Abstract
Mathematical models of the dynamics of rotational and translational motion of the satellite in a circular orbit and the operation of the technical vision system are described. The proposed algorithm for pointing the satellite at the object and determining its relative coordinates. The laws of controlling translational and rotational movement of the satellite are presented. The simulation of the automatic rendezvous system using the technical vision system was carried out and its results were shown.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
