• DocumentCode
    3032646
  • Title

    Maneuver target interception based on multiple model adaptive estimator

  • Author

    Hua, Wen-hua ; Chen, Xing-lin ; Wu, Zhi-peng

  • Author_Institution
    Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    185
  • Lastpage
    190
  • Abstract
    A maneuver target interception algorithm based on multiple model adaptive estimator (MMAE) is researched and a modified differential game guidance law is given. The efficiency of this simplified MMAE algorithm lies mainly in the exploitation of the special structure of the evader maneuver command hypothesis space to reduce the number of MMAE elemental filters running in parallel and to realize the reduction of the computational load. To realize the reduction of the miss distance resulting from the estimation delay, the modified differential game guidance law increases the lateral acceleration command for small values of time-to-go of the pursuer to the maximum available value by enhancing the gain of the command. The Monte Carlo simulations are carried out for the homing performance comparison and the results demonstrate the superiority and effective of the proposed methods.
  • Keywords
    Monte Carlo methods; adaptive Kalman filters; adaptive estimation; target tracking; MMAE; Monte Carlo simulations; elemental filters; estimation delay; evader maneuver command hypothesis space; maneuver target interception; modified differential game guidance law; multiple model adaptive estimator; Acceleration; Estimation; Filtering theory; Games; Mathematical model; Noise; Switches;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5632563
  • Filename
    5632563