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本文主要研究了微机电陀螺的误差分析、建模和补偿，以及在飞行器导航中的应用。
Error analysis, modeling and compensation of MEMS gyroscope and its application in navigation of flight vehicle are researched in this paper.
微机电陀螺与传统的机电类陀螺和光电类陀螺相比，具有成本低、尺寸小、重量轻、可靠性高等优点。
Comparing with conventional electro-mechanical gyroscope and electro-optical gyroscope, MEMS gyroscope has the advantages of low cost, small size, low weight and high reliability.
为实时准确获取弹体俯仰和滚转参数，提出一种利用磁阻传感器获取地磁场强度，结合微机电陀螺精确求解弹体姿态的方法。
To acquire projectile body pitch and roll parameters on real-time, put forward a new projectile body attitude method, using to obtain geomagnetic field intensity and combine microcomputer gyroscope.
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