Problems of flight operations monitoring nanosatellite with a fair launches from the orbiter of launch vehicle ”Soyuz”

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Considered uncontrolled move the center of mass of associated nanosatellite after launch from the orbiter of launch vehicle “Soyuz”. Formed probabilistic models of the initial conditions of angular motion. Thepossibility of a successful solution of navigation and connected problems during the short-term scientific experiments using satellite navigation systems and low-altitude communication networks.

The center of mass motion, regular precession, density distribution, phase center of the antenna, satellite navigation, satellite communication system globalstar, launch vehicle, nano-satellite

Короткий адрес: https://sciup.org/148201625

IDR: 148201625

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