过载控制导弹发射段弹道研究  

Study of Launch Way of Overload-Control Missile

作　　者：赵红超[1] 顾文锦[1] 

机构地区：[1]海军航空工程学院,山东烟台264001

出　　处：《弹箭与制导学报》2002年第2期15-18,22,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：研究了反舰导弹在机载发射方式和舰载发射方式下的发射段弹道。由于其控制系统采用过载控制技术进行设计 ,导引规律采用虚拟目标比例导引法 ,使导弹的发射方式更加灵活多样 ,而且发射后可以实现大空域机动飞行。因此 ,其适应性、突防能力。The launch trajectory of anti ship missile launched by airplane and warship is studied. Because the technology of overload control is used to design the control system, and the virtual target's proportional navigation guidance is used to design the guidance law, the launch trajectory of missile is more flexible and various, moreover, the missile can realize large-space maneuver fly. Therefore, the adaption, break ability and operation ability of the missile are built up.

关 键 词：导弹发射 弹道 机载发射 舰载发射 过载控制 虚拟目标比例导引 大空域机动 

分 类 号：TJ013[兵器科学与技术—兵器发射理论与技术]