The Design and Analysis for Autopilot Control and Stability mentation of UAV
碩士 === 中華技術學院 === 飛機系統工程研究所 === 97 === Flight control systems are required for aircrafts which are unstable and unable to meet aviation quality specification. The flight control system for a general aircraft consists of three control loops: pitch, roll, and yaw. The output for the transfer function...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2009
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| Online Access: | http://ndltd.ncl.edu.tw/handle/07840379476607438541 |