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 :
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