基于传递矩阵的并联机构正向运动学求解新理论方法

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Jin Wang, Zijian Jing, Junli Guo, Tao Qin, Han Li, Xin Li, Zhenchuang Li, Fanhui Meng, Bo Qi
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引用次数: 0

摘要

柔性并联机构具有精度高、无摩擦、无缝运动等诸多优点,在精密仪器中得到广泛应用。建立该机构的运动方程对于并联机构的设计、分析、控制和仿真至关重要。虽然现有的逆运动学求解理论非常全面,但由于姿态方程的非线性性质,建立正向求解模型具有挑战性。为解决这一问题,本研究提出了一种基于传递矩阵方法的新方法来计算并联机构的正向运动学。提出的方法可用于分析平面和空间柔性机构的前向运动学和工作空间。仿真计算和实验验证了该方法的有效性。结果表明,误差约为 2%,表明了计算方法的可行性和准确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A New Theoretical Method for Solving Forward Kinematics of the Parallel Mechanisms Based on Transfer Matrix
The flexible parallel mechanism is widely utilized in precision instruments, thanks to its numerous advantages, such as high precision, frictionless operation, and seamless movements. The establishment of the motion equations for this mechanism is crucial for designing, analyzing, controlling, and simulating parallel mechanisms. While the existing inverse kinematics solution theory is comprehensive, developing a forward solution model is challenging due to the nonlinear nature of the attitude equation. To address this issue, a new method based on the transfer matrix approach is proposed in this research to calculate the forward kinematics of parallel mechanisms. The proposed method is applied to analyze the forward kinematics and workspace of both planar and spatial flexible mechanisms. Simulation calculations and experiments are conducted to verify the method’s effectiveness. The results demonstrate that the error is approximately 2%, indicating the feasibility and accuracy of the calculation method.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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