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激光平台型导引头跟踪控制技术与炮兵火箭应用研究
引用本文:牛春峰,王荣梅,王潇.激光平台型导引头跟踪控制技术与炮兵火箭应用研究[J].计算机测量与控制,2022,30(9):125-132.
作者姓名:牛春峰  王荣梅  王潇
作者单位:中国兵器工业导航与控制技术研究所,,
摘    要:基于激光平台型导引头的工作机理和控制原理,分析了导引头视线角速度噪声和隔离度的影响因素并提出提高隔离度的措施;构建了基于力矩干扰的激光平台型导引头模型、频带模型和隔离度模型,搭建测试平台,通过对比分析仿真、测试和某火箭弹飞行试验结果,验证了上述因素对频带和隔离度的影响,经测试和飞行试验验证,提高隔离度和频带的措施合理可行,达到了降低视线角速度噪声的目的,可满足野战火箭环境下工程应用的要求。

关 键 词:激光平台型导引头  隔离度  力矩干扰  视线角速度噪声  炮兵火箭
收稿时间:2022/6/23 0:00:00
修稿时间:2022/7/10 0:00:00

The Application Research of the Laser Platform-type Seeker Tracking Control Technology on Artillery Rocket
Abstract:Based on the working mechanism and control principle of the laser platform-type seeker, this paper analyzes the influencing factors of the angular velocity noise and disturbance rejection rate,and puts forward measures to improve the disturbance rejection rate. A laser platform lead model and disturbance rejection rate model based on torque disturbance are constructed, and a test platform was built. Through comparative and analysis of simulation and test results, the factors affecting of disturbance rejection rate are verified, and the effectiveness of measures to improve disturbance rejection rate and reduce the angular velocity noise of sight are verified, that can meet the requirements of engineering applications in rocket environments.
Keywords:Laser semi-active seeker  Disturbance rejection rate  Disturbing moment  Angular velocity noise  Artillery rocket  
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