Helicopter Flight Control and Nonlinear Simulation
碩士 === 國立成功大學 === 航空太空工程學系 === 87 === The purpose of this thesis is to design helicopter flight control system to improve stability, maneuverability, and agility of a helicopter. First, the linear mathematical model of a helicopter is established from nonlinear, 6 D.O.F. dynamic equation. Then, mode...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/49582345943310633151 |