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Development of Attitude Determination System for Moving Carrier Based on MEMS Sensors

机译:基于MEMS传感器的移动载具姿态确定系统的开发

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摘要

The moving carrier need accurate positioning and localization for their guidance, navigation and control. In order to get the space attitude of the carrier accurately and real-time, an attitude determination system of MEMS gyros, accelerometers and magnetometer is proposed in this paper. The design of electronic system adopts dual-core mode that based on FPGA and DSP, FPGA reads the measurement data of combined sensors to internal FIFO and then sends interrupt signal to DSP, Float-point DSP is used as the attitude determination processor to exert the multiple sensors data fusion to accomplish the attitude determination. The paper illuminates the hardware realization of the scheme, as well as the software which is composed of overall process and the implement of IC protocol. Furthermore, the software of the multiple sensors data fusion is developed to calculate the accurate result of the carrier's attitude. Finally, the experiment of prototype vehicle verification was made. The result indicates that the static accuracy and dynamic accuracy of the attitude angle are respectively better than 0.15° and 2°, which meets the moving carrier's navigational requirements such as high reliability and high precision.
机译:移动的载体需要对其导航,导航和控制进行精确的定位和定位。为了准确,实时地获得载体的空间姿态,本文提出了一种MEMS陀螺仪,加速度计和磁力计的姿态确定系统。电子系统的设计采用基于FPGA和DSP的双核模式,FPGA将组合传感器的测量数据读取到内部FIFO,然后将中断信号发送到DSP,浮点DSP被用作姿态确定处理器来执行多传感器数据融合,完成姿态确定。阐述了该方案的硬件实现,以及由整个过程和IC协议的实现组成的软件。此外,开发了多传感器数据融合软件来计算载体姿态的准确结果。最后,进行了原型车验证实验。结果表明,姿态角的静态精度和动态精度分别优于0.15°和2°,满足了移动载体对导航的高可靠性,高精度等导航要求。

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