DocumentCode
1752483
Title
Design of the Coordinated Turning Control for a Helicopter Digital Autopilot
Author
Yu, Xiang ; Wang, Xinmin ; Li, Yan
Author_Institution
Sch. of Autom., Northwestern Polytech. Univ., Xi´´an
Volume
1
fYear
0
fDate
0-0 0
Firstpage
564
Lastpage
568
Abstract
The sideslip problem during the coordinated turning of a helicopter is studied in this paper. An improved control law for the helicopter digital autopilot is presented. Compared with the existing control law, this control law reduced the sideslip much. Simulation and test flight results are given to show that the sideslip is controlled within the required range
Keywords
aircraft control; helicopters; motion control; control law; coordinated turning control; helicopter digital autopilot; sideslip problem; Aerospace simulation; Automatic control; Automation; Helicopters; Intelligent control; Testing; Turning; digital autopilot; helicopter; sideslip; the Coordinated Turning;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location
Dalian
Print_ISBN
1-4244-0332-4
Type
conf
DOI
10.1109/WCICA.2006.1712403
Filename
1712403
Link To Document