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舰载机进近减速运动及下滑速度的双站测量
引用本文:郁涛. 舰载机进近减速运动及下滑速度的双站测量[J]. 上海交通大学学报, 2011, 45(3): 429-432
作者姓名:郁涛
作者单位:(中国电子科技集团公司 第五十一研究所, 上海 201802)
摘    要:应用多普勒频移分析了舰载机进近下滑时的运动规律,证明在匀速下滑时,由多普勒变化率为零的条件即能得出比例导引律;证明了在等比减速下滑时相邻多普勒变化率是近似相等的.然后,基于舰载机进近下滑是一个减速运动的事实,提出了在运动平台上实时探测舰载机进近下滑角和下滑速度的工程方案.与现有的多站测量方式不同,通过利用测向所引入的角度,由多普勒频移方程即可在位置参数未知时直接导出求解舰载机速度矢量的解析式.误差分析表明,如能使航母的速度测量误差均方根小于0.1 m/s,则速度测量误差就能小于0.1 m/s.

关 键 词:进近着陆   导引律   速度测量   多普勒定位   有源定位系统  

Retarded Motion in Approach and Glide Speed Measurement with Two-Stations for Carrier Aircraft
YU Tao. Retarded Motion in Approach and Glide Speed Measurement with Two-Stations for Carrier Aircraft[J]. Journal of Shanghai Jiaotong University, 2011, 45(3): 429-432
Authors:YU Tao
Affiliation:(The 51th Research Institute of CETC, Shanghai 201802, China)
Abstract:The motion law in approach for carrier aircraft was analyzed by applying Doppler shift.When carrier aircraft is in uniform glide motion,the proportional navigation guidance law can be derived according to the condition that Doppler changing rate tends towards zero.Then,the retarded motion at equal proportion is emphatically researched and the conclusion is obtained that adjacent Doppler changing rate tends to equal.Based on the fact that the approach for carrier aircraft must be practically a retarded motio...
Keywords:approach and landing  guidance law  speed measurement  Doppler positioning  active location system  
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