Carrier rocket orbit parameter reconstruction method based on iterative guidance

The invention relates to a carrier rocket orbit parameter reconstruction method based on iterative guidance, and belongs to the field of carrier rocket guidance control. The method comprises the following steps of 1, collecting carrier rocket state information; 2, calculating the consumption of a pr...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KUANG DONGZHENG, MAO CHENGYUAN, QIU WEI, HAO CHUANCHUAN, CHEN ERKANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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