Design of the air force research laboratory micro aerial vehicle research configuration

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 12, Issue , 2007, Pages 8086-8097

  Stewart, Kelly ^a,c   Wagener, Jeffrey ^a,c   Abate, Gregg ^a,c   Salichon, Max ^b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b OREGON STATE UNIVERSITY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERO STRUCTURAL INTERACTION; MICRO AERIAL VEHICLE (MAV); SIMULATION MODELS;

AIRCRAFT; FLIGHT DYNAMICS; FUSELAGES; MACHINE DESIGN; OPTIMIZATION; PROJECT MANAGEMENT;

RESEARCH LABORATORIES;

EID: 34347206691     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. http://www.mn.afrl.af.mil/
2. Mueller, T.J., "Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications," Progress in Astronautics and Aeronautics, vol. 195, AIAA, Reston, 2001.
3. DeLuca, A., Reeder, M., Ol, M., Freeman, J., Bautista, I., and Simonich M., "Experimental Investigation into the Aerodynamic Properties of a Flexible and Rigid Wing Micro Air Vehicle," AIAA Paper 2004-2396, June 2004.
4. Ifju, P., Jenkins, D., Ettinger, S., Lian, Y., Shyy, W., and Waszak, R.M., "Flexible-Wing-Based Micro Air Vehicles," AIAA Paper 2002-0705, Jan. 2002.
5. Carmichael, B.H. "Low Reynolds Number Airfoil Survey, Vol. 1". NASA CR 165803, November 1981.
6. Deryl Snyder, personal communication
7. Nechyba, M., and Ifju, P. "Towards Autonomous Flight of Micro Air Vehicles (MAVs): Vision-Guided Flight Stability and Control," Informational Briefing-Audience Unknown, Department of Electrical and Computer Engineering and Department of Aerospace and Mechanical Science, University of Florida, Gainesville Florida, 2002.
8. http://web.mit.edu/drela/Public/web/avl/