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Development of multisensor fusion techniques with gating networks applied to reentry vehicles.

机译:具有应用于再入车辆的门控网络的多传感器融合技术的发展。

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摘要

The problem of model inaccuracy for Extended Kalman Filters (EKF) is addressed in the case of vehicle atmospheric entry tracking and navigation with a filter bank architecture, also called mixture-of-experts, regulated by gating network, which is then tested in two different applications.; First, a wind-frame based flight model is developed, which allows for maneuvers, and inclusion of atmospheric and gravity models. This level of complexity allows in theory for better estimation accuracy when used in an EKF, but the filter performance is in part dependent on the accuracy of the vehicle and environment models. The problem is how to deal with imperfect models. The approach treated here, which has already been applied in other domains, is to create a population of filters, each representing a particular modeling of the vehicle and/or environment. The discriminating device between the expert filters is a gating network, which is a simplified single-layer neural network learning in real-time with the help of the statistical information from the filters. The gating network is used to compute a weighted sum of the state estimate from each filter, which is therefore an optimal estimate. The gating network can also be used as an hypothesis tester, which is the case in the first example.; The system was applied to the tracking and identification at high altitude of reentering spiraling objects accompanied by decoys. The object is being tracked at high altitude by three ground radars providing a variety of measurements which are treated in parallel by two filters, one being an expert tuned for the real target and the other tuned for the decoy. Experiments show that the regulated bank can rapidly correctly identify the object as being the real target.; The second application is precision Mars entry navigation, where the on-board navigation system of a maneuvering Mars lander used a bank of expert EKF, each processing inertial acceleration as measurement, and each designed around a specific realization of the imperfectly known atmospheric density profile. The objective here is less to identify the best performing model than optimizing the overall state estimate by combining the estimate from every filter. The system also periodically restarts the filters with the current optimal estimate so as to keep all the filters competitive during all of the descent. The result is that this mixture-of-experts does not perform better than a dead-reckoning scheme unless one of the density model happens to be relatively close from the real density profile, but that it is more robust than dead-reckoning to loss of data, and can readily adapt additional sources of measurements.
机译:扩展卡尔曼滤波器(EKF)模型不准确的问题在车辆大气进入跟踪和导航中采用了由门控网络调节的滤波器组架构(也称为专家混合物)来解决,然后通过两种不同的测试应用。首先,开发了基于风框架的飞行模型,该模型可以进行机动,并包含大气和重力模型。从理论上讲,这种级别的复杂性可以在EKF中提供更好的估计精度,但是滤波器的性能部分取决于车辆和环境模型的精度。问题是如何处理不完善的模型。此处已处理的方法(已应用于其他领域)是创建一组过滤器,每个过滤器代表车辆和/或环境的特定模型。专家过滤器之间的区分设备是选通网络,它是借助来自过滤器的统计信息实时进行的简化的单层神经网络学习。选通网络用于计算每个滤波器的状态估计值的加权和,因此它是最佳估计值。门控网络也可以用作假设检验器,第一个示例就是这种情况。该系统应用于高空跟踪并识别带有诱饵的螺旋形物体。三台地面雷达在高空跟踪该物体,该雷达提供了多种测量结果,并由两个滤波器并行处理,一个是为实际目标调整的专家,另一个是为诱饵调整的专家。实验表明,受监管银行可以迅速正确地将对象识别为真实目标。第二种应用是精确的火星进入导航,其中机动火星着陆器的机载导航系统使用了专家EKF库,每种处理都以惯性加速度作为测量值,并且每种设计均围绕着不完全已知的大气密度剖面的特定实现进行设计。与组合每个滤波器的估算值来优化总体状态估算值相比,此处的目标不是确定最佳性能模型。系统还使用当前的最佳估计值定期重新启动滤波器,以使所有滤波器在所有下降期间保持竞争力。结果是,除非一种密度模型恰好相对于实际密度分布相对接近,否则这种专家混合的性能不会比完全推重方案更好,但是它比完全推论更健壮,不会丢失。数据,并可以轻松调整其他测量来源。

著录项

  • 作者

    Dubois-Matra, Olivier.;

  • 作者单位

    The University of Texas at Austin.;

  • 授予单位 The University of Texas at Austin.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2003
  • 页码 139 p.
  • 总页数 139
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:44:42

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