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A Novel Algorithm of Posture Best Fit based on Key Characteristics for Large Components Assembly

机译:基于关键特征的大型零件装配姿态最佳拟合新算法

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摘要

Measurement and variation control of geometrical Key Characteristics (KCs), such as flatness and gap of joint faces, coaxiality of cabin sections, is the crucial issue in large components assembly from the aerospace industry. Aiming to control geometrical KCs and to attain the best fit of posture, an optimization algorithm based on KCs for large components assembly is proposed. This approach regards the posture best fit, which is a key activity in Measurement Aided Assembly (MAA), as a two-phase optimal problem. In the first phase, the global measurement coordinate system of digital model and shop floor is unified with minimum error based on singular value decomposition, and the current posture of components being assembly is optimally solved in terms of minimum variation of all reference points. In the second phase, the best posture of the movable component is optimally determined by minimizing multiple KCs’ variation with the constraints that every KC respectively conforms to its product specification. The optimal models and the process procedures for these two-phase optimal problems based on Particle Swarm Optimization (PSO) are proposed. In each model, every posture to be calculated is modeled as a 6 dimensional particle (three movement and three rotation parameters). Finally, an example that two cabin sections of satellite mainframe structure are being assembled is selected to verify the effectiveness of the proposed approach, models and algorithms. The experiment result shows the approach is promising and will provide a foundation for further study and application.
机译:几何关键特性(KC)的测量和变化控制,例如接合面的平整度和间隙,机舱截面的同轴度,是航空航天工业中大型组件组装中的关键问题。为了控制几何KC并获得最佳的姿态拟合,提出了一种基于KC的大型零件装配优化算法。这种方法将姿势最佳拟合(这是测量辅助组件(MAA)中的一项关键活动)视为两阶段最优问题。在第一阶段,基于奇异值分解,将数字模型和车间的全局测量坐标系统一为具有最小误差的状态,并根据所有参考点的最小变化来最佳地解决组件的当前姿态。在第二阶段,通过将多个KC的变化减到最小,并在每个KC分别符合其产品规格的约束条件下,最佳地确定可移动部件的最佳姿态。提出了基于粒子群算法(PSO)的两阶段最优问题的最优模型和处理过程。在每个模型中,每个要计算的姿势都被建模为6维粒子(三个运动和三个旋转参数)。最后,选择一个将卫星大型机结构的两个机舱部分组装在一起的示例,以验证所提出的方法,模型和算法的有效性。实验结果表明该方法是有前途的,将为进一步的研究和应用提供基础。

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