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作 者:徐航[1] 白晓东[1,2] 张喜涛 Xu Hang;Bai Xiaodong;Zhang Xitao(China Airborne Missile Academy,Luoyang 471009,China;National Key Laboratory of Air-based Information Perception and Fusion,Luoyang 471009,China)
机构地区:[1]中国空空导弹研究院,河南洛阳471009 [2]空基信息感知与融合全国重点实验室,河南洛阳471009
出 处:《航空兵器》2024年第1期66-70,共5页Aero Weaponry
摘 要:针对传统抗干扰性能评估指标集中在导弹制导系统层面,无法满足导引系统抗干扰性能评估的问题,本文在分析抗干扰过程中制导系统内部误差传递原理的基础上,基于导引系统的测量误差,提出了基于视线角速度精度的导引系统抗干扰性能评估指标,从而在导引系统研制过程中,能够及时对其抗干扰性能进行评估。由于视线角速度精度在外场试验中不易测量,为了提高该指标的测试效率,基于比例导引制导原理,给出了视线角速度精度的简化计算方法,并针对非比例导引制导场景,给出了利用识别时间对视线角速度精度进行等效测试的方法。外场数据测试结果表明,该指标能够反映导弹在不同场景下的抗干扰性能,具有一定合理性。In response to the problem that traditional anti-interference performance evaluation indices are concentrated at the level of missile guidance systems,which cannot meet the anti-interference performance evaluation of guidance systems,based on the analysis of the internal error transmission principle of guidance systems during the anti-interference process and the measurement error of guidance systems,this paper proposes a guidance system anti-interference performance evaluation index based on line of sight angular velocity accuracy,so as to evaluate its anti-interference performance timely in the development process of guidance systems.Due to the difficulty for measurement of the line-of-sight angular velocity accuracy in field experiments,in order to improve the testing efficiency,a simplified calculation method for line-of-sight angular velocity accuracy is proposed based on the principle of proportional guidance.Furthermore,for non proportional guidance scenarios,an equivalent testing method for line-of-sight angular velocity accuracy using recognition time is given.The results of field data testing indicate that the indices can reflect the anti-interference performance of missile in different scenarios,and this method has certain rationality.
关 键 词:视线角速度 抗干扰 导引系统 识别时间 评估指标 导弹
分 类 号:TJ765[兵器科学与技术—武器系统与运用工程]
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