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Parametric Error Equations for Dead Reckoning Navigators used in Ground Vehicle Guidance and Control

机译:地面车辆制导与控制中航位推测导航器的参数误差方程

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This paper develops and validates parametric error models for a GPS-aided dead reckoning navigator for ground vehicle guidance and control. The dead reckoning navigator fuses information from a rate gyro and a Doppler radar to provide a two-dimensional navigation solution during momentary GPS outages. When available, GPS is used to calibrate the dead reckoning sensor errors. The error models developed provide a quick and accurate method for predicting the navigator's performance during these momentary GPS outages. The models parameterize the navigation performance as a function of sensor quality, sensor sampling rate and GPS outage length. The error models are validated in a series of tests using a farm tractor. The models predict and the tests show that this dead reckoning system can provide a 61 deg heading and 0.3 m position accuracy during a 20-40 s GPS outage.
机译:本文开发并验证了用于地面车辆导航和控制的GPS辅助航位推算导航仪的参数误差模型。航位推测导航器融合了来自速率陀螺仪和多普勒雷达的信息,可在GPS暂时中断时提供二维导航解决方案。 GPS可用时,用于校准航位推算传感器错误。开发的错误模型提供了一种快速而准确的方法,用于在这些瞬时GPS中断期间预测导航器的性能。这些模型将导航性能参数化为传感器质量,传感器采样率和GPS中断长度的函数。使用农用拖拉机在一系列测试中验证了错误模型。模型预测和测试表明,这种航位推算系统可在20-40 s GPS中断期间提供61度航向和0.3 m的定位精度。

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