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空天防御  2025, Vol. 8 Issue (5): 111-116    
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基于线性插值的外场试验导引头测角偏差计算方法
王文涛1,2, 任博1, 何永鹏2, 许琳朋3, 孟梁2, 周珂2
1. 空军工程大学 装备管理与无人机工程学院,陕西 西安 710051; 2. 中国人民解放军某部,甘肃 酒泉735018; 3. 中国空空导弹研究院,河南 洛阳 471009
Calculation Method for Seeker Angle Measurement Deviation in Field Tests Based on Linear Interpolation
WANG Wentao1,2, REN Bo1, HE Yongpeng2, XU Linpeng3, MENG Liang2, ZHOU Ke2
1. Equipment Management & UAV Engineering College, Air Force Engineering University, Xi'an 710051, Shaanxi, China; 2. A Unit of PLA, Jiuquan 735018, Gansu, China; 3. China Airborne Missile Academy, Luoyang 471009, Henan, China
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摘要 导弹测角(目标视线高低角、方位角)偏差评定通常在试验室内部开展,无法完全模拟温度、振动等外场环境影响,为解决传统试验室不能真实反映外场环境而无法准确评定导引头性能的问题,本文提出一种基于线性插值的外场试验导引头测角偏差计算方法,以外场试验获取的导弹、目标设备数据为研究对象,以外场试验导引头测角偏差结果计算为研究内容,对数据进行线性插值处理,使其时拍保持一致;在地面坐标系下使用线性插值后的数据建立测角偏差模型;获取目标真实视线矢量与导弹测量矢量的夹角,即空间测角偏差。本方法可为后续导弹外场试验导引头测角偏差计算提供有力参考,并与内场试验相结合,共同完成对导引头测角性能的评定。 关键词: 导引头; 线性插值; 测角偏差
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关键词 导引头线性插值测角偏差    
Abstract:The evaluation of missile angle measurement deviations (the elevation angle and azimuth angle of the target line-of-sight) is typically conducted in laboratories, where it is impossible to fully simulate the influences of external field environments, including temperature and vibration. To address the issue that traditional laboratory tests fail to actually reflect the external field environment and thus cannot evaluate the performance of seekers accurately, this paper proposes a method for calculating the angle measurement deviation of seekers in external field experiments based on linear interpolation. Focusing on the missile and target equipment data obtained from external field experiments, the research content involved calculating the seeker angle measurement deviation results from these experiments. The method first performed linear interpolation on the data to align their time frames. Secondly, a model of angle measurement deviation was established using the linearly interpolated data within the ground coordinate system. Finally, the spatial angle measurement deviation was obtained, which was the angle between the actual line-of-sight vector of the target and the measured vector of the missile. This method provides a firm reference for the subsequent calculation of seeker angle measurement deviations in missile external field experiments. Additionally, it can be combined with internal field experiments to evaluate the performance of seeker angle measurement jointly.
Key wordsseeker    linear interpolation    angular deviation
收稿日期: 2025-07-02      出版日期: 2025-10-31
ZTFLH:  V 553.2  
作者简介: 王文涛(1990—),男,硕士研究生,工程师。
引用本文:   
王文涛, 任博, 何永鹏, 许琳朋, 孟梁, 周珂. 基于线性插值的外场试验导引头测角偏差计算方法[J]. 空天防御, 2025, 8(5): 111-116.
WANG Wentao, REN Bo, HE Yongpeng, XU Linpeng, MENG Liang, ZHOU Ke. Calculation Method for Seeker Angle Measurement Deviation in Field Tests Based on Linear Interpolation. Air & Space Defense, 2025, 8(5): 111-116.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2025/V8/I5/111

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