Journal
Scientific and technical journal «Priborostroenie»
UDK629.7.05
Issue:4 (52)
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There is analytical method of calculation of realative tethered motion of spacecraft and mini-, microsatellite during the different laws of strength tether. Stretch tether with microsatellite direct the orbit flat of motion centre mass of space tether system. Relative motion microsatellite investigate in mobile orbit system.