High-precision ground trajectory repetitive orbit optimization method and system

The invention provides a high-precision ground trajectory repetitive orbit optimization method and system. The method comprises steps of building a corresponding satellite orbit dynamics recursion model according to the analysis of a non-spherical perturbation order demand of an earth gravity field;...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SUN YINGMEI, CHEN GUOZHONG, LIU YANYANG, LI NAN, CHEN ZHONGHUA, LING HUIXIANG, CHEN YUNLI, XIN TAILIN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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