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全加速度计惯性测量的优化设计及仿真分析 被引量:13

OPTIMIZATION DESIGN AND SIMULATION OF ACCELEROMETER-BASED INERTIAL MEASUREMENT UNIT
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摘要 基于炮弹的几何结构及运动特点 ,设计了一种十二加速度计组合的无陀螺惯性测量方案用于测量弹体运动时的角速度和线加速度 .计算机仿真分析显示这种测量方案直接解算的是弹体运动角速度 ,并可以有效地消除重力加速度分量对解算弹体运动角速度及线加速度的影响 .这种惯性测量技术使惯性测量系统结构简单化 ,并有可能降低成本 ,对提高现有常规武器的性能有重大的意义 . Based on the projectile's geometry structure and movement characteristics, a non gyroscope inertial measurement technique using twelve linear accelerometers for the angular rate measurement and linear acceleration is presented. The simulation shows that the angular rate of moving projectile can be calculated directly by using this kind of measurement unit and the influence of the gravity acceleration on calculating angular rate and acceleration can be eliminated effectively. This accelerometer array inertial measurement technology can simplify the structure of the inertial measurement system and reduce the cost possibly. It is important to improve the performance of present conventional weapon.
出处 《弹道学报》 CSCD 北大核心 2003年第4期12-16,59,共6页 Journal of Ballistics
关键词 加速度计 惯性测量 角速度 线加速度 仿真 accelerometer, inertial measurement, angular rate,acceleration, simulation
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参考文献4

  • 1任思聪.实用惯导系统原理[M].北京:宇航出版社,1992.156-167.
  • 2陆元九.陀螺仪和惯性导航原理.北京:科学出版社,1964
  • 3Authony S H. Rotational measurement techniques using linear accelerometers. Proceeding of the 23rd International Instrumentation Symposium. 1977. 349- 354
  • 4Harkins T E, Brown T G. Practicability issues in deriving angular rates from accelerometer data for the2.75-inch MK66 rocket. 18th International Symposium on Ballistics. San Anionio, 1999. 113- 119

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