Abstract
In this paper we use the theory of multivariate error analysis to find the expression for the covariance matrix of satellite positions attained by the astronomical method. The dependence of the positional accuracy of the target to the reference stars and on its position within an interpolated segment is discussed and explicit formulae are given.
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.
