DocumentCode :
3334146
Title :
Receding horizon FIR filter with estimated horizon initial state and its application to aircraft engine systems
Author :
Han, Soo Hee ; Kim, Pyung Soo ; Kwon, Wook Hyun
Author_Institution :
Sch. of Electr. Eng., Seoul Nat. Univ., South Korea
Volume :
1
fYear :
1999
fDate :
1999
Firstpage :
33
Abstract :
Proposes a version of the discrete-time receding horizon FIR filter (RHFF) using the estimated horizon initial state. The estimated horizon initial state is obtained from the best linear unbiased estimator (BLUE) scheme. The proposed RHFF for the current state can be represented in either an iterative form or a batch form. The proposed RHFF is always time-invariant and has unbiasedness and remarkable deadbeat properties. The proposed RHFF is shown to be equivalent to the existing RHFF with unknown horizon initial state. For the validity of the proposed RHFF, the problem of a third-order dynamic model of an F-404 aircraft engine system is considered via simulation studies
Keywords :
FIR filters; Riccati equations; aerospace engines; discrete time systems; matrix algebra; state estimation; F-404 aircraft engine system; best linear unbiased estimator; deadbeat properties; discrete-time receding horizon FIR filter; estimated horizon initial state; unbiasedness; Aircraft propulsion; Control systems; Engines; Feedback control; Filtering algorithms; Finite impulse response filter; H infinity control; IIR filters; Kalman filters; State estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location :
Kohala Coast, HI
Print_ISBN :
0-7803-5446-X
Type :
conf
DOI :
10.1109/CCA.1999.806139
Filename :
806139
Link To Document :
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