Publisher:Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004.
Citation:14th AAS/AIAA Space Flight Mechanics Meeting, Maui, HI, February 8-12, 2004
Abstract:
This paper describes the navigation-related aspects and analysis of the cut-off algorithm for the orbit-insertion burn. The algorithm is designed to achieve the desired orbital period even after the burn has been restarted due to possible burn interruptions.