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Volume 38 Issue 3
Mar.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (3): 319-323.
Song Yuanyun, Chen Wanchun. High-accuracy quick-reaching sliding mode variable structure terminal guidance law[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 319-323. (in Chinese)
Citation: Song Yuanyun, Chen Wanchun. High-accuracy quick-reaching sliding mode variable structure terminal guidance law[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 319-323. (in Chinese)
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High-accuracy quick-reaching sliding mode variable structure terminal guidance law

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 Oct 2011
  • Publish Date: 30 Mar 2012
    Abstract
  • A variable structure terminal guidance law with adaptive quick-reaching law and a filter approach based on sliding mode observer was developed for short time interception. During the ideal and non-ideal condition with typical target maneuvers, the simulation results demonstrates the higher accuracy, better robustness and easy realized of the designed guidance law by comparing with the conventional proportional navigation, augmented proportional navigation and switched bias proportional navigation. Also the filter approach is shown to be more effective than the extended Kalman filter (EKF) for the colored noise.

     

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    • References(6)
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