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

作　　者：高波[1] 牟建华[2] 王仕成[1] 肖正林[2] 

机构地区：[1]第二炮兵工程学院,陕西西安710025 [2]第二炮兵装备研究院,北京100051

出　　处：《装备制造技术》2009年第9期22-23,31,共3页Equipment Manufacturing Technology

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.

关 键 词：火箭橇试验 惯性系统 大过载 

分 类 号：V42[航空宇航科学与技术—飞行器设计]