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Vehicle-mounted satellite receiver positioning system based on the MEMS gyro

机译:基于MEMS陀螺仪的车载卫星接收器定位系统

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To ensure that the vehicular satellite receiver get enough of their own real-time, accurate attitude information, considering the requirements low-cost, MEMS (Micro- Electron Mechanical System) inertial device is applied to the design of attitude positioning system for satellite receiver. Because of the low accurate degree, inertial navigation can't fully used to help receiver to produce parameter. This paper undertakes to make use of parameter of velocity and attitude produced by laser gyro navigation system that installed in the head of the vehicle as MEMS inertial positioning system external combination information resource. And to integrate the MEMS inertial positioning system in the model of combining velocity and attitude by using Sage-Hausa adaptive filtering algorithm to evaluate the error of inertial navigation system on line, and rectify its calculating result so as to improve its degree of accurate. Through numerous analogical grounds vehicle operation experiments, the MEMS attitude positioning could reach the degree of accurate requirements by satellite receiver, therefore the testing program is feasible.
机译:为了确保车辆卫星接收器获得足够的自身实时,准确的姿态信息,考虑到低成本,MEMS(微电子机械系统)惯性装置应用于卫星接收器的姿态定位系统的设计。由于精度低,惯性导航不能完全用于帮助接收器产生参数。本文承诺利用由安装在车辆头部的激光陀螺导航系统产生的速度和姿态参数,作为MEMS惯性定位系统外部组合信息资源。并将MEMS惯性定位系统集成在组合速度和姿态模型中,使用Sage-Hausa自适应滤波算法在线评估惯性导航系统的误差,并纠正其计算结果,以提高其准确度。通过许多类似的基础地,MEMS姿态定位可以通过卫星接收器达到准确要求的程度,因此测试程序是可行的。

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