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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Bibliographic Details
Main Author: Nogoud, Yasser Abdullah Mahjoub (Author)
Format: Thesis
Published: 2017.
Subjects:
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