DocumentCode
3541581
Title
Radome slope estimation in flight using fuzzy adaptive multiple model for active homing missile
Author
Cao, Xiaorui ; Dong, Chaoyang ; Wang, Qing ; Chen, Yu
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear
2009
fDate
16-19 Aug. 2009
Abstract
For homing missile guidance system in three dimensional engagement scenarios, a new filter structure using fuzzy adaptive multiple model (FAMM) algorithm, based on extended Kalman filter (EKF), for estimating both the radome slope and guidance information is proposed to reduce the influence induced by radome and enhance the system performance. The radome slopes are modeled as a series of possible configurations which the multiple model algorithm is used to get the model match degree based on. The new filtering algorithm includes a fuzzy inference system which adjusted the radome slope model on line to reduce the error of estimation. Simulation results indicate that the proposed filter structure can estimate the radome slope availably and improve the guidance system performance.
Keywords
Kalman filters; aerospace simulation; filtering theory; fuzzy set theory; inference mechanisms; missile guidance; radomes; active homing missile; extended Kalman filter; filtering algorithm; flight model; fuzzy adaptive multiple model; fuzzy inference system; missile guidance system; radome slope estimation; Adaptive control; Adaptive filters; Estimation error; Filtering algorithms; Fuzzy systems; Inference algorithms; Information filtering; Information filters; Missiles; System performance; extended Kalman filter; fuzzy inference; multiple model; radome estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4244-3863-1
Electronic_ISBN
978-1-4244-3864-8
Type
conf
DOI
10.1109/ICEMI.2009.5274149
Filename
5274149
Link To Document