DocumentCode :
3173627
Title :
MIMO High Gain Trajectory Linearization Observer Design and Hardware-in-the-loop Test
Author :
Huang, Rui ; Zhu, J. Jim
Author_Institution :
Ohio Univ., Athens
fYear :
2007
fDate :
9-13 July 2007
Firstpage :
248
Lastpage :
253
Abstract :
In this paper, we extend the previous TLO results for SISO trajecotory linearization observer (TLO) to MIMO nonlinear dynamic systems. Regular perturbation and nonlinear high-gain observer theories are applied to analyze the stability and robustness of the TLO method. The high-gain observer theory has been extended from time-invariant cases to time-varying cases using a singular perturbation approach. The high-gain TLO design method is applied to the attitude tracking controller for Quanser UFO, which is a real-time nonlinear control test bed. Both computer simulation and hardware-in- the-loop (HIL) experimental results are presented to show the effectiveness of TLO method.
Keywords :
MIMO systems; attitude control; control system synthesis; nonlinear control systems; nonlinear dynamical systems; observers; perturbation techniques; time-varying systems; MIMO high gain trajectory linearization observer design; MIMO nonlinear dynamic systems; Quanser UFO; SISO trajecotory linearization observer; attitude tracking controller; computer simulation; hardware-in- the-loop; hardware-in-the-loop test; high-gain observer theory; nonlinear high-gain observer; real-time nonlinear control test bed; singular perturbation; stability; time-invariant cases; time-varying cases; Attitude control; Computer simulation; Control systems; Design methodology; Linear feedback control systems; MIMO; Nonlinear control systems; Robust stability; Stability analysis; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2007. ACC '07
Conference_Location :
New York, NY
ISSN :
0743-1619
Print_ISBN :
1-4244-0988-8
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2007.4282978
Filename :
4282978
Link To Document :
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