52nd IEEE Conference on Decision and Control 2013
DOI: 10.1109/cdc.2013.6760951
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Formation control of UAVs with a fourth-order flight dynamics

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Cited by 35 publications
(12 citation statements)
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“…Table I defines the above symbols. Note that linearized quadrotor models on the horizontal plane can be expressed as a forth-order system [8].…”
Section: A Modeling a Uavmentioning
confidence: 99%
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“…Table I defines the above symbols. Note that linearized quadrotor models on the horizontal plane can be expressed as a forth-order system [8].…”
Section: A Modeling a Uavmentioning
confidence: 99%
“…We have been studying cooperative control problems for multi-vehicle systems [6]- [9] with particular focus on solving formation control problems using a consensus algorithm. We expressed the UAV dynamics on the horizontal plane as a fourth-order system and the dynamics in the vertical direction as a second-order system separately, then proposed two consensus-based control algorithms for a multi-UAV system to cooperatively fly in formation on the horizontal plane and in the vertical direction [8], [9]. Using these two consensusbased cooperative control algorithms, UAVs can fly in formation in three-dimensional space.…”
Section: Introductionmentioning
confidence: 99%
“…Most nonlinear system identification model parameters use a minimization algorithm. The UAV nonlinear model is 23…”
Section: The Model Of Uavmentioning
confidence: 99%
“…5). The layout is generated as in W j = Wo TL I j E {I, ... ,M} , (9) where W j denotes the width of marker j, decreasing from Wo. The width ratio Tw should not be too large to allow enough discriminative content between the markers, and 682 not smaller than the ratio of min and max image marker area limits to guarantee detection of at least one marker per target at a time.…”
Section: Nested Marker Designmentioning
confidence: 99%
“…In addition, quadrocopters in volve a challenging control problem due to their nonlinear dynamics. In the areas of robotics and control engineer ing, the attitude control [5], the take-off control [6], the 978 -89-93215-06-995560114/$15 ©ICROS 678 visual navigation control [7], the acrobatic control [8], the formation control [9], and others have been studied.…”
Section: Introductionmentioning
confidence: 99%