航天推进技术研究院主办
[1]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(06):5-7.
LI Peng,LIANG Shu-qiang.Study on simulator of attitude control power device[J].Journal of Rocket Propulsion,2012,38(06):5-7.
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LI Peng,LIANG Shu-qiang.Study on simulator of attitude control power device[J].Journal of Rocket Propulsion,2012,38(06):5-7.
姿控动力装置仿真模拟器研制
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年06期
页码:
5-7
栏目:
研究与设计
出版日期:
2012-12-15
- Title:
- Study on simulator of attitude control power device
- 文章编号:
- 1672-9374(2012)06-0005-03
- 分类号:
- V434-34
- 文献标志码:
- A
- 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。
- 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.
相似文献/References:
[1]赵庆华,王莉莉,刘 欣.固液混合火箭发动机在武器与航天领域的应用[J].火箭推进,2014,40(06):51.
ZHAO Qing-hua,WANG Li-li,LIU Xin.Application of hybrid rocket engine in the fieldsof weapons and space launching[J].Journal of Rocket Propulsion,2014,40(06):51.
备注/Memo
收稿日期：2012-03-08；修回日期：2012-06-12
基金项目：总装备部预研项目（2007AA705303）
作者简介：李鹏（1976—），男，工程师，研究领域为航天发动机测控技术
更新日期/Last Update:
1900-01-01