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Development of an Integrated Low-Cost GPS/Rate Gyro System for Attitude Determination

机译:集成的低成本GPS /速率陀螺仪姿态确定系统的开发

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摘要

The use of low-cost GPS receivers and antennas for attitude determination can significantly reduce the overall hardware system cost. Compared to the use of high performance GPS receivers, the carrier phase measurements from low-cost equipment are subject to additional carrier phase measurement errors, such as multipath, antenna phase centre variation and noise. These error sources, together with more frequent cycle slip occurrences, severely deteriorate attitude determination availability, reliability and accuracy performance. This paper presents the investigation of a low-cost GPS/gyro integration system for attitude determination. By employing the dead reckoning sensor type, the ambiguity search region can be specifically defined as a small cube to enhance the ambiguity resolution process. A Kalman filter is implemented to fuse the rate gyro data with GPS carrier phase measurements. The quality control system based on innovation sequences is used to identify cycle slip occurrences and incorrect inter-antenna vector solutions. The availability of the integrated system also improves with respect to the GPS standalone system since the attitude parameters can be estimated using the angular rate measurements from rate gyros during GPS outages. The low-cost hardware used to design and test the integrated system consists of CMC Allstar receivers with the OEM AT575-70 antennas and Murata ENV-05D-52 piezoelectric vibrating rate gyroscopes. Tests in the urban area demonstrated that the introduction of rate gyros in a GPS-based attitude determination system not only effectively decreased the noise level in the estimated attitude parameters but coasted the attitude output during GPS outages and also significantly improved the system reliability.
机译:使用低成本GPS接收器和天线进行姿态确定可以显着降低总体硬件系统成本。与使用高性能GPS接收器相比,来自低成本设备的载波相位测量会遭受额外的载波相位测量误差,例如多径,天线相位中心变化和噪声。这些错误源以及更频繁的周跳发生,严重恶化了姿态确定的可用性,可靠性和准确性。本文提出了一种用于姿态确定的低成本GPS /陀螺仪集成系统的研究。通过使用航位推算传感器类型,可以将模糊度搜索区域具体定义为一个小立方体,以增强模糊度解析过程。实施了卡尔曼滤波器以将速率陀螺仪数据与GPS载波相位测量值融合在一起。基于创新序列的质量控制系统用于识别周跳现象和不正确的天线间矢量解。相对于GPS独立系统,集成系统的可用性也得到了提高,因为可以使用GPS中断期间来自速率陀螺仪的​​角速率测量来估算姿态参数。用于设计和测试集成系统的低成本硬件包括带有OEM AT575-70天线的CMC Allstar接收器和Murata ENV-05D-52压电振动速率陀螺仪。在市区进行的测试表明,在基于GPS的姿态确定系统中引入速率陀螺仪不仅可以有效地降低估计的姿态参数中的噪声水平,而且可以在GPS中断期间保持姿态输出,并显着提高系统的可靠性。

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