托比特-无香料-卡尔曼-基于过器的态度估计算法使用恒星传感器和惯性陀螺组合
Xinmei Wang1,2,3,4, Hui Zhang1,2,3, Xiaodong Gao1,2,3
1National Key Laboratory of Optical Field Manipulation Science and Technology, Chinese Academy of Sciences, Chengdu 610209, China.
Micromachines
|June 28, 2023
概括
这项研究引入了一种托比特无气味的卡尔曼波器,以提高航天器在恒星传感器数据不可用时的位置估计准确性. 新的算法在传感器故障时提高了90%的精度,有效地管理了陀螺漂移.
科学领域:
- 太空飞船的导航和控制.
- 估计理论估计理论
- 传感器的融合传感器
背景情况:
- 环境因素迫使航天器恒星传感器中的数据进行审查,降低了传统的态度确定算法.
- 现有的算法在恒星传感器中断时难以准确地估计位置.
研究的目的:
- 为航天器开发一个高精度的态度估计算法.
- 为了解决因恒星传感器数据审查而导致的位置确定能力降低的问题.
主要方法:
- 建立了一个集成的恒星传感器和陀螺仪导航系统的非线性状态方程.
- 改进了无气味卡尔曼波器的测量更新过程.
- 应用托比特模型来描述陀螺仪在恒星传感器故障时的漂移,计算潜测量值并推导测量误差共变.
主要成果:
- 计算机模拟验证了拟议的算法.
- 在15分钟的恒星传感器故障期间,Tobit无气味卡尔曼波器在准确度上比标准无气味卡尔曼波器提高了90%.
- 过器有效地估计了由陀螺漂移引起的错误.
结论:
- 拟议的Tobit无气味卡尔曼波器提供了一种可行且有效的方法,用于高精度的航天器态度估计.
- 该算法成功地弥补了恒星传感器故障期间的陀螺漂移.
- 这种方法为航天器导航中的实际工程应用提供了理论支持.
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