2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference (IAEAC) 2015
DOI: 10.1109/iaeac.2015.7428584
|View full text |Cite
|
Sign up to set email alerts
|

Design and implementation of twin-rotor tail-sitter UAV

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2019
2019
2024
2024

Publication Types

Select...
3
1
1

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(2 citation statements)
references
References 5 publications
0
2
0
Order By: Relevance
“…With the rapid development of UAV‐related technologies, a wide variety of UAVs have been proposed. According to the structure, UAVs can be classified into fixed‐wing UAVs [30], rotor UAVs [34], tilt‐rotor UAVs [35], tail‐sitter UAVs [36], and so forth, as shown in Figure 2.…”
Section: Classification Of Uavsmentioning
confidence: 99%
“…With the rapid development of UAV‐related technologies, a wide variety of UAVs have been proposed. According to the structure, UAVs can be classified into fixed‐wing UAVs [30], rotor UAVs [34], tilt‐rotor UAVs [35], tail‐sitter UAVs [36], and so forth, as shown in Figure 2.…”
Section: Classification Of Uavsmentioning
confidence: 99%
“…A canardmain wing-shroud propeller configuration for tailsitter was proposed and nice experimental results were presented in [4], [5]. The researchers in [6] designed a quadcopter tailsitter called VertiKUL which did not rely on control surfaces. However, most of the tailsitter aircrafts in previous studies are made with propellers or duct fans, which had low thrust and less efficiency.…”
Section: Introductionmentioning
confidence: 99%