火箭推进2012，Vol.38Issue(6)：5-7,58,4.
姿控动力装置仿真模拟器研制
Study on simulator of attitude control power device
摘要
Abstract
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Key words
missile/attitude power device/missile control system/real-time simulator分类
航空航天引用本文复制引用
李鹏,梁树强..姿控动力装置仿真模拟器研制[J].火箭推进,2012,38(6):5-7,58,4.基金项目
总装备部预研项目 （）
