Missile-borne platform navigation method and system

The invention provides a missile-borne platform navigation method and system. The missile-borne platform navigation method comprises the following steps: acquiring an output state value at the current moment through an inertial navigation device; inquiring a map landmark at the current moment, and c...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: HE ZHANGMING, LYU DONGHUI, WANG JIONGQI, CHEN YUYUN, HOU BOWEN, WEI JUHUI, ZHOU XUANYING
Format: Patent
Sprache:chi ; eng
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