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A beacon configuration optimization method based on Fisher information for Mars atmospheric entry

机译:基于Fisher信息的火星大气进入信标配置优化方法

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摘要

The navigation capability of the proposed Mars network based entry navigation system is directly related to the beacon number and the relative configuration between the beacons and the entry vehicle. In this paper, a new beacon configuration optimization method is developed based on the. Fisher information theory and this method is suitable for any number of visible beacons. The proposed method can be used for the navigation schemes based on range measurements provided by radio transceivers or other sensors for Mars entry. The observability of specific state is defined as its Fisher information based on the observation model. The overall navigation capability is improved by maximizing the minimum average Fisher information, even though the navigation system is not fully observed. In addition, when there is only one beacon capable of entry navigation and the observation information is relatively limited, the optimization method can be modulated to maximize the Fisher information of the specific state which may be preferred for the guidance and control system to improve its estimation accuracy. Finally, navigation scenarios consisted of 1-3 beacons are tested to validate the effectiveness of the developed optimization method. The extended Kalman filter (EKF) is employed to derive the state estimation error covariance. The results also show that the zero-Fisher information situation should be avoided, especially when the dynamic system is highly nonlinear and the states change dramatically.
机译:所提出的基于火星网络的进入导航系统的导航能力与信标号以及信标和进入车辆之间的相对配置直接相关。在此基础上,开发了一种新的信标配置优化方法。 Fisher信息理论和此方法适用于任何数量的可见信标。所提出的方法可以用于基于无线电收发器或其他用于火星进入的传感器提供的距离测量的导航方案。特定状态的可观察性定义为基于观察模型的Fisher信息。即使没有完全观察到导航系统,也可以通过使最小的平均Fisher信息最大化来提高整体导航功能。另外,当只有一个信标能够进入导航并且观察信息相对有限时,可以对优化方法进行调制,以最大化特定状态的Fisher信息,这对于制导和控制系统可能更可取,以改善其估计准确性。最后,测试了由1-3个信标组成的导航场景,以验证所开发优化方法的有效性。扩展卡尔曼滤波器(EKF)用于导出状态估计误差协方差。结果还表明,应该避免零费舍信息的情况,特别是当动态系统是高度非线性的并且状态急剧变化时。

著录项

  • 来源
    《Acta astronautica》 |2017年第4期|467-475|共9页
  • 作者单位

    Beijing Inst Technol, Inst Deep Space Explorat, Mail Box 22, Beijing 100081, Peoples R China|Beijing Inst Technol, Minist Ind & Informat Technol, Key Lab Autonomous Nav & Control Deep Space Explo, Beijing 100081, Peoples R China|Minist Educ, Key Lab Dynam & Control Flight Vehicle, Beijing 100081, Peoples R China;

    Beijing Inst Technol, Inst Deep Space Explorat, Mail Box 22, Beijing 100081, Peoples R China|Beijing Inst Technol, Minist Ind & Informat Technol, Key Lab Autonomous Nav & Control Deep Space Explo, Beijing 100081, Peoples R China|Minist Educ, Key Lab Dynam & Control Flight Vehicle, Beijing 100081, Peoples R China;

    Beijing Inst Technol, Inst Deep Space Explorat, Mail Box 22, Beijing 100081, Peoples R China|Beijing Inst Technol, Minist Ind & Informat Technol, Key Lab Autonomous Nav & Control Deep Space Explo, Beijing 100081, Peoples R China|Minist Educ, Key Lab Dynam & Control Flight Vehicle, Beijing 100081, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Beacon configuration; Optimization Fisher information; Radio navigation; Mars entry;

    机译:信标配置;优化Fisher信息;无线电导航;火星进入;

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