...
首页> 外文期刊>IEEE Transactions on Aerospace and Electronic Systems >Optimization-based alignment for strapdown inertial navigation system: comparison and extension
【24h】

Optimization-based alignment for strapdown inertial navigation system: comparison and extension

机译:捷联惯性导航系统基于优化的对准:比较和扩展

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper, the optimization-based alignment (OBA) methods are investigated with the main focus on the vector observation construction procedures for the strapdown inertial navigation system (SINS). The contributions of this study are twofold. First, the OBA method is extended to be able to estimate the gyroscope biases coupled with the attitude based on the construction process of the existing OBA methods. This extension transforms the initial alignment into an attitude estimation problem that can be solved by using the nonlinear filtering algorithms. The second contribution is the comprehensive evaluation of the OBA methods and their extensions with different vector observations construction procedures in terms of convergence speed and steady-state estimate by using field test data collected from different grades of SINS. This study is expected to facilitate the selection of appropriate OBA methods for different grades of SINS.
机译:在本文中,研究了基于优化的对准(OBA)方法,主要侧重于捷联惯性导航系统(SINS)的矢量观测构造过程。这项研究的贡献是双重的。首先,将OBA方法扩展为能够基于现有OBA方法的构建过程来估计陀螺仪偏差和姿态。此扩展将初始对准转换为可以通过使用非线性滤波算法解决的姿态估计问题。第二个贡献是,通过使用从不同等级的SINS收集的现场测试数据,在收敛速度和稳态估计方面对OBA方法及其扩展进行了不同矢量观测构建程序的综合评估。预期这项研究将有助于为不同等级的SINS选择合适的OBA方法。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号