MainCatalogAviation, Rocket and Space EngineeringDynamics, Ballistics, Flying Vehicle Motion Control
Precise system of navigation and motion control of artificial Earth sattelites
Authors: Gaushus E.V., Zybin Yu.N., Mikhaylov M.V., Antonov A.V. | Published: 12.07.2015 |
Published in issue: #1(25)/1997 | |
DOI: | |
Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
Keywords: |
A problem of modem precise navigation and motion control systems development for artificial Earth satellites is considered. One of the prospective modifications is proposed for building the artificial satellite orientation control systems. As external information sensors the star sensors are only used, as executive members - double-degree gyro stabilizers (gyrodynes) and jet engines.