DocumentCode
2075059
Title
Improvement of Homing Missile Guidance Performance Using Fuzzy Adaptive IMM Radome Slope Estimation
Author
Cao, Xiaorui ; Dong, Caoyang ; Wang, Qing ; Chen, Yu
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2009
fDate
17-19 Oct. 2009
Firstpage
1
Lastpage
5
Abstract
For homing missile guidance system, a radome compensation method using fuzzy adaptive interacting multiple mode (FAIMM) algorithm for estimating both the radome slope and guidance information is proposed to reduce the influence induced by radome and enhance system performance. The new filtering algorithm includes two levels fuzzy inference systems based on the standard interacting multiple mode (IMM). In the first level the filtering measurement innovations and innovation error covariance are used as the inputs of fuzzy inference to take out the matched degrees for each sub-filter model which are computed intricately in the standard IMM. The radome slope model is adaptively adjusted to reduce the error of estimation using the second level fuzzy inference. Simulation results indicate that FAIMM can estimate the radome slope availably and improve the guidance system performance. Compared with IMM algorithm, the new aglorithm can get more accurate results with the same amount of sub-models.
Keywords
adaptive systems; fuzzy reasoning; missile guidance; fuzzy adaptive IMM radome slope estimation; guidance information; homing missile guidance; interacting multiple mode; Adaptive control; Estimation error; Filtering algorithms; Fuzzy systems; Inference algorithms; Matched filters; Measurement standards; Missiles; System performance; Technological innovation;
fLanguage
English
Publisher
ieee
Conference_Titel
Image and Signal Processing, 2009. CISP '09. 2nd International Congress on
Conference_Location
Tianjin
Print_ISBN
978-1-4244-4129-7
Electronic_ISBN
978-1-4244-4131-0
Type
conf
DOI
10.1109/CISP.2009.5301115
Filename
5301115
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