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Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/ (Rudolph, Devan Jessie Aaron.)
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Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/
Author:
Rudolph, Devan Jessie Aaron. Search Author in Amazon Books

Publisher:
University of Kyrenia,
Edition:
2023.
Classification:
TL685
URL:

http://docs.neu.edu.tr/library/9665817163.pdf
Additional related names
Detailed notes
    - Master (Thesis).
    - Uncludes references (58-59 p.)
    - In English.
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Items (2)
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Status
Library
Section
9665817163
Item available
University of Kyrenia Grand Library1st Floor (TL685 .R83 2023)
Reference Section
9669535162
Item available
University of Kyrenia Grand Library1st Floor (TL685 .R83 2023)
Reference Section

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