摘要
建立了 BTT 导弹的数学模型.对 BTT 导弹控制系统的耦合因素作了定性分析。用模型跟踪法进行了解耦控制器的设计。将设计结果用于某战术导弹,并对±30°扇面角发射的初始段进行了仿真计算.从结果看出,导弹速度损失小,最小射程短,机动性强.证明采用倾斜转弯控制技术对改善战术导弹的性能是有效的.
The mathematical models of BTT missile arc built up.Coupling factors of BTT missile control system is gualitatively analyzed.The decoupling controller is designed with model-following-method,and is used for a tactical missile.Then,simulation to initial launching phase of missile with±30°sector angle has been carried cut.The simulation results show that loss of missile velocity is smaller,minimum launching dis- tance is shorter,maneuverability of missile is inproved,and the method is effective for improving perform- ance of tactical missile using BTT control techniques.
出处
《战术导弹技术》
1993年第4期29-37,共9页
Tactical Missile Technology
关键词
战术导弹
控制系统
数学模型
Tactical missile
Control system
Mathematical model
Decoupling control
BTT technique
