A design method of the micro inertial measurement unit (MIMU) system is introduced.
介绍了一种微惯性测量组合(MIMU)系统的设计方法。
A low cost calibration system for micro inertial measurement unit (MIMU) has been designed.
设计了一台低成本的微惯性测量组合标定系统。
In the paper, a series of research work was performed for improvement of reliability and precision of MIMU.
本文的研究工作正是针对提高微惯性元件和微惯性测量组合可靠性及精度这一中心展开的。
The MIMU navigation system has become one of the most popular navigation system for its outstanding merits and prospective applications.
MIMU导航系统因其突出的优点和良好的应用前景而成为当前导航界研究的热点之一。
However, comparing with conventional inertial measurement components, MIMU has lower precision, which severely handicap its application.
但是，与传统的惯性测量组合相比，微惯性测量组合的精度明显偏低，这极大地限制了它的应用。
MIMU/GPS integrated method is proposed for solving the problem that MIMU can not work alone for long time and the signal of GPS is not stable.
针对微惯性测量组合无法长时间单独工作、GPS卫星信号不稳定的问题，提出MIMU/GPS组合导航的方法。
Initial alignment could not be done by MIMU itself because of its low precision, so a method of using electrical compass in initial alignment is presented.
由于MIMU精度不高，无法实现自对准，所以系统采用电子罗盘辅助它完成初始化对准。
To study the data synchronization problem of MIMU/GPS integrated navigation systems, a new data synchronization method for GPS measurement data delay is proposed.
然后针对MIMU/GPS组合导航的数据时间同步问题，提出了一种新的GPS时间延迟补偿算法。
Micro inertial Measurement Unit (MIMU) which made up of micro inertial sensors gives a great progress in the miniaturization and micromation of inertial instrument.
采用微机械惯性敏感器的微惯性测量组合使得惯性仪表小型化和微型化技术产生了一次新的飞跃。
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.
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.
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。
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