• DocumentCode
    1794901
  • Title

    A rapid endgame performance analysis method for exoatmosphere interceptor based on CADET

  • Author

    TaoTao Zhang ; CongYing Li ; Zhiyong Yang

  • Author_Institution
    7th Dept., Naval Astronaut. & Aeronaut. Univ., Yantai, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    558
  • Lastpage
    563
  • Abstract
    The relative equations between interceptor and target are conducted in rotation coordinate of Line of Sight. An error propagate model of LOS rate is established which is based on CADET (Covariance Analysis Describing Function Technique). This model takes several factors into consideration, such as estimate error of LOS rate, acceleration saturation of interceptor, sampling rate. A set of analytical solution is acquired. The uncertainty of Zero Effort Miss distance can be got conveniently according to the variety of LOS rotate rate. Finally, a contrast simulation with Mont-Carlo is taken to demonstrate the preciseness and efficiency of the method proposed in this paper.
  • Keywords
    Monte Carlo methods; aerospace instrumentation; covariance analysis; CADET; LOS rate; Monte Carlo method; covariance analysis describing function technique; error propagate model; exoatmosphere interceptor; rapid endgame performance analysis method; zero effort miss distance uncertainty; Acceleration; Analytical models; Covariance matrices; Equations; Mathematical model; Uncertainty; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007283
  • Filename
    7007283