Spacecraft orbital orientation stabilization by the inertial executive devices using unloading by the structure transformation method
Published: 14.05.2024
Authors: Simonyants R.P., Bulavkin V.N.
Published in issue: #5(149)/2024
DOI: 10.18698/2308-6033-2024-5-2359
Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft