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组合导航自适应卡尔曼滤波改进算法研究
引用本文:李旦,秦永元,梅春波. 组合导航自适应卡尔曼滤波改进算法研究[J]. 测控技术, 2011, 30(3): 114-116
作者姓名:李旦  秦永元  梅春波
作者单位:西北工业大学自动化学院,陕西西安,710129
摘    要:针对常规卡尔曼滤波由于噪声的统计特性与实际情况不相符而引起滤波误差增大的问题,提出了一种新的在线估计系统噪声和量测噪声的自适应滤波算法.新算法通过新息序列自适应量测噪声,对Sage-Husa滤波算法进行改进以估计系统噪声,该算法在噪声统计特性未知的情况下能进行滤波计算.最后对改进的新算法与常规卡尔曼滤波算法作了对比试验...

关 键 词:卡尔曼滤波  自适应滤波  新息序列  Sage-Husa滤波  组合导航

An Improved Adaptive Kalman Filter Algorithm for SINS/GPS Integrated Navigation System
LI Dan,QIN Yong-yuan,MEI Chun-bo. An Improved Adaptive Kalman Filter Algorithm for SINS/GPS Integrated Navigation System[J]. Measurement & Control Technology, 2011, 30(3): 114-116
Authors:LI Dan  QIN Yong-yuan  MEI Chun-bo
Affiliation:LI Dan,QIN Yong-yuan,MEI Chun-bo (School of Automation,Northwestern Polytechnical University,Xi'an 710129,China)
Abstract:A new adaptive Kalman filter algorithm is presented aiming at figure out accretion on the error of Kalman filter when process noise covariance matrix(Q) and measurement noise covariance matrix(R) are incorrectly with actual noise.The algorithm estimates R based on innovation sequence of measure and Q through an improved Sage-Husa adaptive filter,which can keep the filter work steadily and correctly when Q and R are unknown.Practical test on the new approach and the conventional Kalman filter algorithm compa...
Keywords:Kalman filtering  adaptive filtering  innovation sequence  sage-husa filtering  integrated navigation Building the Model of IMU in Flight Simulation  
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