DocumentCode
2003293
Title
Hovering Controller Design for a Helicopter
Author
Jiao, Yusong ; Li, Yan ; Yu, Xiang ; Wang, Xinmin
Author_Institution
Northwestern Polytech. Univ., Xi´´an
fYear
2007
fDate
May 30 2007-June 1 2007
Firstpage
1028
Lastpage
1031
Abstract
This paper studies the hovering controller design for a helicopter. The linear helicopter motion equation is introduced. The hovering control law is designed and the parameters mapping method is employed to search the best available hover controller parameters in all flight states. The digital simulation models are established. Simulation results are given to demonstrate the effectiveness of the designed controllers. The hover maneuver controlled by the designed controller passed the test flight.
Keywords
aircraft control; control system synthesis; helicopters; hovercraft; motion control; digital simulation models; flight testing; hovering controller design; linear helicopter motion equation; Aerospace control; Automatic control; Control systems; Design automation; Digital simulation; Equations; Helicopters; Testing; Unmanned aerial vehicles; Velocity control; flight tests; helicopter; hover controller; parameter mapping method;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2007. ICCA 2007. IEEE International Conference on
Conference_Location
Guangzhou
Print_ISBN
978-1-4244-0818-4
Electronic_ISBN
978-1-4244-0818-4
Type
conf
DOI
10.1109/ICCA.2007.4376512
Filename
4376512
Link To Document