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不同传感器精度下的地形辅助导航系统性能评估
引用本文:赵龙,颜廷君.不同传感器精度下的地形辅助导航系统性能评估[J].北京航空航天大学学报,2013,39(8):1016-1019.
作者姓名:赵龙  颜廷君
作者单位:北京航空航天大学飞行器控制一体化技术重点实验室,北京,100191;北京航空航天大学飞行器控制一体化技术重点实验室,北京,100191
基金项目:国家自然科学基金资助项目(41274038,61039003);航空基础科学基金资助项目(20100851018);中国航天创新基金资助项目(CASC201102)
摘    要:为完成地形辅助导航系统的传感器选型以及改进地形匹配算法和地形辅助导航系统可靠性的研究,开展了传感器精度对地形匹配概率的影响研究.针对不同的地形,分析了高度表误差、速度误差和航向角误差对地形匹配概率的影响,并根据实际要求通过仿真计算确定地形匹配系统中各传感器的误差范围.利用丘陵、山地和高山地等大量地形数据进行测试验证,仿真结果表明:在地形匹配概率大于90%时,速度误差小于2.2 m/s,航向角误差小于0.6°,高度表噪声标准差小于16.4 m.

关 键 词:地形辅助导航  匹配概率  传感器精度  系统性能
收稿时间:2012-08-09

Performance evaluation of a terrain-aided navigation system under different accuracy of sensor
Zhao Long;Yan Tingjun.Performance evaluation of a terrain-aided navigation system under different accuracy of sensor[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(8):1016-1019.
Authors:Zhao Long;Yan Tingjun
Institution:Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:In order to select the type of the sensor, improve the terrain-aided navigation(TAN) algorithm, and do research on the reliability of the TAN system, the influence of the sensor's accuracy on the match probability was studied in the TAN. Based on different terrain, the factors that impact on match probability were analyzed, which are barometer error, radar altimeter error, velocity error, and heading angle error. The error range of sensors was determined by simulation computing in practical system. A simulation experimentation was implemented by using the digital map of hills, mountains and high mountains. The simulation results shows that TAN system allows the velocity error<2.2 m/s, the heading angle error<0.6° and standard deviation of altimeter noise<16.4 m, when the match probability is > 90%.
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