6-DOF

作品数：115被引量：378H指数：10
导出分析报告
相关领域：自动化与计算机技术更多>>
相关作者：沈惠平邓嘉鸣朱石坚彭利坤邢继峰更多>>
相关机构：哈尔滨工业大学燕山大学吉林大学常州大学更多>>
相关期刊：更多>>
相关基金：国家自然科学基金国家重点基础研究发展计划中央高校基本科研业务费专项资金教育部“新世纪优秀人才支持计划”更多>>
-
在结果中检索

检索结果分析

结果分析中...
选择条件：
  • 期刊=Chinese Journal of Aeronauticsx
共 条 记 录，以下是1-3
全选清除导出
参考文献引证文献引用追踪
视图：
排序：
Influence of deformation zone length on bending radius of SS304 tubes with small diameters manufactured via free bending-based active motion被引量：1
《Chinese Journal of Aeronautics》2023年第6期420-434,共15页Shenghan HU Cheng CHENG Ali Abd EL-ATY Shuo ZHENG Xunzhong GUO Chunmei LIU Jie TAO 
supported by the National Natural Science Foundation of China(Nos:U1937206,52175328,52105360);the Opening Project of State Key Lab of Digital Manufacturing Equipment&Technology(No.DMETKF2021004);Jiangsu Province Key Research and Development Project(No.BE2019007-2);Fundamental Research Funds for the Central Universities(No.NS2021046);Ningbo"science and technology innovation 2025"major special project(No.2020Z078);Natural Science Foundation of Jiangsu Province(No.BK20200453).
In three and six-axis free-bending equipment,the deformation zone length(A)is a fixed mechanical structure parameter modified when the relevant structure is redesigned and manufactured.In this study,a six degree of fr...
关键词：Bending radius Deformation zone length 6-DOF parallel mechanism Free bending-based active motion Small diameter tube 
Error modeling and compensating of a novel 6-DOF aeroengine rotor docking equipment被引量：3
《Chinese Journal of Aeronautics》2022年第6期312-324,共13页Tianyi ZHOU Hang GAO Xuanping WANG Lun LI Qing LIU 
supported by Innovative Research Group Project of the National Natural Science Foundation of China (No. 51621064)
In the docking process of aeroengine rotor parts,docking accuracy that indicates the gaps between the end faces is strictly required.A key issue is improving docking accuracy using automated docking equipment.In this ...
关键词：Accuracy analysis Aeroengine rotor DOCKING Error compensation Error models Multi-degree-of-freedom structures 
Trajectory Planning Algorithm Based on Quaternion for 6-DOF Aircraft Wing Automatic Position and Pose Adjustment Method被引量：10
《Chinese Journal of Aeronautics》2010年第6期707-714,共8页ZhuYongguo Huang Xiang Fang Wei Li Shuanggao 
Basic Scientific Research Projects of Nanjing University of Aeronautics & Astronautics (NS 2010128)
A 6-degree of freedom （6-DOF） aircraft wing position and pose automatic adjustment method is presented to improve ARJ21 wing-fuselage connection precision and efficiency. Wing position and pose are adjusted by three...
关键词：AIRCRAFT assembly calibration position and pose adjustment trajectory planning QUATERNION 
全选清除导出
共1页<1>
检索报告 对象比较 聚类工具 使用帮助 返回顶部