Mathematical model of a maneuvering nanosatellite with a heliothermal propulsion system and a flywheel orientation and stabilization system
Published: 18.05.2021
Authors: Zhumaev Z.S.
Published in issue: #5(113)/2021
DOI: 10.18698/2308-6033-2021-5-2078
Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft