摘要
某反坦克导弹采用垂直弹射方式实现全方位快速攻击目标,使用直接力控制实现快速转弯,文中针对快速转弯问题创新性地给出了一种方法。首先对垂直发射导弹脉冲发动机的布局和建模方法进行了介绍,然后创新性地推导了快速转弯控制偏差的计算方法,并详细给出了脉冲发动机的点火策略,最后通过数学仿真验证了直接力控制快速转弯方法的可行性。
Anti-tank missile adopts the vertical ejection and the quick turn based on reaction-jet control in order to realize omnidirectional attack target, this paper innovatively presents a method of the quick turn based on reaction-jet control. First, the layout and modeling method of the pulse engine are introduced;Second, the calculation method of control deviation for quick turn is derived innovatively, and the ignition strategy of pulse engine is given in detail;Finally, the feasibility of the method of the quick turn based on reaction-jet control is verified by mathematical simulation.
作者
栗金平
曾望
张爱戈
何润林
LI Jinping;ZENG Wang;ZHANG Aige;HE Runlin(Xi’an Modern Control Technology Research Institute, Xi’an 710065, China;No.63963 Unit, Beijing 100070, China)
出处
《弹箭与制导学报》
北大核心
2019年第2期36-39,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
