Abstract
The first results of the improvement of the state vector of the Spektr-R spacecraft of the RadioAstron mission, which is a part of an earth–space radio interferometer, are presented. The state vector includes three components for the spacecraft position and three components for its velocity in the Geocentric Celestial Reference System. Kalman filtering on the basis of radio range and Doppler data allows refinement of the components at each iteration. It is shown that orbit improvement increases the accuracy of the orbit determined at the Keldysh Institute of Applied Mathematics.
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.
