2006•NASA Technical Reports Server (NASA)Requires access
Conversion Between Osculating and Mean Orbital Elements
Joseph Guinn, Min-Kun Chung, Mark A. Vincent
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Abstract
Osculating/Mean Orbital Element Conversion (C version) (OSMEANC) is a C-language computer program that performs precise conversions between osculating and mean classical orbital elements. OSMEANC can be used for precise design of spacecraft missions and maneuvers and precise calculation of planetary orbits. The program accounts for the full complexity of gravitational fields, including aspherical and third-body effects.