Abstract
In this paper, we discuss problems that exist during nanosatellite identification procedure. These problems are: choice of data collection interval that allows to identify required parameters with desired error, study of dependence model between identification parameters. We studied solution of these problems on the example of variable-mass SamSat-M nanosatellite which is equipped with propulsion unit. We obtained analytical model of parameters dependences and provided results of identification of fuel level.
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