Zobrazeno 1 - 10
of 20
pro vyhledávání: '"孔 健"'
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 1/18/2025, Vol. 29 Issue 2, p419-429. 11p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 9/28/2024, Vol. 28 Issue 27, p4413-4420. 8p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 9/28/2024, Vol. 28 Issue 27, p4397-4404. 8p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 9/8/2024, Vol. 28 Issue 25, p4094-4100. 7p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 8/18/2024, Vol. 28 Issue 23, p3743-3750. 8p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu. 3/8/2024, Vol. 28 Issue 7, p1105-1111. 7p.
Publikováno v:
Chinese Journal of Tissue Engineering Research / Zhongguo Zuzhi Gongcheng Yanjiu; 10/18/2024, Vol. 28 Issue 29, p4717-4725, 9p
Publikováno v:
Special Oil & Gas Reservoirs; 2020, Vol. 27 Issue 2, p30-36, 7p
Autor:
Kung, Chien Chung, 孔健中
96
This study aims to explore the criterion of observation in modern psychiatric team’s madness observing, and to explore what is the basis of the criterion of observation. The research methods involved field observation and qualitative interv
This study aims to explore the criterion of observation in modern psychiatric team’s madness observing, and to explore what is the basis of the criterion of observation. The research methods involved field observation and qualitative interv
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/08112544057449920946
Autor:
Chien-Chun Kung, 孔健君
88
Unlike the conventional control design where aerodynamic model must be established in advance, this dissertation presents a new flight control design framework wherein nonlinear H∞ flight control allows that flight control design and aerody
Unlike the conventional control design where aerodynamic model must be established in advance, this dissertation presents a new flight control design framework wherein nonlinear H∞ flight control allows that flight control design and aerody
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/15197623232228656761