Study on simulator of attitude control power device(PDF)
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
- Issue:
- 2012年06期
- Page:
- 5-7
- Research Field:
- 研究与设计
- Publishing date:
Info
- Title:
- Study on simulator of attitude control power device
- Author(s):
- LI Peng; LIANG Shu-qiang
- Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
- Keywords:
- missileattitude power devicemissile control systemreal-time simulator
- PACS:
- V434-34
- DOI:
- -
- 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.
Last Update: 1900-01-01