Using the error model,the observability of SINS error states was quantificationally analyzed,rotating azimuth axis, pitch and yaw axis under two position alignment respectively.

 
  • 應用該模型,對SINS分別繞方位軸、俯仰軸和橫滾軸兩位置對準時(shí)系統的可觀(guān)測性進(jìn)行了定量分析,明確了SINS繞3個(gè)正交軸旋轉系統的可觀(guān)測性。
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