• DocumentCode
    2077978
  • Title

    Space Relative Navigation Filter Based On-Board Radar Observation

  • Author

    Ma, Weihua ; Luo, Jianjun ; Wang, Mingming ; Yang, Bo

  • Author_Institution
    Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
  • fYear
    2009
  • fDate
    17-19 Oct. 2009
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    The absolute attitude error of chaser vehicle is always neglected in observation equation of space relative navigation filter when chaser satellite on-board radar using as the measurement sensor. But the attitude error could affect relative navigation filter precision in fact. The new observation equation, which contains the absolute attitude error of chaser vehicle, is constructed. And the plan, using equivalent measurement error as attitude error, is put forward. The simulations show that the filter precision of relative position and velocity descend when attitude error is big, and the precision is improved when attitude equivalent error is introduced to filter. The plan of attitude equivalent error is proved to be feasible.
  • Keywords
    aircraft navigation; attitude measurement; measurement errors; spaceborne radar; absolute attitude error; chaser satellite on-board; chaser vehicle; equivalent measurement error; measurement sensor; on-board radar observation; space relative navigation filter; Equations; Extraterrestrial measurements; Jacobian matrices; Laser radar; Measurement errors; Microwave filters; Radar measurements; Satellite navigation systems; Spaceborne radar; Vehicles;
  • 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.2009.5301217
  • Filename
    5301217