NMPC-PID based new control structure design for altitude and attitude stabilization of non-linear quad-rotor type unmanned aerial vehicles (UAV)
Quad-rotor typed unmanned aerial vehicles (UAV) are rotorcraft that has four propellers. In this design there are two arms and each arm has two propellers at their end.. It has complex controlling structure, that is why this rotorcraft is overall non-linear in nature. Hence, it creates a lot of dif...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Thesis |
| 語言: | English |
| 主題: | |
| 在線閱讀: | http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/44117/1/p.1-24.pdf http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/44117/2/full%20text.pdf |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|