Simulation and flight control of a Tilt duct UAV

AIAA Modeling and Simulation Technologies Conference

Volumn , Issue , 2009, Pages

  Tekinalp, Ozan ^a,b   Unlu, Tugba ^a,b   Yavrucuk, Ilkay ^a,b  

^a MIDDLE EAST TECHNICAL UNIVERSITY   (Turkey)

^b Aerospace Engineering Department   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROLLERS; DUCTS; EQUATIONS OF MOTION; INVERSE PROBLEMS; UNMANNED AERIAL VEHICLES (UAV);

ALLOCATION ALGORITHM; FLIGHT CONTROL; FORWARD FLIGHT; INVERSE CONTROL; REDUNDANT CONTROLS; SIMULATION CODE; TRANSITION FLIGHT; TRANSITION PHASE;

FLIGHT SIMULATORS;

EID: 77958188464     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-6138     Document Type: Conference Paper

References (7)

1. Armutcuoglu, O, Kavsaoglu, M.S. and O. Tekinalp "ilt Duct Vertical Takeoff and Landing Uninhabited Aerial Vehicle Concept Design Study, " AIAA Journal of Aircraft, Vol. 41, No. 2, 2004, pp. 215-223.
2. Okan, A., Tekinalp, O., and Kavsaoglu, M., "Flight Control of a Tilt-Duct UAV, " 1st International Conference on Unmanned Aerospace Vehicles, AIAA-2002-3466, May 2002.
3. Tayfun Cimen "State-Dependent Ricatti Equation (SDRE) Control : A Survey, " The International Federation of Automatic Control, 2008, pp. 3761 - 3775.
4. Hammet, K.D., Hall, C.D., and Ridgley, D.B., "Controllability issues in Nonlinear State-Dependent Ricatti Equation Control, " Journal of Guidance Control and Dynamics, Vol. 21, No.5, 1998, pp. 767-773.
5. Coultier, J.R., Stansbery, D.T., "Nonlinear, Hybrid Bank-to-Turn/Skid-to-Turn Missile Autopilot Design, " AIAA Guidance Navigation and Control Conference, AIAA-01-5929, 2001.
6. Tekinalp, O., Yavuzoglu, E., "A New Steering Law for Redundant Control Moment Gyroscope Clusters, " Aerospace Science and Technology, V. 9, 2005, pp. 626-634.
7. Lan, C-T.E., Roskam, J., Airplane Aerodynamics and Performance, U. of Kansas, Lawrence, Kansas, 1988.