2018
DOI: 10.1088/1757-899x/450/2/022028
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Simulation of short-range navigation system based pseudolites and investigation of its accuracy characteristics

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“…The position of the objects of observation is determined by the specified grid sizes and limited by the specified contour. The input parameters of the algorithm are divided into 3 groups: own parameters of the calculation, parameters of the technical characteristics of the remote sensing spacecraft and radio line, parameters of the data reception point and parameters of the simulation model [26][27][28][29][30][31][32][33].…”
Section: Evaluation Parametersmentioning
confidence: 99%
“…The position of the objects of observation is determined by the specified grid sizes and limited by the specified contour. The input parameters of the algorithm are divided into 3 groups: own parameters of the calculation, parameters of the technical characteristics of the remote sensing spacecraft and radio line, parameters of the data reception point and parameters of the simulation model [26][27][28][29][30][31][32][33].…”
Section: Evaluation Parametersmentioning
confidence: 99%
“…This suggests that the receiver firmware has been appropriately and significantly modified. In the simulated system [7], the authors suggested the creation of separate frames for sending coordinates of both satellites and pseudolites. Older solutions described in the literature assume storing pseudolites positions in databases inside the mobile receiver or transmitting stored pseudolite positions via wireless networks [8,9].…”
Section: Introductionmentioning
confidence: 99%