滑翔式空中靶标总体设计与弹道仿真  

System Design of a Glide Aerial Target and Trajectory Simulation

作　　者：丁力军[1] 张俊 辛庆伟[3] 

机构地区：[1]92493部队 [2]中国航天科技集团第九研究院 [3]海军航空工程学院接改装训练大队

出　　处：《海军航空工程学院学报》2017年第1期161-166,共6页Journal of Naval Aeronautical and Astronautical University

摘　　要：空中靶标作为一种消耗性的无人飞行器,在防空反导武器系统试验训练中具有不可或缺的重要作用,须统筹考虑其逼真性和经济性。为此,提出了滑翔式空中靶标系统发展思路与工作原理,设计了滑翔式空靶总体方案,并利用Datcom和Matlab对其滑翔供靶弹道进行了仿真分析。仿真计算表明,弹道性能满足亚音速俯冲类目标模拟供靶要求,系统具有高性能、低成本、使用安全等显著特点。As a kind of expendable UAV, aerial target plays a very important role in the test and training of the air defense weapon systems, and its fidelity and affordability should be taken into account as a whole. Therefore, the development approach and operation principle of a glide aerial target system were put forward, the system concept of the target was designed, and its glide flight trajectory was simulated and analyzed using Datcom and Matlab tools. The results of trajectory simulation indicated that the glide trajectory could meet the requirements of the subsonic diving target. The glide target possessed characteristics of high performance, low cost and operational safety.

关 键 词：滑翔式空靶 总体设计 弹道分析 

分 类 号：V211[航空宇航科学与技术—航空宇航推进理论与工程]