Superaugmentation and stability augmentation control system for unmanned aerial vehicle
It is always a challenge to compromise between stability and controllability in the design of an aircraft. The challenge is becoming bigger in designing a flight control system of a small, light weight and low speed unmanned aerial vehicle (UAV). This type of UAV is facing a higher degree of difficu...
| 第一著者: | |
|---|---|
| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2017
|
| 主題: | |
| オンライン･アクセス: | http://eprints.utm.my/81628/1/YasserAbdullahMahjoubPFKM2017.pdf |