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Low-cost attitude estimation with MIMU and two-antenna GPS for Satcom-on-the-move

机译:利用MIMU和两天线GPS进行移动卫星的低成本姿态估计

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摘要

We detail a low-cost method to estimate vehicle attitude for Satcom-on-the-move (SOTM) using micro inertial measurement unit and two-antenna global positioning system (GPS). The attitude is calculated by integrating gyros, while accelerometers and GPS are used as an aiding system to calibrate the gyro biases. In order to accurately eliminate the accelerometer errors induced by maneuvering accelerations, a sideslip compensation is proposed to calibrate the acceleration estimation derived from the GPS-measured velocity. An adaptive unscented Kalman filter is then developed to deal with the failure of the two-antenna GPS to provide the yaw and sideslip angles. When the yaw angle is unavailable and the vehicle is in straight motion, the yaw angle observation is substituted by velocity heading. During turning, the yaw angle observation is turned off and the yaw angle estimates are obtained from integrating gyros only. Meanwhile, the sideslip angle is estimated by differencing the yaw angle estimate and the velocity heading. The performance of the proposed method is demonstrated with driving tests, suggesting that this technique is a viable candidate for low-cost SOTM.
机译:我们详细介绍了一种使用微惯性测量单元和两天线全球定位系统(GPS)估算移动卫星(SOTM)车辆姿态的低成本方法。姿态是通过集成陀螺仪来计算的,而加速度计和GPS则用作校准陀螺仪偏置的辅助系统。为了准确消除由机动加速度引起的加速度计误差,提出了一种侧滑补偿,以校准从GPS测量的速度得出的加速度估计值。然后,开发了自适应无味卡尔曼滤波器,以处理两天线GPS无法提供偏航角和侧滑角的问题。当偏航角不可用并且车辆处于直线运动时,偏航角观测将由速度航向代替。在转弯期间,关闭偏航角观察,并且仅从积分陀螺仪获得偏航角估计。同时,通过使偏航角估计和速度航向相差来估计侧滑角。驾驶测试证明了该方法的性能,表明该技术是低成本SOTM的可行选择。

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