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Initial Relative Orbit Determination Analytical Covariance and Performance Analysis for Proximity Operations

机译:初始操作的相对轨道确定分析协方差和性能分析

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摘要

This research furthers the development of a closed-form solution to the angles-only initial relative orbit determination problem for close-in proximity operations when the camera offset from the vehicle center of mass allows for range observability. Emphasis is placed on developing closed-form error covariance equations for the initial relative orbit state solution and verification of the analytic covariance equations through systematic nonlinear Monte Carlo simulation of typical rendezvous missions. Closed-form analytic estimates of the relative state error covariance based on angle measurement errors, attitude knowledge errors, and camera center-of-mass offset uncertainties for three or more observations are obtained. A two-body Monte Carlo simulation system is used to evaluate the performance of the closed-form relative state estimation algorithms and associated closed-form covariance equations. The sensitivity of the solution accuracy to spacecraft trajectories, camera offset, camera accuracy, attitude knowledge, and the time interval between measurements is presented and discussed.
机译:这项研究进一步发展了一种封闭形式的解决方案,该解决方案用于当摄像头偏离车辆质心时允许进行范围可观察性时,用于近距离接近操作的仅角度初始相对轨道确定问题。重点放在开发用于初始相对轨道状态解的闭合形式误差协方差方程,以及通过典型交会任务的系统非线性蒙特卡洛模拟对解析协方差方程进行验证。获得基于角度测量误差,姿态知识误差和相机质量中心偏移不确定性的相对状态误差协方差的闭式解析估计,用于三个或多个观测值。使用两体蒙特卡洛模拟系统评估封闭形式相对状态估计算法和相关封闭形式协方差方程的性能。提出并讨论了解决方案精度对航天器轨迹,摄像机偏移,摄像机精度,姿态知识以及两次测量之间的时间间隔的敏感性。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2016年第5期|822-835|共14页
  • 作者单位

    Northwestern Polytech Univ, 127 Youyi West Rd, Xian 710072, Peoples R China|Utah State Univ, 4130 Old Main Hill, Logan, UT 84322 USA;

    Utah State Univ, 4130 Old Main Hill, Logan, UT 84322 USA;

    Northwestern Polytech Univ, 127 Youyi West Rd, Xian 710072, 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

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