YU Rongrong, YU Chencheng, WANG Xiaoyang, YU Longqi, TAN Xu, JIANG Luhua
纸质出版:2018
移动端阅览
于荣荣,於陈程,王晓阳,于龙岐,谭旭,姜禄华. 一种高精度冗余质量质心测试方法研究[J]. 航空制造技术, 2018, 61(3): 83-89.
YU Rongrong, YU Chencheng, WANG Xiaoyang, YU Longqi, TAN Xu, JIANG Luhua. Research on High Precision Redundant Mass and Gravity Center Measure Method[J]. Aeronautical Manufacturing Technology, 2018, 61(3): 83-89.
于荣荣,於陈程,王晓阳,于龙岐,谭旭,姜禄华. 一种高精度冗余质量质心测试方法研究[J]. 航空制造技术, 2018, 61(3): 83-89. DOI: 10.16080/j.issn1671-833x.2018.03.083.
YU Rongrong, YU Chencheng, WANG Xiaoyang, YU Longqi, TAN Xu, JIANG Luhua. Research on High Precision Redundant Mass and Gravity Center Measure Method[J]. Aeronautical Manufacturing Technology, 2018, 61(3): 83-89. DOI: 10.16080/j.issn1671-833x.2018.03.083.
针对传统质量质心测试方法测试精度相对不高、系统容错性差的问题,设计了一种高精度冗余质量质心测试方法。该方法对测量单元进行在线标定,软件根据传感器测量值自动选择标定系数,对系统进行质量和质心修正,从而消除传感器的非线性误差;根据精测的产品安装误差,软件自动进行质心测试结果的补偿,降低被测件安装的横移和偏斜影响,进而提高质量和质心的测量精度;通过硬件系统的备份设计和软件系统的数据共享,实现系统交叉冗余,提高系统的可靠性。最后,经实测验证,系统的质量测量误差优于0.05%,质心测量误差±1mm,且冗余切换简单方便。
The precision of traditional mass and gravity center measure method is relatively low and the system fault tolerance is not high. This paper presents a high precision redundant measure method for mass and gravity center. The method could make on-line calibration for the measurement unit
and the software could automatically select the calibration coefficient with respect to the measurement value of sensors to correct the mass and gravity center value
so as to eliminate the nonlinear error of the sensors. The software can automatically compensate the measurement result of the gravity center according to the installation error of the payload so that the misalignment and deflection effect of installation can be reduced and the measurement accuracy of the mass and gravity center can be improved. The system reliability is enhanced based on the realization of cross redundancy through the hardware system’s redundant design and the software system data sharing. The method has passed the actual tests
its mass measurement error is better than 0.05%
and its gravity center measurement error is less than ±1mm
at the same time the mass and gravity center redundancy switching function of the system has been verified.
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