2015 International Conference on Unmanned Aircraft Systems (ICUAS) 2015
DOI: 10.1109/icuas.2015.7152412
|View full text |Cite
|
Sign up to set email alerts
|

Modeling and simulation analysis of an unmanned tandem ducted fan vehicle with tilting system

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

0
5
0

Year Published

2016
2016
2022
2022

Publication Types

Select...
4
3

Relationship

2
5

Authors

Journals

citations
Cited by 8 publications
(5 citation statements)
references
References 16 publications
0
5
0
Order By: Relevance
“…In a previous study, 12 the thrust of the rotor was presented as a complex implicit integration, making model trimming and linearization challenging. Therefore, in this research, the primary ducted-rotor thrust is derived as an explicit expression based on the conservation theory of momentum and energy…”
Section: Primary Ducted-fan Dynamicsmentioning
confidence: 99%
See 2 more Smart Citations
“…In a previous study, 12 the thrust of the rotor was presented as a complex implicit integration, making model trimming and linearization challenging. Therefore, in this research, the primary ducted-rotor thrust is derived as an explicit expression based on the conservation theory of momentum and energy…”
Section: Primary Ducted-fan Dynamicsmentioning
confidence: 99%
“…Note that equation (12) describes the forces and moments of a single primary ducted-fan rotor. Since the rotation directions and locations (in body-fixed coordinates) of the two primary ducts are opposite, certain signs in the equations for the other primary ducted-fan rotor must be switched.…”
Section: Primary Ducted-fan Dynamicsmentioning
confidence: 99%
See 1 more Smart Citation
“…However, both simulation and experiment results demonstrate that the previous prototype exhibits poor controllability on the roll channel due to the lack of control forces and torques. 6 In this case, a tilting mechanism is introduced to produce more effective control moment. Aside from the controllability enhancement, another contribution of tilting system is to reduce the number of actuators since vanes that have been replaced require lots of servos.…”
Section: Introductionmentioning
confidence: 99%
“…flying robot to accomplish multiple missions in different stage, such as high-risk tasks inspection, disaster rescue, complex environmental investigation, and indoor anti-terrorism. Xiang et al 6 also show that sophisticated aerodynamics and control couplings in roll and yaw bring challenges to flight control system design. Meanwhile, uncertain parameters also deteriorate the performance of model-based controller.…”
Section: Introductionmentioning
confidence: 99%