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Conversion between osculating and mean orbital elements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Guinn, Joseph Vincent, Mark Chung, Min-Kun |
| Copyright Year | 2006 |
| Description | 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. |
| File Size | 49105 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110014148 |
| Archival Resource Key | ark:/13960/t8jd9tz8v |
| Language | English |
| Publisher Date | 2006-11-01 |
| Access Restriction | Open |
| Subject Keyword | Space Communications, Spacecraft Communications, Command And Tracking Orbital Mechanics Spacecraft Orbits Spacecraft Maneuvers Orbit Calculation C Programming Language Orbit Determination Orbital Position Estimation Orbital Elements Space Navigation Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
