2009
DOI: 10.1007/978-3-642-10284-4_15
|View full text |Cite
|
Sign up to set email alerts
|

Nonlinear Landing Control for Quadrotor UAVs

Abstract: Abstract. Quadrotor UAVs are one of the most preferred type of small unmanned aerial vehicles because of the very simple mechanical construction and propulsion principle. However, the nonlinear dynamic behavior requires a more advanced stabilizing control and guidance of these vehicles. In addition, the small payload reduces the amount of batteries that can be carried and thus also limits the operating range of the UAV. One possible solution for a range extension is the application of a mobile base station for… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2013
2013
2015
2015

Publication Types

Select...
2
1

Relationship

1
2

Authors

Journals

citations
Cited by 3 publications
(3 citation statements)
references
References 8 publications
0
3
0
Order By: Relevance
“…Some examples include work presented by Lange in [ 47 ] where a visual system is used to estimate a vehicle position relative to a landing place. In [ 48 , 49 ], a decomposition of a quadrotor control system to an outer-loop velocity control and an inner-loop attitude control system is proposed. In this work, the landing controller consists of a linear altitude controller and a nonlinear 2D-tracking controller.…”
Section: Related Workmentioning
confidence: 99%
“…Some examples include work presented by Lange in [ 47 ] where a visual system is used to estimate a vehicle position relative to a landing place. In [ 48 , 49 ], a decomposition of a quadrotor control system to an outer-loop velocity control and an inner-loop attitude control system is proposed. In this work, the landing controller consists of a linear altitude controller and a nonlinear 2D-tracking controller.…”
Section: Related Workmentioning
confidence: 99%
“…Some examples are the work presented by Lange in Lange et al (2008) where the visual system is used to estimate a vehicle position relative to a landing place. Voos (2009), Voos andBouAmmar (2010) propose a decomposition of a quadrotor control system in an outer-loop velocity control and an inner-loop attitude control system. In which the landing controller consists of a linear altitude controller and a nonlinear 2D-tracking controller.…”
Section: Introductionmentioning
confidence: 99%
“…is the vector of generalized torques applied to the vehicle [85], [151]. These features are typically found in commercially-available multicopters and flight controllers [75].…”
Section: Uav Modelmentioning
confidence: 99%