Simplified perturbations models
Results: 4
| # | Item |
|---|---|
1 | Microsoft Word - AIAARevisiting Spacetrack Report 3 Rev 2.docxAdd to Reading ListSource URL: celestrak.comLanguage: English - Date: 2012-08-06 14:16:05 |
2![Derivation of the Relationship Between B * and n&[removed]by Ted Molczan, October 1999 Background During, my experience with the NORAD “2-line” orbital elements and the SGP and SGP4 orbit propagators, revealed](https://www.pdfsearch.io/img/c41b123e807ff032894c5d302aeab703.jpg "Derivation of the Relationship Between B * and n&[removed]by Ted Molczan, October 1999 Background During, my experience with the NORAD “2-line” orbital elements and the SGP and SGP4 orbit propagators, revealed") | Derivation of the Relationship Between B * and n&[removed]by Ted Molczan, October 1999 Background During, my experience with the NORAD “2-line” orbital elements and the SGP and SGP4 orbit propagators, revealedAdd to Reading ListSource URL: www.satobs.orgLanguage: English - Date: 2014-03-04 13:06:01 |
3 | Tech Note #2 December 12, 2001Add to Reading ListSource URL: www.cdeagle.comLanguage: English - Date: 2012-12-12 06:26:36 |
4 | PDF DocumentAdd to Reading ListSource URL: www.amsat.orgLanguage: English - Date: 1996-10-06 04:10:13 |