首页> 外国专利> HIGH SPEED GYROCOMPASS ALIGNMENT VIA MULTIPLE KALMAN FILTER BASED HYPOTHESIS TESTING

HIGH SPEED GYROCOMPASS ALIGNMENT VIA MULTIPLE KALMAN FILTER BASED HYPOTHESIS TESTING

机译:通过基于多个卡尔曼滤波器的假设检验进行高速陀螺仪对准

摘要

A method of aligning a gyro-compass comprising operating at least two Kalman filters in a set of Kalman filters to generate an error correction to at least a single navigation solution in a set of navigation solutions in order to provide coarse alignment azimuth convergence. The method further comprises selecting at least one selected Kalman filter from the set of Kalman filters and at least one selected navigation solution from the set of navigation solutions, and operating the at least one selected Kalman filter and the at least one selected navigation solution to provide fine alignment convergence to a correct azimuth. The selecting is based at least in part on the generated error correction, each navigation solution includes an azimuth different from the azimuth of each other navigation solution and each navigation solution azimuth is separated by no more than two times a small angle error assumption.
机译:一种对准陀螺罗盘的方法,包括操作一组卡尔曼滤波器中的至少两个卡尔曼滤波器,以对一组导航解决方案中的至少一个导航解决方案产生误差校正,以便提供粗略的对准方位角收敛。该方法进一步包括从该组卡尔曼滤波器中选择至少一个选择的卡尔曼滤波器和从该组导航解决方案中选择至少一个选择的导航解决方案;以及操作该至少一个选择的卡尔曼滤波器和该至少一个选择的导航解决方案以提供精确对准收敛到正确的方位角。该选择至少部分地基于所产生的误差校正,每个导航解决方案包括与彼此导航解决方案的方位角不同的方位角,并且每个导航解决方案方位角相隔不超过小角度误差假设的两倍。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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