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...
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| 主要作者: | |
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2017
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| 主題: | |
| 在線閱讀: | http://eprints.utm.my/id/eprint/81628/1/YasserAbdullahMahjoubPFKM2017.pdf |
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