林穎裕 教授 簡介

職稱:國立成功大學航空太空工程研究所副教授
辦公室:5860
電話:886-6-2757575 ext. 63673
傳真:(06)238-9940
實驗室網頁:林穎裕老師網站

學歷

美國維吉尼亞理工暨州立大學工程科學暨力學研究所 博士 1984/09~ 1988/07
美國密希根州立大學機械工程學研究所 碩士 1982/09~ 1984/03
國立臺灣大學機械工程學系 學士

經歷

國立成功大學 航空太空工程研究所 副教授 1988/08

維吉尼亞理工暨州立 工程科學暨力學系 教學助理 1984/09 至 1988/06

密希根州立大學 機械工程學系 教學助理 1983/09 至 1984/06

吉興工程顧問公司 機械部 工程師 1980/06 至 1982/07

專長及研究領域

航空工程 , 太空工程 , 機械工程 , ,
1. , Image Processor and Fuzzy PID Controller Design for Robot-Car Intercept Mission , Journal of the Chinese Society of Mechanical Engineers , 2009 (SCI) 摘要
2. , Analysis of Roll-Yaw Control Law Applied to the Initial Attitude Acquisition of Spacecraft with Single Pitch Wheel , Journal of the Chinese Society of Mechanical Engineers , 2005 (SCI) 摘要
3. , Guidance and Nonlinear Flight Control Integrated Design Applied toUnmanned Air Vehicle , Journal of the Chinese Society of Mechanical Engineers , 2004 (SCI)
4. , Parameter Space Nonlinear Control of Rigid Spacecraft Attitude Maneuver , Journal of the Chinese Society of Mechanical Engineers , 2003 (SCI) 摘要
5. , Large-Angle Attitude Control of Spacecraft with Structure Spillover , Journal of the Chinese Society of Mechanical Engineers , 2002 (SCI) 摘要
6. , Nonlinear Control with Lyapunov Stability Applied to Spacecraft with Flexible Structures , PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING 215 , 2001 (SCI) 摘要
7. , General Attitude Maneuvers of Spacecraft with Flexible Structures," the Journal of Guidance , Journal of Guidance, Control, Dynamics , 1995 (SCI) 摘要
1. [95] 具俯仰動量輪皮米衛星初始姿態取得最佳方法研究
國科會 (95.8.1-96.7.31)
2. [93] 皮米級衛星姿態控制方法研究
國科會 (93.8.1-94.7.31)
3. [90] 無尾翼戰機動態系統與控制方法之研究(II)
國推會 (90.1.1-90.12.31)
1.Kraige, L.G. and Lin, Y.Y., 1989, "Motion Simulation and Utility Routine Software for Use in Dynamics Part I: Sophomore-Level Software," International Journal of Applied Engineering Education, Vo1.5, No.1, pp 21-29.

2.Kraige, L.G. and Lin, Y.Y., 1989, "Motion Simulation and Utility Routine Software for Use in Dynamics Part II:Upper Undergraduate/Graduate Level Software," International Journal of Applied Engineering Education, Vo1.5, No.4, pp 21-29.

3.Lin, Y.Y. and Kraige, L.G., 1989, "Enhanced Techniques for Solving the TPBVP Associated with the Optimal Attitude Control of Spacecraft," the Journal of the Astronautical Sciences, Vol.37, No.1, January-March, pp. 1-15.

4.Lin, Y.Y. and Lin, G.L., 1995, "General Attitude Maneuvers of Spacecraft with Flexible Structures," the Journal of Guidance, Control, Dynamics. Vol.18,No.2, March-April, pp.264-271.

5.Lin, Y.Y. and Lin, G.L., 2001, "Nonlinear Control with Lyapunov Stability Applied to Spacecraft with Flexible Structures," Accepted for publication by the Journal of Systems and Control Engineering.

6.Lin,Y.Y. and Lin,G.L., 2001, "Nonlinear Attitude Control of Spacecraft with Flexible Structures and Spillover Phenomenon," Revised for publication review by the Journal of Dynamic Systems, Measurement, and Control
70101台南市大學路一號自強校區 TEL:+886-6-2757575 ext. 63600
No.1, University Road, Tainan City, Taiwan FAX:+886-6-2389940
本網站由 航太系電腦室 建置管理登入
Best View: IE7.0 / 1024x768 32-bit color