大型结构调姿机构末端重心校准方法
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1.南京工业职业技术大学航空工程学院南京210023; 2.北京机械工业自动化研究所有限公司北京100032

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TH166

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江苏省高等学校自然科学研究项目(24KJB460020)、南京工业职业技术大学引进人才科研启动基金(YK23-03-02)资助


Terminal centroid calibration method for large component adjustment mechanism
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1.School of Aeronautical Engineering, Nanjing University of Industry Technology,Nanjing 210023, China; 2.Beijing Research Institute of Automation for Machinery Industry Co., Ltd, Beijing 100032, China

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    摘要:

    调姿机构末端重心位置是影响调姿机构动力学模型的重要参数,不准确的重心位置导致调姿驱动力偏离理想状态,造成调姿机构变形,最终影响装配特征的对准精度。针对大型结构的精准柔顺定位需求,提出一种考虑球铰关节摩擦力矩的调姿机构末端重心位置校准方法。首先,通过构建调姿机构的动力学模型,并采用数值仿真方法分析了重心偏差对调姿内力的影响;接着,基于坐标系间力和力矩的变换原理,建立考虑球铰摩擦力矩的重心解算模型,同时采用M估计样本一致性(MSAC)算法优化重心参数,以减小传感器随机误差和定位器运动误差的影响;然后,采用蒙特卡洛方法研究随机误差和重心校准策略对重心校准精度的影响,结果表明传感器测量误差是影响重心校准精度的主要随机因素,提高末端最大旋转角度和称重次数可提升校准精度,且当称重次数≥6次时MSAC算法的优化效果显著。最后,在实验室环境下进行调姿机构末端的重心校准和翼身结构调姿对准实验。实验结果表明所提重心校准方法能显著提高末端重心校准的精度,采用所提重心校准方法获得的重心参数进行驱动力规划,调姿内力的平均值下降了56.0%,叉耳孔的同轴度偏差平均降低了47.6%,验证了所提重心校准方法能有效降低调姿内力并提高装配特征的对准精度。

    Abstract:

    The terminal centroid of the large component adjustment mechanism is an important parameter that affects its dynamic model. An inaccurate centroid position can cause the adjustment driving force to deviate from the ideal state, resulting in deformation of the adjustment mechanism and ultimately affecting the alignment accuracy of the assembly features. To meet the requirements for high-precision and compliant positioning of large-scale structures, this paper proposes a centroid position calibration method for the end of the posture adjustment mechanism that accounts for the friction torque of spherical joints. Firstly, a dynamic model of the posture adjustment mechanism is established, and the influence of centroid deviation on the internal force of posture adjustment is analyzed using numerical simulations. Secondly, based on the principle of force and torque transformation between coordinate systems, a centroid calculation model that incorporates the friction torque of ball joints is constructed. Meanwhile, the M-estimate sample consensus (MSAC) algorithm is adopted to optimize centroid parameters, so as to reduce the impact of random sensor errors and motion errors of positioners. Then, the Monte Carlo method is used to study the effects of random errors and centroid calibration strategies on calibration accuracy. The results show that sensor measurement error is the main random factor affecting the accuracy of centroid calibration. Increasing the maximum rotation angle of the terminal and the number of weightings can improve calibration accuracy, and the optimization effect of the MSAC algorithm is significant when the number of weightings is ≥ 6. Finally, centroid calibration of the mechanism terminal and posture adjustment alignment experiments of wing-body structures are conducted in a laboratory environment. The experimental results indicate that the proposed centroid calibration method can significantly improve the calibration accuracy of the terminal centroid. Using the centroid parameters obtained by this method for driving force planning, the average internal posture adjustment force is reduced by 56.0%, and the average coaxiality deviation of the fork ear holes is decreased by 47.6%, verifying that the proposed centroid calibration method can effectively reduce the internal forces of posture adjustment and improve the alignment accuracy of assembly features.

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褚文敏,周蒯,滕利臣.大型结构调姿机构末端重心校准方法[J].仪器仪表学报,2025,46(11):367-381

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  • 在线发布日期: 2026-02-09
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