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Comparison of Several Nonlinear Filters for Mars Entry Navigation Using Radiometric Measurements

机译:火星进入导航使用辐射测量的几种非线性滤波器的比较

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摘要

This paper studies the application of several nonlinear filters for the problem of Mars entry navigation by using radiometric measurements from Mars orbiters and Mars Surface Beacons (MSBs). A suitable dynamic model of Mars entry is developed. The movement of MSBs due to Mars rotation is also considered in the measurement model. The performance of an Extended Kalman Filter (EKF), First-order Divided Difference Filter (DDF1), Unscented Kalman Filter (UKF), and Particle Filter (PF) is compared in terms of estimation capability and computation costs. The theoretical Cramer-Rao Lower Bound (CRLB) of estimation errors are derived for Mars entry to evaluate the performance of the filters. A consistency test is also carried out to verify the filters. In simulations, by the comparison of estimation errors, position and velocity Root Mean Square Error (RMSE), error standard deviation versus Square Root of CRLB (SR CRLB), credibility and computation time, it is concluded that DDF1 is preferred for Mars entry navigation.
机译:本文使用火星轨道器和火星表面信标(MSB)的辐射测量技术,研究了几种非线性滤波器在火星进入导航问题中的应用。建立了合适的火星进入动力学模型。测量模型中还考虑了火星旋转引起的MSB移动。在估计能力和计算成本方面,对扩展卡尔曼滤波器(EKF),一阶除差滤波器(DDF1),无味卡尔曼滤波器(UKF)和粒子滤波器(PF)的性能进行了比较。推导了估计误差的理论Cramer-Rao下界(CRLB),供火星进入以评估滤波器的性能。还执行一致性测试以验证过滤器。在仿真中,通过比较估计误差,位置和速度均方根误差(RMSE),误差标准偏差与CRLB的平方根(SR CRLB),可信度和计算时间,得出结论,DDF1是火星进入导航的首选。

著录项

  • 来源
    《The Journal of Navigation》 |2017年第5期|983-1001|共19页
  • 作者单位

    Beijing Inst Technol, Sch Automat, Beijing, Peoples R China|Beijing Inst Technol, Key Lab Intelligent Control & Decis Complex Syst, Beijing, Peoples R China|Beijing Inst Technol, Key Lab Autonomous Nav & Control Deep Space Explo, Minist Ind & Informat Technol, Beijing, Peoples R China;

    Beijing Inst Technol, Sch Automat, Beijing, Peoples R China|Beijing Inst Technol, Key Lab Intelligent Control & Decis Complex Syst, Beijing, Peoples R China;

    Beijing Inst Technol, Sch Automat, Beijing, Peoples R China|Beijing Inst Technol, Key Lab Intelligent Control & Decis Complex Syst, Beijing, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Mars entry navigation; Radiometric measurements; First-order Divided Difference Filter (DDF1); Root Mean Square Error (RMSE);

    机译:火星进入导航;辐射测量;一阶除差滤波器(DDF1);均方根误差(RMSE);

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