A Helicopter Model for Real-Time Dynamic Simulation
碩士 === 國立臺北科技大學 === 機電整合研究所 === 91 === The purpose of this research is to build a helicopter real-time flight simulation model based on the rotor blade element method. The research consists of three parts: the rotor dynamic model, the aircraft equation-of-motion trim recursive program and the real-t...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/71736406566897151329 |