Volume 42 Issue 5
May  2016
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FAN Jiping, JIAO Jian, ZHAO Haitao, et al. SEU soft error effect modeling and simulation method for navigation satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(5): 1008-1015. doi: 10.13700/j.bh.1001-5965.2015.0325(in Chinese)
Citation: FAN Jiping, JIAO Jian, ZHAO Haitao, et al. SEU soft error effect modeling and simulation method for navigation satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(5): 1008-1015. doi: 10.13700/j.bh.1001-5965.2015.0325(in Chinese)

SEU soft error effect modeling and simulation method for navigation satellite

doi: 10.13700/j.bh.1001-5965.2015.0325
  • Received Date: 21 May 2015
  • Publish Date: 20 May 2016
  • Single event upset (SEU) soft error is one of the most important factors that affect the reliability and availability of satellite. To analyze and evaluate the SEU soft error propagation and effect in navigation satellite system, a novel finite-state machine (FSM)/Stateflow modeling method is proposed, where the basic model elements and modeling principles combined with protection and recovery strategies in satellite are presented. Through the simulation based on Simulink/Stateflow platform, the availability of satellite and mean task interruption time are obtained, and the effects of several recovery strategies on the availability of satellite are analyzed; moreover, a co-simulation between MATLAB and STK is conducted to evaluate the constellation positioning dilution of precision (PDOP) availability obtained from the simulation result of single satellite soft error propagation, which reflects the impacts of SEU soft error on both single satellite and constellation.

     

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