高超声速目标运动特性及其对预警系统的影响  

Kinematic performance and influence on early warning system of hypersonic targets

作　　者：郑建成 谭贤四[1] 曲智国[1] 喻晨龙[1] ZHENG Jiancheng;TAN Xiansi;QU Zhiguo;YU Chenlong(The Third Department,Air Force Early Warning Academy,Wuhan 430019,China;Unit 95246 of the People’s Liberation Army,Nanning 530007,China)

机构地区：[1]空军预警学院三系,武汉430019 [2]中国人民解放军95246部队,南宁530007

出　　处：《兵器装备工程学报》2023年第1期66-72,共7页Journal of Ordnance Equipment Engineering

摘　　要：在建立高超声速目标运动模型的基础上,采用定量比较的方式分析其与弹道导弹的飞行路径、飞行时间和机动能力,以利于对目标进行预警探测。分析表明,典型参数条件下高超声速滑翔飞行器大气层内相对低空飞行,飞行时间比弹道导弹慢数分钟,但横向机动范围达数千公里,使对其全程探测、搜索捕获和轨迹预测困难。分析结果可为反临预警体系建设提供技术支撑。Based on the establishment of a hypersonic target motion model,this paper uses a quantitative comparison to analyze its flight path,flight time and maneuvering capability with those of a ballistic missile for early warning detection of the target.The analysis shows that the hypersonic gliding vehicle flies relatively low in the atmosphere under typical parameter conditions,and its flight time is several minutes slower than that of ballistic missiles,but its cross maneuvering range reaches thousands of kilometers,making it difficult to detect,search,capture and predict its trajectory over time.The analysis results can provide technical support for the construction of anti-imminent early warning system defense.

关 键 词：高超声速滑翔飞行器 弹道导弹 运动特性 定量比较 预警体系 

分 类 号：TJ761.9[兵器科学与技术—武器系统与运用工程]