摘要
提高拖靶系统飞行速度,对于增加靶标的真实性和有效性具有显著意义。针对系统速度提升后,如何确定系统的使用边界进行了研究,分析了拖靶定高飞行工作原理,建立了拖靶、拖缆系统动力学模型,进行超低空定高飞行仿真计算,给出了拖靶提速后掠海定高飞行的使用边界。其结果直接应用于某新型拖靶的研制试验中,取得了满意的效果。
Improving the flight speed of the towed-target drone, is significant to increase the authenticity and validity of the targets.The present paper investigated the working conditions when the drone accelerated, analyzed the operating principle of height keeping control system, established the system dynamics model and simulated the calculation of ultra-low altitude flight, investigated the boundary conditions of flight control system of low level sea-skimming.The research results are directly applied to the development of new towed-target drone and has a good effect.
作者
田新锋
邓雨辰
TIAN Xin-feng;DENG Yu-cheng(Unit 92419 the PLA,Xincheng 125106,China)
出处
《指挥控制与仿真》
2018年第4期88-90,共3页
Command Control & Simulation
关键词
拖机
拖靶
拖缆
动力学模型
touting plane
tout target
towline
dynamics model