Abstract
The problem of transferring GEO SC to a specified standing point taking into account the SC insertion and correction error is considered. A combined method for calculating insertion corrections is suggested based on the algorithm for the optimal burn correction and numerical model for forecasting active SC COG motion, which yields a high calculation accuracy and allows one to minimize the orbit eccentricity at the end of the transferring phase. The method is software implemented and can be used to calculate transfer correction parameters during both the phase of GEO SC design and SC operation for their control.
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.
