概括
精确的航天器立场测定需要精确校准集成的恒星传感器和陀螺仪. 这项研究引入了一种逐步校准方法,以有效地纠正外部参数错误,显著提高态度估计的准确性.
科学领域:
- 太空飞船态度的确定空间飞船的态度的确定
- 传感器融合式传感器
- 导航系统 导航系统
背景情况:
- 整合恒星传感器和陀螺仪可以提高航天器的态度测量动态和稳定性.
- 集成传感器外部参数中的错误会增加定位判断中的固定的错误.
- 集成系统参数的实时校正对于准确的态度估计至关重要.
研究的目的:
- 为了解决在统一校准中合参数的挑战,这增加了计算时间.
- 为高效和准确的系统参数校正提出一个阶段性校准方法.
- 在高度动态的场景中提高航天器态度估计的准确性.
主要方法:
- 利用不变的内部星角进行相机内在参数校准,独立于外在参数.
- 基于集成传感器的观测向量误差模型构建观察和状态方程.
- 实施以可观测性分析为指导的4位置机动策略,以快速解陀螺仪偏差,态度误差和外部参数.
主要成果:
- 拟议的逐步校准方法有效地将系统参数脱.
- 外在参数误差被减少到弧秒级.
- 模拟结果验证了该方法在提高态度估计准确性的有效性.
结论:
- 步骤校准方法为纠正集成传感器参数提供了有效的解决方案.
- 这种方法显著提高了航天器定位的准确性和可靠性.
- 该方法对于高精度和高动态航天器应用特别有利.
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