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  • 1  Static model identification of quartz flexible accelerometer based on PSO-BP
    SHI Youzhi FENG Renjian LI Xiaoting
    2025, 45(3):78-84. DOI: 10.11823/j.issn.1674-5795.2025.03.07
    [Abstract](318) [HTML](143) [PDF 3.16 M](838)
    Abstract:
    To improve the identification accuracy of the static model of quartz flexible accelerometer, this study proposes a static model parameter identification method based on a Particle Swarm Optimization-Back Propagation (PSO-BP) neural network. This approach addresses the local optima susceptibility of Back Propagation (BP) neural networks through Particle Swarm Optimization (PSO) integration. The neural architecture is configured according to accelerometer input-output dimensions, where the PSO's global exploration capability optimizes the initial weight for the BP network. Precision centrifuge-based calibration experiments were conducted to validate the proposed method. Experimental results demonstrate that the PSO-BP neural network exhibits significantly enhanced capability in resolving nonlinear coefficients compared to the standard BP network, achieving a reduction of the mean squared error (MSE) by two orders of magnitude, which provides technical support for advancing the development of high-precision navigation technologies in airborne inertial navigation systems.
    2  Analysis of truss structure of centrifugal composite calibration device based on ANSYS
    QIN Chaojun LIU Jingya
    2023(2). DOI: 10.11823/j.issn.1674-5795.2023.02.12
    [Abstract](714) [HTML](242) [PDF 3.30 M](806)
    Abstract:
    In order to ensure that the strength of the truss meets the application requirements of centrifugal composite calibration under the ultimate load condition of the centrifugal composite calibration device, the finite element analysis and verification test process of the truss structure were studied. ANSYS finite element analysis software was used to design the simulation process to complete the centrifugal boom truss structure analysis. The whole analysis process was described from the structure composition, model establishment, grid division, load constraint setting and other programs. By analyzing the result nephogram, it is confirmed that the stress result of truss meets the requirement of mechanical structure. The results of structural analysis are verified by the calibration test of the linear accelerometer. The results show that the structural strength of the truss meets the requirements of use, the deformation is close to the measured value, the structural analysis results are in accordance with the actual application test value, and the analysis results are reliable. The process and verification method of truss analysis can provide reference for similar truss analysis.
    3  Design of high-sensitivity low-frequency optical accelerometer
    LI Ruijun LEI Yingjun FAN Kuangchao
    2023(2). DOI: 10.11823/j.issn.1674-5795.2023.02.06
    [Abstract](975) [HTML](307) [PDF 5.64 M](1144)
    Abstract:
    In the fields of structural health monitoring, seismic monitoring, and aerospace, low-frequency micro-vibrations with frequencies below 10 Hz and amplitude less than 1 mm need to be measured accurately. The acceleration values of low-frequency micro-vibrations are on the order of mg ~ μg, while the sensitivity of existing commercial accelerometers is mostly below 0.5 V/g, which can no longer meet the requirements. In this paper, high-sensitivity low-frequency optical accelerometers is carried out. Based on the sensing principle of accelerometers, the technical requirements related to the design of low-frequency accelerometers are determined through theoretical modeling, and one-dimensional (1D), two-dimensional (2D), and three-dimensional (3D) elastic mechanisms are constructed by using leaf springs and flexible hinges as elastic elements with single and multiple seismic masses; based on high-precision optical sensing principles such as the principle of image dispersion, laser triangulation, and laser auto-collimation, a high-sensitivity optical sensing system is designed. 1D, 2D and 3D low-frequency optical accelerometers have been designed and their performance has been verified by experiments, with sensitivity better than 9 V/g and resolution better than 1 mg, which can be used for low-frequency micro-vibration measurements.
    4  Analysis of abnormal output fault of single axis pendulum accelerometers
    DANG Jing YU Zhen LIU Yu
    2023(5). DOI: 10.11823/j.issn.1674-5795.2023.05.13
    [Abstract](710) [HTML](250) [PDF 10.34 M](1212)
    Abstract:
    The oretical analysis is conducted on the typical fault problem of abnormal voltage output during the use of a certain type of single axis pendulum accelerometer. The fault tree comprehensive analysis method is used to track and analyze layers by layers, expressing the internal relationship between abnormal output voltage faults and intuitively pointing out the logical relationship between unit faults and overall faults, We have effectively summarized and summarized the problem of abnormal output voltage faults of single axis pendulum accelerometers encountered in engineering applications. Then, the cause of the fault was accurately and meticulously located, and the D4 diode positive electrode gold wire fracture in the oscillator circuit was proposed as the root cause of the accelerometer fault. The circuit gold wire fracture mechanism analysis method was incorporated, and the accuracy of this fault analysis was verified through experimental testing and improvement measures, which to some extent improved the reliability of the accelerometer. The research results can provide a certain reference for the reliable use of accelerometers.
    5  Research Status and Development Trend of MEMS Inertial Sensor
    卞玉民,胡英杰,李博,徐淑静,杨拥军
    2019, 39(4). DOI: 10.11823/j.issn.1674-5795.2019.04.06
    [Abstract](1173) [HTML](240) [PDF 1.97 M](1173)
    Abstract:
    Since the 1990s, study of MEMS inertial device became more and more popular.MEMS inertial sensors began to get a wide range of business applications . In this paper, some recent research results at home and abroad are classified and summarized, respectively for MEMS acceleration sensor, MEMS gyroscope ,MIMU(Micro Inertial Messurement Unit)and inertial microsystem of literature review and analysis, and get the conclusion of MEMS inertial sensor development trend, the future development of MEMS inertial device mainly has four directions: high precision, to adapt to the application requirements of higher precision and intelligent technology;Miniaturization for portable equipment installation; High integration to achieve multiple functional integration;High adaptability, to adapt to complex environment, to broaden the scope of application.
    6  Design of Single Axis Testing Turntable Control System
    任海燕,金挺,董青华
    2019, 39(2). DOI: 10.11823/j.issn.1674-5795.2019.02.07
    [Abstract](945) [HTML](118) [PDF 1.77 M](977)
    Abstract:
    In this paper, taking the single-axis test turntable system as the research object, the overall control scheme of the system is determined according to the technical requirements of the system function and performance, the key components are selected and matched, and the relevant mathematical model is established. At the same time, according to the dynamic test requirements of the system, the frequency domain characteristic method is used to correct the system and design the PID controller. The effectiveness of the control algorithm is proved by MATLAB simulation. At the same time, through the debugging in practical engineering, the positioning accuracy is not more than 2″, and the speed accuracy and stability are not more than 5×10-3. The operating frequency band is 10Hz and the amplitude error is less than 10%. This makes the system meet the requirements of the index and achieve the desired control effect.
    7  Coupling Effects of SINS Calibration Parameters in Discrete Calibration
    赵雪米,张蕾,李四海
    2019, 39(3). DOI: 10.11823/j.issn.1674-5795.2019.03.06
    [Abstract](1099) [HTML](127) [PDF 1.12 M](963)
    Abstract:
    Optical SINS error accumulate over time,as an error compensation technique,discrete calibration is a necessary means to improve navigation accuracy. SINS calibration parameters are mainly the scale factor、installation angle and bias, the article described IMU calibration principle, derived the transmission way of calibration parameters errors, theoretically analyzed the correlation effects of the calibration parameters, and get the following results: Bias repeatability errors have no effect on the scale factor and the installation angle calibration; Scale factor linearity and repeatability errors have no effect on the installation angle and bias calibration; Bias stability errors have effect on calibration of scale factor as well as installation angle ; Angle random walk has effect on the gyroscope three calibration parameters; Random noise has effect on the accelerometer three calibration parameters; Asymmetry of the calibration scale factor has effect on installation angle and bias of gyro;Installation angle repeatability errors have effect on bias and no effect on scale factor calibration of gyro ,and have no effect on scale factor or bias calibration of accelerometer.The conclusion is of great significance for INS performance evaluation, error allocation and device selection.
    8  Research on Measurement Uncertainty of Accelerometer Scale Factor
    于亚云,熊磊
    2018, 38(2). DOI: 10.11823/j.issn.1674-5795.2018.02.11
    [Abstract](959) [HTML](143) [PDF 2.59 M](844)
    Abstract:
    In order to solve the problem that the repetitive test results of the accelerometer scale factor have a 10-5mA/g error in the production process, the accelerometer’s static rolling four-point test in the gravity field is performed. Using the principle of accelerometer test system, the accelerometer scale factor is tested and calculated, and the measurement uncertainty of scale factor is studied. The measurement error source that affects the accelerometer scale factor is found.
    9  Research on the Calibrating Device for High Precision and Low Impact Acceleration
    孙浩琳,张大治
    2021(2). DOI: 10.11823/j.issn.1674-5795.2021.02.26
    [Abstract](797) [HTML](99) [PDF 2.41 M](1009)
    Abstract:
    This article introduces a high precision and low impact acceleration standard device based on ISO international standard. The high precision calibration of the acceleration sensor with half sinusoidal waveform is realized in the range of the peak acceleration (20~10000) m/s2 and pulse width (0.5~10) ms. This paper introduces the structure and working principle of standard device. It can realize the uncertainty of 0.5% (k=2) impact acceleration measurement through comparison with the national benchmarks for impact acceleration in the National Institute of Metrology (NIM). The device improves the accuracy of the standard device of impact acceleration. It meets the need of high precision calibration of impact accelerometers in aerospace, transportation and automobile industry.
    10  Research on the Optimal Calibration Method of IMU Based on Three-axis Turntable
    马知瑶,周一览
    2020, 40(3). DOI: doi:10.11823∕j.issn.1674-5795.2020.03.03
    [Abstract](1117) [HTML](146) [PDF 1.67 M](908)
    Abstract:
    The three-axis turntable is the key equipment of the model coefficient calibration of the inertial measurement unit. Its integrated pointing error will affect the calibration test and reduce the application accuracy of the inertial measurement unit. For practical engineering application, based on the black box analysis method, the simulation analysis and data mining are carried out, and the rule of test error caused by the integrated pointing error is studied. According to this, the optimal discrete calibration method of inertial measurement unit based on the UOT three-axis turntable is arranged. Through tests on 24 positions and 6 rotations of 5 initial states, the calibration error is restrained to the greatest extent with the shortest calibration time, and the calibration accuracy is significantly higher than the traditional method, which has important engineering application value.