DocumentCode
566064
Title
Design of augmentation stability control system for hovering of ducted propeller air vehicle
Author
Li, Mingxi ; Xiang, Changle ; Yue, Ma ; Zhu, Lijun ; Xu, Bin
Author_Institution
School of Mechanical Engineering, BeiJing Institute of Technology, 100081, China
fYear
2012
fDate
24-26 June 2012
Firstpage
873
Lastpage
877
Abstract
The aerodynamic dynamic model of hovering for air vehicle with longitudinal double ducted propeller is established by analysis aerodynamic characteristics, Relative gain array of various channels is calculated to evaluate the coupling degree among various channels, Decoupling control matrix and stability augmentation control system is designed. The empirical data on scaled model shows that air vehicle could hover stably and be in good agreement with the design goal.
Keywords
Air Vehicle; Decoupling Control; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on
Conference_Location
Wuhan, Hubei, China
Print_ISBN
978-1-4673-1524-1
Type
conf
Filename
6260246
Link To Document