DocumentCode :
3122655
Title :
Kalman Filter Based State Estimation for Linearized Twin Rotor System
Author :
Haider, Khawaja Shafiq ; Kazmi, Ijaz Hussain ; Rehman, M. Inam-ur
Author_Institution :
Dept. of Electr. Eng., Wah Eng. Coll., Wah, Pakistan
fYear :
2011
fDate :
19-21 Dec. 2011
Firstpage :
179
Lastpage :
182
Abstract :
In this paper, states estimation for MIMO Twin Rotor System (TRS) is performed. In practical, often, system states are unknown or immeasurable. In applications like state feedback control design, fault diagnostics or system monitoring, the states information is needed. The precise estimation of states can be done and verified using Kalman filter as state observer. For generation and confirmation of correct states estimate, DC inputs (resembling practical inputs) are developed and outputs from TRS model are collected. The I/O data is invoked in Kalman filter and resulting states estimates are verified for correctness first by examining the state error covariance and then by comparing the evolution of actual and estimated states. The results show that the Kalman state estimates are highly precise and fast convergent to the actual states. The extracted TRS states information is usable for fault diagnostics, control design, system monitoring or as an alternate to costly instruments used to measure system states in industries.
Keywords :
Kalman filters; MIMO systems; control system synthesis; fault diagnosis; linearisation techniques; machine control; rotors; state estimation; state feedback; DC inputs; Kalman filter; MIMO Twin Rotor System; TRS model; fault diagnostics; linearized twin rotor system; state error covariance; state estimation; state feedback control design; system monitoring; Kalman filters; Noise; Observers; Radar tracking; Rotors; Estimator; Kalman Filter; Observer; State feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Frontiers of Information Technology (FIT), 2011
Conference_Location :
Islamabad
Print_ISBN :
978-1-4673-0209-8
Type :
conf
DOI :
10.1109/FIT.2011.40
Filename :
6137141
Link To Document :
بازگشت