文献分析表明，惯性测量与姿态参考系统的理论及应用研究主要集中在传感器信息综合方面。
Many references show that the theoretic and practical researches on inertial surveying and attitude reference systems are predominantly in the field of sensor data integration.
该课题希望通过对MEMS技术和MEMS惯性传感器的研究，研制和设计出一系列能够应用于火箭和导弹制导的MIMU系统。
By the research for MEMS and the MEMS acceleration sensor, This assignment will finish a series of MIMU system, which will be applied to the rocket and the missile guided system.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法，并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
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