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...
| मुख्य लेखक: | Nogoud, Yasser Abdullah Mahjoub |
|---|---|
| स्वरूप: | थीसिस |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
2017
|
| विषय: | |
| ऑनलाइन पहुंच: | http://eprints.utm.my/81628/1/YasserAbdullahMahjoubPFKM2017.pdf |
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समान संसाधन
-
Structural design improvement of unmanned aerial vehicle wing
द्वारा: Kanesan, Gunasegaran
प्रकाशित: (2014) -
Propeller locations study on delta-winged unmanned aerial vehicle (UAV) model
द्वारा: Kasim, Khushairi Amri
प्रकाशित: (2017) -
Autorotation performance of unmanned aerial vehicle helicopter using rectangular and quadratic blades
द्वारा: Mat Ali, Mohamed Sukri
प्रकाशित: (2007) -
The development of autopilot system for an unmanned aerial vehicle (UAV) helicopter model
द्वारा: Shamsudin, Syariful Syafiq
प्रकाशित: (2007) -
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द्वारा: Mazlan, Mohd. Farizal Firdaus
प्रकाशित: (2017)