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首页> 外文期刊>Advances in space research >X-ray pulsars/Doppler integrated navigation for Mars final approach
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X-ray pulsars/Doppler integrated navigation for Mars final approach

机译:X射线脉冲星/多普勒综合导航,火星最终进近

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摘要

The performance of the navigation system during the Mars final approach phase determines the initial accuracy of Mars entry phase, which is critical for a pin-point landing. An X-ray pulsars/Doppler integrated navigation strategy is proposed to improve the estimation accuracy of the spacecraft's entry state, as well as to enhance the autonomy, real-time and reliability. The navigation system uses the X-ray pulsar measurements and Doppler velocity measurements which are complementary to each other. The performance degradation in velocity estimation at the end of the final approach phase for X-ray pulsar based navigation can thus be eliminated. The nonlinearity of the system and the performance of Extended Kalman Filter are analyzed in this paper. Furthermore, in order to optimize the navigation scheme, a principle for navigation beacons selection based on the Fisher information matrix is used. Finally, a navigation scenario based on the 2012 encounter at Mars of Mars Science Laboratory spacecraft is considered to demonstrate the feasibility and accuracy of the proposed scheme. Simulation results also indicate that the proposed navigation scheme has reference value for the design of the future Mars explorations.
机译:导航系统在火星最后进近阶段的性能决定了火星进入阶段的初始精度,这对于精确着陆至关重要。提出了一种X射线脉冲星/多普勒组合导航策略,以提高航天器进入状态的估计精度,并增强其自主性,实时性和可靠性。导航系统使用相互补充的X射线脉冲星测量值和多普勒速度测量值。因此,可以消除基于X射线脉冲星的导航在最终进近阶段结束时速度估计的性能下降。本文分析了系统的非线性和扩展卡尔曼滤波器的性能。此外,为了优化导航方案,使用了基于费舍尔信息矩阵的导航信标选择原理。最后,以2012年在火星科学实验室飞船上的相遇为基础的导航场景被认为可证明该方案的可行性和准确性。仿真结果还表明,所提出的导航方案对未来火星探测的设计具有参考价值。

著录项

  • 来源
    《Advances in space research 》 |2016年第9期| 1889-1900| 共12页
  • 作者单位

    Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 10081, China Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China Mail box 22, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 10081, China Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China Mail box 22, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 10081, China Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China Mail box 22, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 10081, China Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China Mail box 22, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

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

    X-ray pulsar based navigation; Doppler velocity measurement; Integrated navigation; Mars final approach;

    机译:基于X射线脉冲星的导航;多普勒速度测量;集成导航;火星最后的方法;

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