摘要
针对某超音速导弹用气动舵系统进行研究,描述了舵系统的基本结构和工作原理;对气动舵系统各组成部分进行了分析,建立了全参数舵系统工程仿真模型,并对整个舵系统数学模型进行了仿真研究。通过研究该模型可以方便的分析各个参数对舵系统性能的影响,有利于改善系统的静、动态性能,对气动舵系统的研究有重要意义。
The pneumatic rudder-control system of some type of supersonic missile is investigated. The structure and principle of rudder-control system are described. The mathematic models for each part of pneumatic rudder-control system are introduced and the whole simulation model is established. Through the investigation of the model, the effect of each parameter on system performance could be analyzed expediently. It has reference value for the investigation of pneumatic rudder-control system.
出处
《航天控制》
CSCD
北大核心
2006年第3期84-88,共5页
Aerospace Control
关键词
气动舵系统
建模
仿真
Pneumatic rudder-control system Modeling Simulation
