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Volume 39 Issue 11
Nov.  2013
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Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(11): 1503-1508.
Zhang Yachong, Yue Yazhou, Liu Yushuang, et al. Design of integrated navigation system simulation platform based on RT-LAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1503-1508. (in Chinese)
Citation: Zhang Yachong, Yue Yazhou, Liu Yushuang, et al. Design of integrated navigation system simulation platform based on RT-LAB[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1503-1508. (in Chinese)
shu

Design of integrated navigation system simulation platform based on RT-LAB

  • 1.

    Science and Technology on Aircraft Control Laboratory, Xi'an Flight Automatic Control Research Institute, Xi'an 710065, China

  • 2. School of Instrumentation Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 04 Dec 2012
  • Publish Date: 30 Nov 2013
    Abstract
  • A strapdown inertial navigation system/global positioning system/celestial navigation system(SINS/GPS/CNS) simulation platform based on RT-LAB was designed. Based on attitude, position and velocity, the integrated navigation system solution with federated Kalman filter has the capability of fault detection, isolation and system reconfiguration. The SINS/GPS sub-filter observations are the difference of position and velocity. And the inertial attitude information of carrier was given by CNS, therefore the attitude error measurement of SINS was obtained. Simulation results show that the solutions have the stronger fault tolerant performance and higher navigation accuracy and the stronger real-time performance. The work is valuable for the research of related techniques in integrated navigation system.

     

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