"The ultimate goals of this study were to use experimental data to estimate the flight capabilities of a flapping wing nano aerial vehicle (NAV), estimate the power required to provide such flight, and develop a controller approach for future use in the design of this aircraft. The experimental data is a collection of measurements of the normal force on a flapping wing taken in stationary water, and was used to develop empirical coefficient derivatives for use in the dynamic modeling of the NAV"--Abstract, page iii.
Landers, Robert G.
McAdams, Daniel A.
Isaac, Kakkattukuzhy M.
Mechanical and Aerospace Engineering
M.S. in Mechanical Engineering
United States. Defense Advanced Research Projects Agency
University of Missouri--Rolla
xiii, 85 pages
© 2007 Wyatt Emery Davenport, All rights reserved.
Thesis - Open Access
Library of Congress Subject Headings
Airplanes -- Wings
Guidance systems (Flight)
Print OCLC #
Electronic OCLC #
Link to Catalog Recordhttp://laurel.lso.missouri.edu/record=b6400644~S5
Davenport, Wyatt Emery, "Development, modeling, and simulation of a nano aerial vehicle using empirical data" (2007). Masters Theses. 4582.