Rapid aiming method and system for rocket launched on sea

The invention relates to the field of rocket launching, in particular to a rapid aiming system for a marine launched rocket, which comprises a photoelectric auto-collimator, an inertia-satellite integrated navigation system and an aiming computer which are fixed in an equipment cabin, the inertia-sa...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	WU WEIPING, LIU KAI, HAN GUANCHAO, MA YUHAI, ZHANG ZHIJING
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AMMUNITION APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HARPOON GUNS HEATING LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to the field of rocket launching, in particular to a rapid aiming system for a marine launched rocket, which comprises a photoelectric auto-collimator, an inertia-satellite integrated navigation system and an aiming computer which are fixed in an equipment cabin, the inertia-satellite integrated navigation system is used for obtaining speed, position and attitude information of the inertia-satellite integrated navigation system in real time; the photoelectric autocollimator is used for measuring the azimuth angle deviation between the photoelectric autocollimator and the prism on the rocket; the aiming computer takes the speed and position of the inertia-satellite integrated navigation system as the speed and position information of the rocket, and obtains the azimuth angle of the prism on the rocket according to the received azimuth angle deviation between the photoelectric autocollimator and the prism on the rocket and the attitude information of the inertia-satellite integrated naviga