姿控动力装置仿真模拟器研制  

Study on simulator of attitude control power device

作　　者：李鹏[1] 梁树强[1] 

机构地区：[1]西安航天动力研究所,陕西西安710100

出　　处：《火箭推进》2012年第6期5-7,58,共4页Journal of Rocket Propulsion

基　　金：总装备部预研项目(2007AA705303)

摘　　要：为研究某型号导弹飞行中段的姿态控制、验证飞行试验控制系统功能,研制了姿控动力装置半实物实时仿真模拟器系统。与导弹控制系统进行的弹道模飞联合仿真试验表明,该系统功能稳定、实时性高,在仿真试验中发挥了重要作用,实现了姿控动力装置在不同工况下的半实物仿真和数字仿真功能。To research the attitude control in the mid-course flight of the missile and verify the function of the flight test control system, a semi-physical real-time simulator system for the attitude power device was developed. A co-simulation test with missile control system conducted for ballistic mode fly indicated that the system was stable wiht high real time accuracy. The attitude power device played an important role in the simulation experiment. The functions of semi-physical simulation and digital simulation of attitude power device were achieved under different working conditions.

关 键 词：导弹 姿态动力装置 导弹控制系统 实时模拟器 

分 类 号：V434-34[航空宇航科学与技术—航空宇航推进理论与工程]