DocumentCode :
2673253
Title :
Robust control arithmetic with limitation of system input energy for attitude system of subminiature unmanned helicopter
Author :
Cao, Lianmin ; Xiao, Xingyuan ; Zeng, Qingliang ; Zhang, Xin
Author_Institution :
Shan Dong Univ. of Sci. & Technol., Qing Dao, China
Volume :
5
fYear :
2010
fDate :
27-29 March 2010
Firstpage :
660
Lastpage :
664
Abstract :
A new robust control arithmetic is put forward to deal with the uncertain attitude model of small unmanned helicopter (SUH). Firstly, the attitude matrix model of SUH is denoted by the block diagonally radioactive matrix. Secondly, based on the restriction of the closed-loop pole and variance constraints, a new robust control, which has the characteristic of system input energy limited, is put forward. Furthermore, the worst system instance of the robust control is analyzed. Finally, simulation proves that the robust control arithmetic has the good performance at the worst condition. In other words, the robust control arithmetic preferably resolves the attitude control of SUH.
Keywords :
attitude control; closed loop systems; helicopters; remotely operated vehicles; robust control; attitude matrix model; attitude system; block diagonally radioactive matrix; closed loop pole; robust control arithmetic; subminiature unmanned helicopter; system input energy; variance constraints; Aerospace electronics; Arithmetic; Attitude control; Control system analysis; Control systems; Helicopters; Mathematical model; Nonlinear dynamical systems; Robust control; Uncertain systems; closed-loop pole; robust control; small unmanned helicopter; system input energy limited; variance constraints;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Computer Control (ICACC), 2010 2nd International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4244-5845-5
Type :
conf
DOI :
10.1109/ICACC.2010.5486787
Filename :
5486787
Link To Document :
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