Roll control for a micro air vehicle using active wing morphing

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Garcia, Helen M ^a   Abdulrahim, Mujahid ^a   Lind, Rick ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOPILOT DESIGNS; CONTROL AUTHORITIES; FLIGHT SYSTEMS; FLIGHT TEST; MORPHING; ROLL MANEUVERS; URBAN ENVIRONMENTS; WING MORPHING;

MICRO AIR VEHICLE (MAV);

VEHICLES;

EID: 84896693758     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. M. Amprikidis and J.E. Cooper,.Development of Smart Spars for Active Aeroelastic Structures,. AIAA- 2003-1799, 2003.
2. J. Blondeau, J. Richeson and D.J. Pines,.Design, Development and Testing of a Morphing Aspect Ratio Wing using an Infiatable Telescopic Spar,. AIAA-2003- 1718.
3. J. Bowman, B. Sanders and T. Weisshar,.Evaluating the Impact of Morphing Technologies on Aircraft Performance,. AIAA-2002-1631, 2002.
4. D. Cadogan, T. Smith, R. Lee and S. Scarborough,.Infiatable and Rigidizable Wing Components for Unmanned Aerial Vehicles,. AIAA-2003-1801, 2003.
5. C.E.S. Cesnik and E.L. Brown,.Active Warping Control of a Joined-Wing Airplane Configuration,. AIAA-2003-1716, 2003.
6. J.B. Davidson, P. Chwalowski and B.S. Lazos,.Flight Dynamic Simulation Assessment of a Morphable Hyper-Elliptic Cambered SpanWinged Configuration,. AIAA-2003-5301, 2002.
7. S.M. Ettinger, M.C. Nechyba, P.G. Ifju and M. Waszak,.Vision-Guided Flight Stability and Control for Micro Air Vehicles,. IEEE International Conference on Intelligent Robots and Systems, October 2002, pp. 2134-2140.
8. J.M. Grasmeyer and M.T. Keennon,.Development of the Black Widow Micro Air Vehicle,. AIAA- 2001-0127, 2001.
9. P.G. Ifju, D.A. Jenkins, S. Ettinger, Y. Lian, W. Shyy and M.R. Waszak,.Flexible-Wing-Based Micro Air Vehicles,. AIAA-2002-0705.
10. C.O. Johnston, D.A. Neal, L.D. Wiggins, H.H. Robertshaw, W.H. Mason and D.J. Inman,.A Model to Compare the Flight Control Energy Requirements of Morphing and Conventionally ActuatedWings,. AIAA- 2003-1716, 2003.
11. L. Ljung, System Identification, Prentice Hall, Englewood Cliffs, NJ, 1987.
12. P. de Marmier and N. Wereley,.MorphingWings of a Small Scale UAV Using Infiatable Actuators for Sweep Control,. AIAA-2003-1802.
13. E.W. Pendleton, D. Bessette, P.B. Field, G.D. Miller and K.E. Griffin,.Active AeroelasticWing Flight Research Program: Technical Program and Model Analytical Development,. Journal of Aircraft, Vol. 37, No. 4, 2000, pp. 554-561.
14. B. Sanders, F.E. Eastep and E. Forster,.Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control Surfaces for Morphing Aircraft,. Journal of Aircraft, Vol. 40, No. 1, January-February 2003, pp. 94-99.
15. D. Viieru, Y. Lian, W. Shyy and P. Ifju,.Investigation of Tip Vortex on Aerodynamic Performance of a Micro Air Vehicle,. AIAA-2003-3597, 2003.
16. M.R. Waszak, L.N. Jenkins and P. Ifju,.Stability and Control Properties of an Aeroelastic FixedWing Micro Aerial Vehicle,. AIAA-2001-4005.
17. M.R. Waszak, J.B. Davidson, and P.G. Ifju,.Simulation and Flight Control of an Aeroelastic FixedWing Micro Aerial Vehicle,. AIAA-2002-4875
18. R.W. Wlezien, G.C. Horner, A.R. McGowan, S.L. Padula, M.A. Scott, R.J. Silcox and J.O. Simpson,.The Aircraft Morphing Program,. AIAA-98-1927.