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Taiwan Academic Institutional Repository >
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"yeh fu kuang"
Showing items 11-16 of 16 (1 Page(s) Totally) 1 View [10|25|50] records per page
| 國立臺灣大學 |
2002-12 |
Variable structure based nonlinear missile guidance and autopilot design for a direct hit with thrust vector control
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Yeh, Fu-Kuang; Cheng, Kai-Yuan; Fu, Li-Chen |
| 國立臺灣大學 |
2002-05 |
Nonlinear optimal sliding mode midcourse controller with thrust vector control
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Yeh, Fu-Kuang; Chien, Hsiuan-Hau; Fu, Li-Chen |
| 國立臺灣大學 |
2001-06 |
A midcourse guidance law for missiles with Thrust Vector Control
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Yeh, Fu-Kuang; Chien, Hsiuan-Hau; Fu, Li-Chen |
| 臺大學術典藏 |
2001-06 |
A midcourse guidance law for missiles with Thrust Vector Control
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Yeh, Fu-Kuang; Chien, Hsiuan-Hau; Fu, Li-Chen; Yeh, Fu-Kuang; Chien, Hsiuan-Hau; Fu, Li-Chen |
| 國立臺灣大學 |
1999-06 |
A nonlinear missile guidance controller with pulse type input devices
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Fu, Li-Chen; Tsai, Chi-Wang; Yeh, Fu-Kuang |
| 臺大學術典藏 |
1999-06 |
A nonlinear missile guidance controller with pulse type input devices
|
Fu, Li-Chen; Tsai, Chi-Wang; Yeh, Fu-Kuang; Fu, Li-Chen; Tsai, Chi-Wang; Yeh, Fu-Kuang |
Showing items 11-16 of 16 (1 Page(s) Totally) 1 View [10|25|50] records per page
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