ANALYTICAL METHOD FOR CALCULATION OF SMALL SPACE VEHICLE MOTION LINKED TO A BASIC SPACECRAFT
Mozhaysky Military-Space Academy, Department of Information and Computing Systems and Networks;
Read the full article
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.
