DocumentCode
1617849
Title
Ornithopter modeling for flight simulation
Author
Han, Jae-Hung ; Lee, Jin-Young ; Kim, Dae-kwan
Author_Institution
Dept. of Aerosp. Eng., KAIST, Daejeon
fYear
2008
Firstpage
1773
Lastpage
1777
Abstract
This paper presents the flight simulation of flapping-wing air vehicles (ornithopters) based on a refined flapping-wing aerodynamic model; the modified strip theory (MST). Compared with conventional types of micro air vehicles (MAVs), flapping MAVs show more complicated flight behaviors due to their complex wing motions and aerodynamics. In this paper, a flight dynamic model of an ornithopter is presented to analyze its stability and controllability. This paper focuses on the stabilization and path-following control of the ornithopter by adjusting the flapping frequency and tail-wingpsilas elevation angle. In spite of its nonlinear and complex behavior, controlling the tail-wing pitch angle can be effective for the stabilization in longitudinal motion of the ornithopter.
Keywords
aerodynamics; aerospace control; aerospace simulation; controllability; motion control; remotely operated vehicles; stability; complex wing motions; controllability; flapping-wing air vehicles; flight simulation; microair vehicles; modified strip theory; ornithopter modeling; refined flapping-wing aerodynamic model; stability analysis; Aerodynamics; Aerospace engineering; Aerospace simulation; Control system synthesis; Electronic mail; Force control; Frequency; Strips; Unmanned aerial vehicles; Vehicle dynamics; bio-inspired; flapping-wing aerodynamic model; flight simulation; ornithopters; wing flexibility;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation and Systems, 2008. ICCAS 2008. International Conference on
Conference_Location
Seoul
Print_ISBN
978-89-950038-9-3
Electronic_ISBN
978-89-93215-01-4
Type
conf
DOI
10.1109/ICCAS.2008.4694517
Filename
4694517
Link To Document