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悬丝支承型加速度计静态温度模型辨识及温度补偿方法研究
引用本文:李园晴,傅山,庞秀枝.悬丝支承型加速度计静态温度模型辨识及温度补偿方法研究[J].航空计测技术,2012(5):13-17.
作者姓名:李园晴  傅山  庞秀枝
作者单位:[1]上海交通大学,上海200240 [2]中国空空导弹研究院,河南洛阳471009
摘    要:为了消除环境温度变化对悬丝支承型加速度计精度的影响,采用最小二乘法拟合建立了-50~68℃温度范围内加速度计模型系数零偏K0和标度因数K1的温度模型。由TMS320F2812 DSP和测温模块LM47172组成的硬件系统,根据温度模型对加速度计输出进行补偿后,加速度计输出的拟合均方根误差保持在10-4g数量级以内,比未采用温度补偿时提高了一个数量级,补偿效果明显。

关 键 词:悬丝支承型加速度计  零偏  标度因数  温度模型辨识  温度补偿

Study of the Identification for the Static Temperature Model and the Method for Compensating Temperature of Pendulous Accelerometer
LI Yuanqing,FU Shan,PANG Xiuzhi.Study of the Identification for the Static Temperature Model and the Method for Compensating Temperature of Pendulous Accelerometer[J].Aviation Metrology & Measurement Technology,2012(5):13-17.
Authors:LI Yuanqing  FU Shan  PANG Xiuzhi
Institution:1.Shanghai Jiaotong University,Shanghai 200240,China;2.China Airborne Missile Academy,Luoyang 471009,China)
Abstract:To eliminate the impact of temperature on accelerometer,by using the method of least square fitting,the static temperature model of the accelerometer within-50~ +68℃ has been established.The hardware system is composed of DSP(TMS320F2812) and temperature module(LM47172).After temperature compensation with the above model by the system,the magnitude of output change is 10-4g,which is better than that without temperature compensation,and the stability of the accelerometer output has a significant improvement.
Keywords:pendulous accelerometer  zero offset  scale factor  identification for temperature mode  temperature compensation
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