Response analysis of UTHM’s airship
Response of airship owing to deflection angle of elevator, rudder and vectored thrust during trimmed equilibrium flight can be computed by solving the airship equations of motion. In this study, the linearised decoupled airship equations of motion were used and the solution was computed with the aid...
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| Main Authors: | , , |
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| 格式: | Conference or Workshop Item |
| 出版: |
2008
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| 主题: | |
| 在线阅读: | http://eprints.uthm.edu.my/2244/ http://eprints.uthm.edu.my/2244/1/ME_ID_0358.pdf |
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