首页> 外文会议>2014 International Conference on Multisensor Fusion and Information Integration for Intelligent Systems >X-ray pulsar-based autonomous navigation based on asynchronous observation ST-REKF
【24h】

X-ray pulsar-based autonomous navigation based on asynchronous observation ST-REKF

机译:基于异步观测ST-REKF的基于X射线脉冲星的自主导航

获取原文
获取原文并翻译 | 示例

摘要

X-ray pulsar, as a natural star, has a high precision rotation period and strong antijamming capability. Its high stability and wide range of application is very suitable for spacecraft autonomous navigation. This paper presents an approach for the X-ray pulsar autonomous navigation based on asynchronous observation strong tracking robust kalman filter. The asynchronous observation model can more appropriately and more accurately describe the actual pulsar observation circumstances than the traditional synchronous observation model does. Navigation methods based on this observation model can achieve better real-time performance as well as higher positing accuracy. The approach presented in this paper using strong tracking robust kalman filter (ST-REKF) based on the asynchronous observation model for the pulsar positioning system can effectively improve the robustness and tracking ability to the actual state of the nonlinear system with uncertainties even when jumps occur after the system becomes smooth and steady, which can not be performed well by extended kalman filter (EKF).
机译:X射线脉冲星作为自然星,具有高精度的旋转周期和强大的抗干扰能力。它的高稳定性和广泛的应用范围非常适合航天器自主导航。本文提出了一种基于异步观测强跟踪鲁棒卡尔曼滤波器的X射线脉冲星自主导航方法。与传统的同步观测模型相比,异步观测模型可以更恰当,更准确地描述实际的脉冲星观测情况。基于该观测模型的导航方法可以实现更好的实时性能以及更高的定位精度。本文提出的使用基于异步观测模型的强跟踪鲁棒卡尔曼滤波器(ST-REKF)的脉冲星定位系统的方法可以有效地提高对不确定性非线性系统实际状态的鲁棒性和跟踪能力,即使出现跳跃也是如此系统变得平稳稳定之后,扩展卡尔曼滤波器(EKF)不能很好地执行此操作。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号