| 惯导／GNSS／罗兰C／航姿系统组合导航方案 |
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| 引用本文： | 吴美平,胡小平.惯导／GNSS／罗兰C／航姿系统组合导航方案[J].中国惯性技术学报,2000,8(3):12-16. |
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| 作者姓名： | 吴美平 胡小平 |
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| 作者单位： | 国防科技大学,湖南,长沙,410073 |
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| 摘 要： | 为保证飞行器的导航精度及可靠性，采用了惯导/GNSS/罗兰C/航姿系统的组合导航。该组合导航采用开环组合方式，将多系统导航信息在计算机中进行综合，提高导航信息精度。仿真试验结果说明，所设计的组合导航系统是可行的，能满足任务要求。
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| 关 键 词： | 组合导航 惯导 GNSS 罗兰C 航姿系统 |
| 修稿时间： | 2000-05-28 |
Integrated Navigation of INS/GNSS/LoranC/HARS |
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| WU Mei-ping,HU Xiao-ping.Integrated Navigation of INS/GNSS/LoranC/HARS[J].Journal of Chinese Inertial Technology,2000,8(3):12-16. |
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| Authors: | WU Mei-ping HU Xiao-ping |
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| Abstract: | The integraed navigation system of inertial navigation system(INS),GNSS,LoranC,and HARS are used to ensure the aerocraft navigation precision and reliability.The integrated system adopts an integrated mode of openloop which combines navigation information of many systems in computer to improve navigation precision.The test result shows that the integrated navigation system is feasible,and meets the requirments of the task. |
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| Keywords: | integrated navigation INS GNSS LoranC HARS |
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