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作 者:肖博文 马泽远 鲁天宇 夏群利[1] XIAO Bowen;MA Zeyuan;LU Tianyu;XIA Qunli(School of Astronautics,Beijing Institute of Technology,Beijing 100081,China;Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109,China;Beijing Aerospace Automatic Control Research Institute,Beijing 100070,China)
机构地区:[1]北京理工大学宇航学院,北京100081 [2]上海机电工程研究所,上海201109 [3]北京航天自动控制研究所,北京100070
出 处:《系统工程与电子技术》2024年第11期3595-3604,共10页Systems Engineering and Electronics
摘 要:针对平台导引头隔离度模型在线辨识问题,提出一种改进卷积神经网络的导引头隔离度模型辨识方法,实现对不同干扰力矩以及天线罩误差等干扰参数影响下产生的隔离度模型高效辨识。首先,建立平台导引头模型,推导出隔离度传递函数,并搭建基于隔离度寄生回路的制导回路平台,获取弹体扰动下的视线角速率信息作为训练和测试数据。然后,利用卷积神经网络对视线角速率信号进行特征提取和特征降维。最后,经分类输出模型诊断结果。仿真结果表明,所提辨识方法对隔离度模型识别正确率能够达到99.7%,相较于传统方法提高了模型辨识准确率和快速在线辨识能力,具有较好的工程应用前景。To solve the problem of online identification of platform seeker disturbance rejection rate models,an improved convolutional neural network based seeker disturbance rejection rate model identification method is proposed to realize efficient identification of the model generated by different torques and radome errors.Firstly,the seeker model of the platform is established,the disturbance rejection rate transfer function is derived,the guidance loop platform based on the parasitic loop is built,and the line of sight angle rate information under the disturbance of the missile body is obtained as the training and test data.Then,convolutional neural network is used to extract and reduce the feature dimension of the line of sight angle rate signal.Finally,the model diagnosis results are output by classification.The simulation results show that the proposed identification method of disturbance rejection rate model recognition accuracy can reach 99.7%,which improves the identification accuracy and fast online identification ability compared with traditional methods,and has a good engineering application prospect.
分 类 号:TJ765.3[兵器科学与技术—武器系统与运用工程]
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