首页> 外文期刊>Advances in space research >A real-time airborne terrain aided inertial navigation system and its performance analysis
【24h】

A real-time airborne terrain aided inertial navigation system and its performance analysis

机译:实时机载地形辅助惯性导航系统及其性能分析

获取原文
获取原文并翻译 | 示例
           

摘要

The current terrain aided navigation system has a shortcoming that it depends on terrain feature, so we need to select the terrain matching area and plan the flight path according to the flight mission in advance. In this paper, we present a real-time airborne terrain aided inertial navigation system. The system can plan and select the matching area online according to the heading angle and estimated position errors during aircraft flight, and adopt the appropriate terrain-aided navigation algorithm for different terrain areas and flight conditions. So it can ensure the positioning accuracy and improve the ability of carrier to maneuver at the same time. In order to verify the performance of the system, a flight simulation experiment and a real flight test are carried out, and we conduct a research on the performance of matching area planning and real-time positioning. The tests results show that the system can improve the ability of carrier to maneuver and the performance of real-time positioning. In addition, the system has a higher positioning accuracy and reliability than traditional TERCOM and SIT AN methods. The position error is less than 50 m in acquisition mode and less than 18 m in tracking mode with the terrain elevation map of 25 m-resolution.
机译:当前的地形辅助导航系统有一个缺点,即它取决于地形特征,因此我们需要选择地形匹配区域并根据飞行任务预先计划飞行路径。在本文中,我们提出了一种实时的机载地形辅助惯性导航系统。该系统可以根据航向角和估计的位置误差在线规划和选择匹配区域,并针对不同的地形区域和飞行条件采用合适的地形辅助导航算法。这样既可以保证定位精度,又可以提高运输工具的机动性。为了验证系统的性能,进行了飞行模拟实验和真实飞行测试,并对匹配区域规划和实时定位的性能进行了研究。测试结果表明,该系统可以提高舰载机的机动能力和实时定位性能。此外,该系统比传统的TERCOM和SIT AN方法具有更高的定位精度和可靠性。在具有25 m分辨率的地形高程图的情况下,在采集模式下的位置误差小于50 m,在跟踪模式下的位置误差小于18 m。

著录项

  • 来源
    《Advances in space research》 |2017年第12期|2751-2762|共12页
  • 作者单位

    Digital Navigation Center, Beihang University, Beijing 100191, China;

    Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China,Digital Navigation Center, Beihang University, Beijing 100191, China;

    Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China,Digital Navigation Center, Beihang University, Beijing 100191, China,Beijing Satellites Navigation Center, Beijing 100094, China;

    Beijing Satellites Navigation Center, Beijing 100094, China;

    School of Electrical and Information Engineering, Hunan University, Hunan 410012, China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Terrain-aided navigation; Inertial navigation; Matching area selection; Robust terrain matching algorithm;

    机译:地形辅助导航;惯性导航;配套区域选择;鲁棒的地形匹配算法;

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