Method, device, medium and equipment for determining self-alignment precision of rocket inertial measurement unit

The invention provides a method for determining calibration precision of a rocket inertial measurement unit. The method comprises the following steps: determining a third reference coordinate transformation matrix between a reference inertial measurement unit coordinate system and a to-be-calibrated...

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Bibliographische Detailangaben
Hauptverfasser: WANG ZHIJUN, ZUO ZHAN, DING SHUHANG, HUA XIANGDONG, YUE XIAOFEI, WANG DENGHUI, LI XINRAN, ZHOU XIN, XIE FENGYUN, LI XUN, HUANG XIAOPING
Format: Patent
Sprache:chi ; eng
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