期刊文献+

惯性系统火箭橇试验过载曲线设计方法

Acceleration Simulation of Missile for IMU in Sled Testing
在线阅读 下载PDF
导出
摘要 利用火箭橇试验提供的大过载、高频震动,可以模拟出惯性系统真实的工作环境。讨论了一种基于搜索算法的火箭橇大过载实验设计方法,对惯性系统火箭橇安装方法和火箭橇橇体建模作了系统讨论;根据典型过载曲线,作出合理假设,给出了仿真结果,验证了方法的合理性。 Provided the use of rocket sled test a major overload, high-frequency vibration, inertial system can simulate the real working environment. Discussion of a search algorithm based on the skis than the rocket containing the experimental design method, the inertial system and the installation of a rocket sled rocket sled sled system modeling were discussed; in accordance with a typical load curve, to make reasonable assumptions, the results of the simulation, validation the method is reasonable.
出处 《装备制造技术》 2009年第9期22-23,31,共3页 Equipment Manufacturing Technology
关键词 火箭橇试验 惯性系统 大过载 sled testing inertial measurement device acceleration
  • 相关文献

参考文献1

二级参考文献3

  • 1Peterson Eldon E, Lwrence Capt. S. Sled testing of the MX ADP/AIRS system[C]. Holloman AFB, New Mexico: Tenth Biennial Guidance test Symposium Proceedings, 1981.
  • 2AFDTC-TP-92-38, 6585^th Test Group. Honeywell advanced guidance technology advanced inertial measurement unit laboratory and sled test[C]. Holloman AFB, New Mexico 88330-5000: Guidance Test Division, 1992-08.
  • 3Mixon L C, Evans C B, Gilliam W L. Rail roughness study of Holloman high speed rocket sled test track[R]. AD A105778, 1981-09.

共引文献16

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部