摘要
介绍了助推滑翔的导弹滑翔段的特点和平衡滑翔工程定义。建立了滑翔飞行的模型,进行了仿真研究,并提出了2种最大升阻比的滑翔控制方案,即分别以高程和气动力函数式为基准的滑翔控制方案。对控制方案分别进行了仿真研究,分析了其优缺点。
At first,it introduced the characteristics of glide trajectory and engineering definition of balancing glide.Secondly,it buit a model of gliding flight,and carried on the simulation study.Finally,the two gliding control scheme of the biggest lift-drag ratio were respectively proposed,namely the height-based and aerodynamic functional-based glide control program.And it made the simulation research for the control solution,and analyzed their advantages and disadvantages.
出处
《四川兵工学报》
CAS
2011年第8期27-30,39,共5页
Journal of Sichuan Ordnance
关键词
助推滑翔导弹
优化设计
滑翔弹道
boost-glide missile
optimization design
glide trajectory
