ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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2
Issue
vol 60 / FEBRUARY, 2017
Article
UDC 629.7.05

ANALYTICAL METHOD FOR CALCULATION OF SMALL SPACE VEHICLE MOTION LINKED TO A BASIC SPACECRAFT

A. V. Averianov
Mozhaysky Military-Space Academy, Department of Electron Calculation Techniques;


Abstract. 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.
Keywords: space tether systems, relative microsatellite motion, dynamic of space tetherd systems.