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Information fusion in navigation systems via factor graph based incremental smoothing

机译:导航系统中基于因子图的增量平滑的信息融合

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This paper presents a new approach for high-rate information fusion in modern inertial navigation systems, that have a variety of sensors operating at different frequencies. Optimal information fusion corresponds to calculating the maximum a posteriori estimate over the joint probability distribution function (pdf) of all states, a computationally-expensive process in the general case. Our approach consists of two key components, which yields a flexible, high-rate, near-optimal inertial navigation system. First, the joint pdf is represented using a graphical model, the factor graph, that fully exploits the system sparsity and provides a plug and play capability that easily accommodates the addition and removal of measurement sources. Second, an efficient incremental inference algorithm over the factor graph is applied, whose performance approaches the solution that would be obtained by a computationally-expensive batch optimization at a fraction of the computational cost. To further aid high-rate performance, we introduce an equivalent IMU factor based on a recently developed technique for IMU pre-integration, drastically reducing the number of states that must be added to the system. The proposed approach is experimentally validated using real IMU and imagery data that was recorded by a ground vehicle, and a statistical performance study is conducted in a simulated aerial scenario. A comparison to conventional fixed-lag smoothing demonstrates that our method provides a considerably improved trade-off between computational complexity and performance.
机译:本文提出了一种现代惯性导航系统中高速率信息融合的新方法,该系统具有各种以不同频率工作的传感器。最佳信息融合对应于计算所有状态的联合概率分布函数(pdf)上的最大后验估计,这在通常情况下是计算昂贵的过程。我们的方法由两个关键组成部分组成,这产生了一个灵活,高速率,接近最佳的惯性导航系统。首先,联合pdf使用图形模型(因子图)表示,该模型充分利用了系统的稀疏性,并提供了即插即用的功能,可轻松容纳测量源的添加和删除。其次,应用了一种基于因子图的高效增量推理算法,该算法的性能接近解决方案,该解决方案将通过计算昂贵的批处理优化以较低的计算成本获得。为了进一步提高高速率性能,我们基于最新开发的IMU预集成技术引入了等效的IMU因子,从而大大减少了必须添加到系统中的状态数。通过使用实际IMU和地面车辆记录的图像数据对所提出的方法进行实验验证,并在模拟空中场景中进行了统计性能研究。与常规固定滞后平滑的比较表明,我们的方法在计算复杂度和性能之间提供了显着改善的折衷。

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