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	Design and implementation of agent-based robotic system for agile manufacturing: A case study of ARIAC 2021 期刊论文 OAI收割 Robotics and Computer-Integrated Manufacturing, 2022, 卷号: 77, 页码: 1-7 作者: Wan GX(万广喜); Dong XT(董晓婷); Dong QW(董青卫); He YP(贺云鹏); Zeng P(曾鹏) \| 收藏 \| 浏览/下载：45/0 \| 提交时间：2022/04/23 Agent Agility Manufacturing Robotics
	Investigating the effect of social media application on firm capabilities and performance: The perspective of dynamic capability view 期刊论文 OAI收割 Journal of Business Research, 2021, 期号: 139, 页码: 510–519 作者: YuYe; Qionglei Yu; Yongjun Zhenga; Yi Zheng \| 收藏 \| 浏览/下载：11/0 \| 提交时间：2022/03/01 Adaptability,Agility, Dynamic Capability,Firm Performance,Social Media, Application Time-based Performance
	SGCMG design and time accumulation error analysis (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Mechatronic Science, Electric Engineering and Computer, MEC 2011, August 19, 2011 - August 22, 2011, Jilin, China Xu W. 收藏 \| 浏览/下载：21/0 \| 提交时间：2013/03/25 SGCMG receives much concern due to the performance of its excellent torque output on spacecraft control it has been applied to large foreign spacecraft already but late start and only limited to configurations and steering law study in China. Based on the needs of agility small satellites this article explained the method of SGCMG principle prototype design and proposed the influence on SGCMG output torque precision generated by time accumulation error first time. This article provided a new idea for future SGCMG project development and had good reference value for SGCMG research. 2011 IEEE.
	Analysis of inertia dyadic uncertainty for small agile satellite with control moment gyros (EI CONFERENCE) 会议论文 OAI收割 2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China 作者: Zhang L.; Zhang L.; Sun Z. 收藏 \| 浏览/下载：20/0 \| 提交时间：2013/03/25 With the increasing demands for the agility of the next earth imaging satellite control moment gyro (CMG) is considered to be the most suitable actuator because of its torque amplification capability. However a CMG system may introduce uncertainty of inertia dyadic to a satellite's attitude control system. The uncertainty is negligible for large space vehicles but it has not been tested whether it can be ignored for small agile satellites. How to model the CMG system inertia dyadic varying with gimbal angles and what influence it will put on the performance of attitude control system haven't been test accurately as well. All of them are dealt with mathematically and accurately in this paper. This paper firstly gives mathematic descriptions of the inertia dyadic of the 4-CMG pyramid configuration system varying with gimbal angles and then designs a variable structure control law for small agile satellite using CMGs. Finally numerical simulation suggests that the inertia dyadic variation of a 4-CMG pyramid configuration system is approximately centesimal of the total inertia dyadic of the satellite and that the designed variable structure control law is of good robust performance for an example of large-angle attitude maneuver despite of the variation of the inertia dyadic. 2010 IEEE.
	An Agility Performance Indicator System Based on Business Process for Manufacturing Enterprise 会议论文 OAI收割 International Conference on Agile Manufacturing (ICAM 2003), Beijing, China, December 4-6, 2003 作者: Lv Y(吕毅); Xue JS(薛劲松); Gao Z(高展) 收藏 \| 浏览/下载：27/0 \| 提交时间：2012/10/16 Manufacturing enterprise Agility performance measurement Business process Performance indicator
	An efficient algorithm for computing object poses in a modular fixture or gripper 期刊论文 OAI收割 Journal of Robotic Systems, 2002, 卷号: 19, 期号: 3, 页码: 99–114 作者: Qian, Wen Han; Qiao, Hong 收藏 \| 浏览/下载：15/0 \| 提交时间：2016/12/07 agility metrics enterprise agility agile manufacturing fuzzy logic