| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to space engineering and can be used in control of docked space objects (SO) motion. SOs are launched to target orbits from launching sites of one cosmodrome with time delay and with difference in target orbit inclinations to align orbit ascending nodes which difference depends on launched SO orbit inclination, launching site geographical latitude of SO being launched, angular velocity of Earth rotation and launching site geographic longitudes of SOs being launched, impulse for alignment of docked SOs orbit planes is determined, approach impulse is applied to one of SOs.EFFECT: invention permits to speed up SO docking.4 dwg |
