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大气折射对电视制导导弹定位精度的影响分析
引用本文:刘燕,袁莹涛,郭翔,索涛,李玉龙,于起峰.大气折射对电视制导导弹定位精度的影响分析[J].航空学报,2018,39(12):322248-322248.
作者姓名:刘燕  袁莹涛  郭翔  索涛  李玉龙  于起峰
作者单位:1. 西北工业大学 航空学院, 西安 710072;2. 陕西省冲击动力学及工程应用重点实验室, 西安 710072;3. 国防科技大学 航天科学与工程学院, 长沙 410073
基金项目:国家自然科学基金(11772268,11522220,11272267,11527803,11602201)
摘    要:为了提高电视制导导弹的定位精度,有必要研究大气折射效应的影响。基于大气折射率模型,采用高精度的4阶Runge-Kutta光线追迹方法,以定位误差和俯角误差为大气折射效应的评价标准,建立了电视制导导弹大气折射误差模型,并通过探空仪实测大气参数验证了模型的有效性以及精度测试验证了算法的可靠性。基于该模型,仿真分析了不同发射高度和俯角对定位精度的影响规律。研究结果发现:高海拔时,基于三段模型的大气折射误差要小于其他模型;相同高度下导弹发射的视在俯角扩大10倍,由大气折射造成的定位误差和俯角误差将分别缩小1 000倍和10倍;5 km高度、视在俯角为30°时的定位误差已减小到2 m以内。研究结果表明,该方法可以辅助电视制导导弹的设计,对提高其精确打击能力具有重要意义。

关 键 词:电视制导导弹  大气折射  光线追迹  4阶Runge-Kutta  定位误差  俯角误差  
收稿时间:2018-04-27
修稿时间:2018-06-09

Influence analysis of atmospheric refraction on location of television guiding missiles
LIU Yan,YUAN Yingtao,GUO Xiang,SUO Tao,LI Yulong,YU Qifeng.Influence analysis of atmospheric refraction on location of television guiding missiles[J].Acta Aeronautica et Astronautica Sinica,2018,39(12):322248-322248.
Authors:LIU Yan  YUAN Yingtao  GUO Xiang  SUO Tao  LI Yulong  YU Qifeng
Institution:1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;2. Shannxi Key Laboratory of Impact Dynamics and its Engineering Application, Xi'an 710072, China;3. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Abstract:In order to improve the positioning accuracy of TV guided missiles, the atmospheric refraction effect was studied. Based on atmospheric refractive model, the high-precision fourth-Order Runge-Kutta ray-tracing method was presented to estimate the atmospheric refraction effect. The location error and angle error were proposed as evaluation parameters to establish atmospheric refraction error model of TV guided missiles. The precision test was performed to verify the reliability and accuracy of ray tracing calculations and atmospheric parameters from radiosonde show the validity of model. Simulations were performed based on five models in the altitude range of 0.5-5 km (0.5 km step length) and in the bow angle range of 2°-45°. The results show that the atmospheric refraction error based on the three-segment model is smaller than that of other models at high altitude. At the same altitude, the bow angle increases 10 times, and the location error and angle error decreases approximately 1000 and 10 times respectively. When the bow angle is 30° the location error is less than 2 m. This method can assist the design of TV guided missile and is significant to availably improve accurately fighting capacity.
Keywords:television guiding missiles  atmospheric refraction  ray-tracing  fourth-order Runge-Kutta  location error  angle error  
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