对于高精度旋转惯性导航系统而言,一个以组属为基础的反向对齐方法
Chao Liu1,2, Ding Li1,2, Huiping Li1,2
1College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, China.
本研究引入了用于旋转惯性导航的新反向对齐方法,显著提高了准确性并减少了错误. 这种方法提高了高性能导航系统的精度.
科学领域:
- 工程 工程师 工程师 工程师
- 导航系统 导航系统
- 控制理论 控制理论
背景情况:
- 初始对齐对于惯性导航系统 (INS) 来说至关重要.
- 在对齐期间的定位错误会降低定位和态度估计.
- 标准对齐方法在准确性和速度方面面临着挑战.
研究的目的:
- 为旋转惯性导航提出一种新的反向对齐方法.
- 通过使用组亲属属性和高速计算来加速和完善对齐过程.
- 为了提高INS初始对齐的精度和速度.
主要方法:
- 利用群亲属属性和高速计算.
- 采用反向导航和李群理论.
- 在地球中心的地球同步坐标框架中推导出左不变误差模型.
- 整合前向和反向卡尔曼过以实现快速对齐.
主要成果:
- 与标准方法相比,最大误差和循环误差概率 (CEP) 降低了60%.
- 精度提高了7.2%和20%比传统的组亲缘对齐.
- 在2.5小时的车载测试中,在各种初始失调角度中演示了快速,精确的对齐.
结论:
- 新的反向对齐方法为现代高精度惯性导航提供了显著的好处.
- 该方法在初始对齐中实现了卓越的准确性和速度.
- 对于需要高精度的旋转惯性导航应用有效.
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