摘要
为了满足远程高机动性要求,提出了将冲压发动机和倾斜转弯(BTT)控制技术应用于某型地空导弹的设计方法。建立了BTT导弹三通道独立的数学模型,实现了BTT导弹自动驾驶仪的三通道独立设计,为改进和发展远程地空导弹提供了一种控制方案。
The design project of surface-to-air missiles offered in this paper which adopts a ramair engine and bank-to-turn (BTT) control technology has the property of a long range and high maneuverability. The paper is achieved the BTT missile's dynamic model which has a decoupled three channels, and designs the autopilot of the three decoupled channels with H∞ control theory. The result of the paper has provided a project of the control system for improving and developing long-range suface-to-air missiles.
出处
《飞行力学》
CSCD
北大核心
2005年第4期56-58,62,共4页
Flight Dynamics
基金
航空科学技术基金资助项目(01D53010)
关键词
倾斜转弯
自动驾驶仪
地空导弹
bank-to-turn
autopilot
surface-to-air missile