Development of an Attitude Control System for Quad-Rotor UAV with Fuzzy Control
碩士 === 國立虎尾科技大學 === 航空與電子科技研究所 === 102 === In this paper, the fuzzy controller of flight attitude is developed and implemented for the quad-rotor UAV system. The attitude control system is designed by sensing the signals of accelerometers and inertial navigation system and adjusting the motor speed...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
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| Online Access: | http://ndltd.ncl.edu.tw/handle/n6wts2 |