Failure analysis and finite element simulation for structural systems in an unmanned aerial vehicle
In this paper, failure analysis of an unmanned aerial vehicle (UAV) has been conducted through failure mode and effects analysis (FMEA) and finite element (FE) simulation. For FMEA, a system is broken down into subsystems, and possible failures are considered for each subsystem. Each failure is then...
محفوظ في:
المؤلفون الرئيسيون: | Wang, Bing, Ng, Poh Huat, Elhadidi, Basman Mohamed Nabil Ahmed Khairat, Ang, Hui Shan, Moon, Seung Ki |
---|---|
مؤلفون آخرون: | School of Electrical and Electronic Engineering |
التنسيق: | Conference or Workshop Item |
اللغة: | English |
منشور في: |
2020
|
الموضوعات: | |
الوصول للمادة أونلاين: | https://hdl.handle.net/10356/141497 |
الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة
-
VERTICAL REPLENISHMENT BY UNMANNED AERIAL VEHICLES.
بواسطة: LIU PEIDONG
منشور في: (2015) -
Additive manufacturing in unmanned aerial vehicles (UAVs): Challenges and potential
بواسطة: Goh, G. D., وآخرون
منشور في: (2018) -
Navigation of Unmanned Aerial Vehicles in GPS-denied Environments
بواسطة: CUI JINQIANG
منشور في: (2015) -
Investigation and experiment of radar systems in unmanned aerial vehicles-I
بواسطة: Suren, S
منشور في: (2024) -
JOINT TRAJECTORY AND COMMUNICATION DESIGN FOR UNMANNED AERIAL VEHICLE
بواسطة: ZHANG JINGWEI
منشور في: (2020)