DocumentCode
575180
Title
Experiment of height and attitude control using monorotor unmanned aerial vehicle
Author
Fujita, Shohei ; Sekiguchi, Kazuma ; Sampei, Mitsuji
Author_Institution
Dept. of Mech. & Control Syst. Eng., Tokyo Inst. of Technol., Tokyo, Japan
fYear
2012
fDate
20-23 Aug. 2012
Firstpage
1986
Lastpage
1990
Abstract
This paper shows the usefulness of the nonlinear controller realizing periodic motion of monorotor UAV by experiments. Monorotor UAV has no equilibrium point. So, the control target is semi-hovering; a motion that passes desired non-equilibrium point at which height and attitude stop periodically. In order to achieve this control objective, we propose discontinuous and time-varying output zeroing controller which allows zero dynamics to be controlled. The numerical simulation and experiments show the validity of suggesting controller design method.
Keywords
attitude control; autonomous aerial vehicles; nonlinear control systems; numerical analysis; time-varying systems; vehicle dynamics; attitude control; control objective; controller design method; discontinuous output zeroing controller; height control; monorotor UAV; monorotor unmanned aerial vehicle; non-equilibrium point; nonlinear controller; numerical simulation; periodic motion; time-varying output zeroing controller; Aerodynamics; Attitude control; Nonlinear dynamical systems; Propulsion; Robots; Trajectory; Nonlinear Control; Periodic Motion; UAV; Underactuated System; Zero Dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference (SICE), 2012 Proceedings of
Conference_Location
Akita
ISSN
pending
Print_ISBN
978-1-4673-2259-1
Type
conf
Filename
6318338
Link To Document