Volume 41 Issue 2
Feb.  2015
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HUO Hangyu, ZHANG Xiaolin. Fast satellite selection method for integrated navigation systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 273-282. doi: 10.13700/j.bh.1001-5965.2014.0138(in Chinese)
Citation: HUO Hangyu, ZHANG Xiaolin. Fast satellite selection method for integrated navigation systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 273-282. doi: 10.13700/j.bh.1001-5965.2014.0138(in Chinese)

Fast satellite selection method for integrated navigation systems

doi: 10.13700/j.bh.1001-5965.2014.0138
  • Received Date: 21 Mar 2014
  • Publish Date: 20 Feb 2015
  • On the basis of the relationship between the number of the selected satellites and geometry dilution of precision (GDOP) and navigation computation, a genetic algorithm (GA)-based fast satellite selection method named fast genetic satellite selection method (FGSSM) was proposed. In this method, firstly the initial number of selecting satellites and GDOP threshold was decided according to the precision of user's requirement. And then the initial population of satellite selection solutions was constructed. Under the condition that evolution algebra limit is less than 1, the initial solution was obtained by selection, crossover and mutation operation. Whether the initial solution was optimized based on the principles of GDOP minimum was determined by the relationship between the GDOP of the initial solution and the GDOP threshold. The optimization terminates until the termination condition was satisfied and final solution was obtained. The experiment results show that, the method can satisfy GDOP of the solution at the request of 2.5 to 6 within an evolutionary, with no less than 92.45% probability, at the same time it can effectively reduce more than 54.75% of the navigation computation.

     

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