Flight control of a tilt-duct VTOL UAV

1st UAV Conference

Volumn , Issue , 2002, Pages

  Okan, A ^a,b   Tekinalp, O ^b   Kavsaoglu M S ^b  

^a ROKETSAN Missiles Industries Inc   (Turkey)

^b MIDDLE EAST TECHNICAL UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATIC FLIGHT CONTROL SYSTEMS; CONTROL METHODS; FLIGHT CONDITIONS; FLIGHT CONTROL; FLIGHT MECHANICS; FLIGHT PHASIS; TRANSITION FLIGHT; TRIMMED FLIGHT;

FLIGHT CONTROL SYSTEMS;

DUCTS;

EID: 84896693668     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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3. th Bristol International Conference, pp. 28.1-28.11, 2000.
4. Kavsaoglu, M. Ş., Tekinalp, O., Tulunay, E., Okan, A., Armutcuoglu, Ö. "Design, Flight Mechanics and Control of a VTOL UAV", NATO RTA Applied Vehicle Technology(AVT) Symposium on Unmanned Vehicles(UV) for Aerial, Ground and Naval Military Operations, 9-13 October 2000, Ankara, Turkey.
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16. Okan, A., Modeling and Control of a Tilt-Duct VTOL UAV, M.S. Thesis, Department of Aerospace Engineering, Middle East Technical University, Ankara, Turkey, 2000.