID: 84883099427     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICUAS.2013.6564761     Document Type: Conference Paper

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