郑州机械研究所有限公司, 河南 郑州 450052
收稿:2022-01-22,
网络出版:2023-07-19,
纸质出版:2023-05-31
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杨洪涛, 卢志辉, 孙浩智, 等. 三轴转动惯量的振复摆与扭摆法协同测量比例法[J]. 兵工学报, 2023,44(5):1513-1520.
Hongtao YANG, Zhihui LU, Haozhi SUN, et al. Collaborative Proportional Method for Measuring Triaxial Moment of Inertia Based on Vibration Compound Pendulum and Torsion Pendulum[J]. Acta Armamentarii, 2023, 44(5): 1513-1520.
杨洪涛, 卢志辉, 孙浩智, 等. 三轴转动惯量的振复摆与扭摆法协同测量比例法[J]. 兵工学报, 2023,44(5):1513-1520. DOI: 10.12382/bgxb.2022.0055.
Hongtao YANG, Zhihui LU, Haozhi SUN, et al. Collaborative Proportional Method for Measuring Triaxial Moment of Inertia Based on Vibration Compound Pendulum and Torsion Pendulum[J]. Acta Armamentarii, 2023, 44(5): 1513-1520. DOI: 10.12382/bgxb.2022.0055.
空间飞行体在进行三轴转动惯量测量时需要分别沿3个正交方位做圆周摆动
为减少方位调整次数
提出基于振复摆与扭摆法的协同测量比例法。描述了该方法的测量机构
推导了比例法全因计算公式和近似计算公式;对该方法进行了误差分析
并与扭摆法进行了对比;采用模拟件作为测量对象
对提出的测量方法进行了实验研究。实验结果表明:
J
z
/J
y
小于1.02时
协同比例法的全因计算和近似计算精度基本相同且与扭摆法基本相当;
J
z
/J
y
大于1.02时
只能采用协同比例法全因计算公式
同时该方法解决了带翼飞行体三轴转动惯量测量的难题;协同比例法与前期提出的协同差值法组成了完整的测量体系
可以满足一定类型的回转体和带翼异形体三轴转动惯量测量需求。
A body moving in space needs to do circular swing along three orthogonal directions respectively during the measurement of its triaxial moment of inertia. To reduce the number of azimuth adjustment
a coollaborative proportional method for measuring the triaxial moment of inertia based on vibration compound pendulum and torsion pendulum is proposed. The equipment structure is described
and the full-parameter calculation formula and approximate calculation formula of the proposed method are given. Error analysis is done to this method and a comparison is made with the torsion pendulum method. Simulators are used as the measurement object
and the proposed method is experimentally studied. The experimental results indicate that: the computational results of the two formulas are basically the same when
J
z
/J
y
is less than 1.02; when
J
z
/J
y
is greater than 1.02
only the full-parameter calculation formula can be used
which can also solve the problem of triaxial measurement of the moment of inertia of winged flying bodies; the proposed method and the collaborative difference method previously developed constitute the complete measurement system
which can meet the requirements of certain types of revolving body and heteromorphic body with wings for the triaxial measurement of moment of inertia.
卢志辉 , 孙浩智 , 王和 , 等 . 三轴转动惯量的直立振复摆与圆周扭摆协同测量方法 [J/OL ] . 兵工学报 , 2021 [2022-01-06 ] . DOI: 10.12382/bgxb.2021.0383 https://dx.doi.org/10.12382/bgxb.2021.0383 . DOI: 10.12382/bgxb.2021.0383 http://doi.org/10.12382/bgxb.2021.0383
LU Z H , SUN H Z , WANG H , et al. The collaborative measuring method of triaxial moment of inertia based on vertical vibration compound pendulum and circular torsion pendulum [J/OL ] . Acta Armamentarii , 2021 [2022-01-06 ] . DOI: 10.12382/bgxb.2021.0383 https://dx.doi.org/10.12382/bgxb.2021.0383 . (in Chinese) DOI: 10.12382/bgxb.2021.0383 http://doi.org/10.12382/bgxb.2021.0383
KLAUS L . Comparison of two experiments based on a physical and a torsion pendulum to determine the mass moment of inertia including measurement uncertainties [J ] . Measurement Science Review , 2017 , 17 ( 1 ): 9 - 18 . DOI: 10.1515/msr-2017-0002 http://doi.org/10.1515/msr-2017-0002 https://www.sciendo.com/article/10.1515/msr-2017-0002 https://www.sciendo.com/article/10.1515/msr-2017-0002 To determine the mass-moment-of-inertia properties of devices under test with particularly small mass moments of inertia (some 10−4 kg m2), two measurement set-ups based on different measurement principles were developed. One set-up is based on a physical pendulum, the second set-up incorporates a torsion pendulum. Both measurement set-ups and their measurement principles are described in detail, including the chosen data acquisition and analysis. Measurement uncertainty estimations according to the Guide to the Expression of Uncertainty in Measurement (GUM) were carried out for both set-ups by applying Monte Carlo simulations. Both set-ups were compared using the same three devices under test. For each measurement result, the measurement uncertainties were estimated. The measurement results are compared in terms of consistency and the resulting measurement uncertainties. For the given devices under test, the torsion pendulum set-up gave results with smaller measurement uncertainties compared to the set-up incorporating a physical pendulum.
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CHE Y , LI Z G , CHEN L H , et al. Development and error analysis of an inspecting system for measuring the rotational inertia of bullets [J ] . Acta Armamentarii , 2000 , 21 ( 1 ): 87 - 89 . (in Chinese) An instrument for measuring the rotational inertia of various Dullets and rifle grenades with precision is introduced. In this measuring instrument, a double suspension structure is adopted, and an optoelectronic timing system is used to extract the information of the periods of torsional-oscillation of the measured bullet. The data is processed by the measuring system consisting of MCS-51 series of monolithiccomputers, and the measured results are displayed on displayer LED. In this paper, the working principle of the instrument is expounded, the relevant formulae are derived, and the main factors affecting precision discussed. Precision of the instrument is analysed quantitatively. Experimental results and measuring precision are given.
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卢志辉 , 支余吉 . 转动惯量标准件标准值的不确定度研究 [C ] ∥全国计量测试技术学术交流会论文集 . 北京 : 中国计量测试学会 , 2016 : 256 - 261 .
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张心明 , 王凌云 , 刘建河 , 等 . 复摆法测量箭弹转动惯量和质偏及其误差分析 [J ] . 兵工学报 , 2008 , 29 ( 4 ): 450 - 453 . 基于复摆原理,阐述了箭弹的质偏和转动惯量的测量方法及装置,推导出了质偏和转动惯量的计算公式。对影响测量精度的因素进行了分析。给出测量结果的不确定度计算公式,在假定各测量参数误差为正态分布条件下,导出了测量结果的极限误差计算公式。同时还进行了实例计算和实验测试。结果表明,用复摆法测量弹箭的质偏和转动惯量是可行有效的,其测量精度可满足工程实际要求。该方法采用刀口支承,且在测试中工装简单,便于操作,特别适用于中小弹体的质偏和转动惯量的测量。
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张心明 , 王德民 , 李俊烨 , 等 . 基于复摆测量法阻尼对转动惯量的影响分析 [J ] . 长春理工大学学报(自然科学版) , 2018 , 41 ( 4 ): 54 - 59 .
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GABL R , DAVEY T , NIXON E , et al. Accuracy analysis of the measurement of centre of gravity and moment of inertia with a swing [J ] . Applied Sciences , 2021 , 11 ( 12 ): 5345 . DOI: 10.3390/app11125345 http://doi.org/10.3390/app11125345 https://www.mdpi.com/2076-3417/11/12/5345 https://www.mdpi.com/2076-3417/11/12/5345 Floating devices under wave and current loads are typically designed based on numerical methods followed by a validation with experimental investigations. This allows an independent check due to the comparison of two different modelling approaches based on different assumptions. At an early stage of the project, numerical simulations are based on theoretical (ideal) values of the centre of gravity (CG) and moment of inertia (MI). The building process of a scaled model results very often in a requested simplification of certain parts, which can influence the CG and also the MI of the scaled model. Knowing those discrepancies allows us to improve the comparability of both approaches but the measurement of those values is connected with either a higher uncertainty or a high level of effort. A significant improvement of such measurements can be reached by the deployment of a specific experimental set-up. This paper presents the classification of the newly designed swing with a high accuracy inertial inclinometer, which was verified by the marker-based motion capturing system. The achieved experiences are useful for the future use of the set-up as well as similar investigations. The comparison with the theoretical values for the swing as well as an example model showed very good agreements and a high accuracy of few millimetres for the CG and an error smaller 1% for MI.
卢志辉 , 孙志扬 , 李祥云 , 等 . 高精度质心测量方法研究 [J ] . 兵工学报 , 2009 , 30 ( 12 ): 1748 - 1752 . 质心测量对于空间飞行器至关重要,新型武器的研制对质心测量精度的要求不断提高。将传统的天平原理与旋转轴结合,利用传感器技术,设计了一种新型质心测量机构,提出了一种能够明显提高质心测量精度的测量方法。描述了具体测量机构的主体结构,给出了机构的测量原理、测量方法,并进行了机构对于质心测量的误差分析。结合测量设备研制,进行了误差估算,理论估算的结果最大误差为0.023 mm.采用标准样件的方法进行了实验验证,具体测量数据显示,最大误差为0.020 mm.结果表明此测量方法理论分析计算与实验结果具有较好的一致性,并达到了较高的测量精度。已采用该方法成功地研制出系列高精度测量设备,配用于相关领域。
LU Z H , SUN Z Y , LI X Y , et al. Research on high precision measurement of centroid [J ] . Acta Armamentarii , 2009 , 30 ( 12 ): 1748 - 1752 . (in Chinese)
张磊乐 , 武艺泳 , 时永华 . 基于立式旋转平衡系统的惯性积测试方法研究 [J ] . 计量学报 , 2020 , 41 ( 12A ): 124 - 128 .
ZHANG L L , WU Y Y , SHI Y H . Research on the method of measuring inertial product based on vertical Rotating balance system [J ] . Acta Metrologica Sinica , 2020 , 41 ( 12A ): 124 - 128 . (in Chinese)
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