• 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