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A general time element using cartesian coordinates: eccentric orbit integration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Janin, G. |
| Copyright Year | 1980 |
| Description | A general time element, valid with any arbitrary independent variables, and used with Cartesian coordinates for the integration of the elliptic motion in orbits, is examined. The derivation of the time element from a set of canonical elements of the Delaunay type, developed in the extended phase space, is presented. The application of the method using an example of a transfer orbit for a geosynchronous mission is presented. The eccentric and elliptic anomaly are utilized as the independent variable. The reduction of the in track error resulting from using Cartesian coordinates with the time element is reported. |
| File Size | 789303 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800008861 |
| Archival Resource Key | ark:/13960/t6zw6862b |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Orbital Mechanics Measure and Integration Error Analysis Eccentric Orbits Time Functions Transfer Orbits Mathematical Models Cartesian Coordinates 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 |
