用高精度光学传感器对太极形成进行自主状态估计和可观测性分析
Bo Wen1,2,3, Wenlin Tang2, Xiaodong Peng1,2,4
1School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS, Hangzhou 310024, China.
Sensors (Basel, Switzerland)
|November 14, 2023
概括
准确的航天器状态估计对于导航任务至关重要. 这项研究使用机载测量增强了跟踪,通过航天器间干扰度和辐射速度传感器显著提高了准确性.
科学领域:
- 太空飞船导航导航 太空飞船导航
- 天体动力学是指天体动力学.
- 估计理论估计理论
背景情况:
- 在某些航行任务阶段的地面观测限制.
- 不准确的航天器跟踪仅使用动态方程和先前知识.
- 需要使用机载测量来改进状态估计.
研究的目的:
- 为了调查船上的测量选择,以准确地估计太极形成的太空船状态.
- 通过使用航天器间干扰测量和传感器数据来评估两个方案.
- 分析系统可观测性和错误共变量传播.
主要方法:
- 使用单数值分解对可观测性的数值分析.
- 用立方卡尔曼波器进行错误共变量传播分析.
- 设计和模拟两个状态估计方案.
主要成果:
- 高精度的航天器间角度测量显著提高了系统的可观测性.
- 图1估计绝对位置和速度的精度分别为~3.1公里和~0.14米/秒.
- 使用辐射速度传感器数据的第2方案,与第1方案相比,大约提高了18倍的速度估计精度.
结论:
- 船上测量,特别是航天器间干扰测量,对于精确估计航天器状态至关重要.
- 拟议的方案在导航任务的传统方法上提供了显著的改进.
- 辐射速度传感器数据为速度估计的准确性提供了巨大的好处.
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