DocumentCode :
3396199
Title :
Attitude control for unmanned helicopter using h-infinity loop-shaping method
Author :
Mingyun Lv ; Yanpeng Hu ; Peng Liu
Author_Institution :
Sch. of Aeronaut. Sci. & Technol., Beihang Univ., Beijing, China
fYear :
2011
fDate :
19-22 Aug. 2011
Firstpage :
1746
Lastpage :
1749
Abstract :
The aim of this paper is to design an attitude controller of an unmanned helicopter using h-infinity and loop-shaping methods. A pre-compensator and a post-compensator are selected to modify the singular values of the normal system to get a desired loop shape. The h-infinity feedback controller is synthesized and the stability margin is calculated. The simulation results show that the attitude controller designed with robust performance has a good response performance, and h-infinity and loop-shaping methods can make unmanned helicopter have an excellent decoupling and dynamic performance.
Keywords :
H control; aerospace robotics; aircraft control; attitude control; compensation; control system synthesis; feedback; helicopters; mobile robots; remotely operated vehicles; stability; attitude controller design; h-infinity feedback controller synthesis; h-infinity loop-shaping method; post-compensator; precompensator; stability margin; unmanned helicopter; Attitude control; Control systems; H infinity control; Helicopters; Robustness; Shape; Stability analysis; controller; h-infinity; loop-shaping; simulation; unmanned helicopter;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
Conference_Location :
Jilin
Print_ISBN :
978-1-61284-719-1
Type :
conf
DOI :
10.1109/MEC.2011.6025819
Filename :
6025819
Link To Document :
بازگشت