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A Tightly-Coupled GNSS/IMU Integration Algorithm for Multi-Purpose INS

机译:多功能INS的紧密耦合GNSS / IMU集成算法

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A tightly-coupled GNSS/INS integration algorithm hasbeen developed. It implements an approach where userdynamics model is expressed via accelerometer and gyromeasurements. That resulted in higher computationalefficiency and seamless filter design. In proposedalgorithm INS data is fed into receiver’s tracking loops tocompensate line-of-sight dynamics and tighten theirbandwidths. It increases the receiver’s sensitivity andantijam capability. From the other hand, receiver’s PVT(Position, Velocity, Time) output allowed to estimate andcompensate IMU errors – that resulted in more preciseINS navigation solution in standalone mode (duringGNSS outages). The development and simulation resultsfor the proposed algorithm with tactical-grade IMU arepresented in this paper.
机译:紧密耦合的GNSS / INS集成算法具有 已开发。它实现了一种方法,其中用户 动力学模型通过加速度计和陀螺仪表示 测量。导致更高的计算量 效率和无缝过滤器设计。在提议中 算法INS数据被馈送到接收器的跟踪循环中,以 补偿视线动态并加强其动态 带宽。它提高了接收器的灵敏度,并且 抗干扰能力。另一方面,接收者的PVT (位置,速度,时间)输出允许估算和 补偿IMU错误–导致更精确 独立模式下的INS导航解决方案(在 GNSS中断)。开发与仿真结果 对于带有战术级IMU的拟议算法, 在本文中提出。

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