首页 | 本学科首页   官方微博 | 高级检索  
     

欠驱动指爪机构的被动弹性元件参数优化设计
引用本文:楚中毅,赖咪,燕少博. 欠驱动指爪机构的被动弹性元件参数优化设计[J]. 航空学报, 2018, 39(1): 421370-421370. DOI: 10.7527/S1000-6893.2017.421370
作者姓名:楚中毅  赖咪  燕少博
作者单位:北京航空航天大学 仪器科学与光电工程学院, 北京 100083
基金项目:国家自然科学基金(51375034,61327809)
摘    要:
欠驱动指爪机构具有抓取不同目标物的自适应性,可满足操作任务的多样化需求。其欠驱动特性使得被动弹性元件的参数对抓取性能的稳定性和自适应能力有很大影响。若弹簧刚度选择过小,欠驱动指爪的稳定性会降低;若弹簧刚度选择过大,指爪的自适应能力会下降。因此,本文基于抓取状态平面法,对欠驱动指爪的被动弹性元件参数进行优化设计。首先,在欠驱动指爪静力学分析的基础上,建立弹簧刚度与驱动力的平衡方程。然后,通过对不同抓取模式拓扑转换的定量分析,获得欠驱动指爪与目标物之间不同的接触状态;同时为了保证稳定抓取,考虑了不同抓取模式下指爪弹性元件刚度与驱动力矩的参数匹配关系。在此基础上,基于抓取状态平面法建立被动弹性元件刚度与机构稳定区域关系的解析表达,并基于稳定区域面积最大化的思想,进行弹簧刚度的最优设计。最后,基于不同的抓取状态模型对弹簧刚度进行了优化设计,为后续欠驱动指爪机构设计和控制应用奠定理论和技术基础。

关 键 词:欠驱动指爪  弹性元件  参数优化  抓取模式  抓取状态平面  
收稿时间:2017-04-27
修稿时间:2017-08-02

Optimization design of passive elastic element parameter for underactuated gripper
CHU Zhongyi,LAI Mi,YAN Shaobo. Optimization design of passive elastic element parameter for underactuated gripper[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 421370-421370. DOI: 10.7527/S1000-6893.2017.421370
Authors:CHU Zhongyi  LAI Mi  YAN Shaobo
Affiliation:School of Instrument Science and Opto-electronics Engineering, Beihang University, Beijing 100083, China
Abstract:
The underactuated gripper is adaptive to different objects, and is expected to satisfy diverse operation tasks. Its underactuated characteristic determines that the design of passive elastic elements has a great impact on stability and adaptability of the gripper. If the spring becomes compliant, stability of the underactuated gripper will be reduced. On the other hand, if the spring becomes too stiff, adaptability of the gripper will decrease. This paper proposes a metric to design the spring stiffness for the underactuated gripper based on the grasp-state plane method. The equation for the equilibrium between spring stiffness and the driving force is established based on statics analysis. Through the transition between various grasp types, the different contact states between the underactuated finger and the object are obtained, and the matching relationship between the spring stiffness and the driving torque is considered to ensure the stable grab of different grasp types. A stable region is defined based on the grasp-state plane method, and spring stiffness is chosen by maximizing the area of the stable region. Several grasp models are given to demonstrate the effectiveness of the proposed method, providing foundation for the design and control of the underactuated gripper in future study.
Keywords:underactuated gripper  elastic element  parameter optimization  grasp type  grasp-state plane  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号