DocumentCode
233814
Title
Research on Line-of-Sight rate extraction of strapdown seeker
Author
Wang Pei ; Zhang Ke
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
fYear
2014
fDate
28-30 July 2014
Firstpage
859
Lastpage
863
Abstract
The strapdown guidance technology, which can improve the system reliability and reduce cost efficiently, has been paid great attention and developed quickly. However, the detecting information of strapdown seeker can´t be used to proportional navigation directly because it is coupled with missile attitude, so the method of Line-of-Sight (LOS) rate extraction for strapdown seeker is investigated. Background noise and any inaccurate metrical information would be reflected to the extraction result, thus a LOS rate extraction method based on nonlinear Tracking-Differentiator(TD) and unscented Kalman filter (UKF) was proposed to obtain more precise guidance information. At the last, Monte Carlo simulations are performed; the results verify the performance and effectiveness of the designed method.
Keywords
Kalman filters; Monte Carlo methods; missile guidance; nonlinear filters; LOS; Monte Carlo simulations; TD; UKF; background noise; cost reduction; line-of-sight rate extraction method; metrical information; missile attitude; nonlinear tracking-differentiator; precise guidance information; proportional navigation; strapdown guidance technology; strapdown seeker; system reliability; unscented Kalman filter; Equations; Kalman filters; Mathematical model; Missiles; Noise; Noise measurement; Vectors; LOS rate extraction; Nonlinear Tracking-Differentiator; Strapdown Seeker; Unscented Kalman Filter;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896740
Filename
6896740
Link To Document