2017 International Conference on Unmanned Aircraft Systems (ICUAS) 2017
DOI: 10.1109/icuas.2017.7991310
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A power consumption model for multi-rotor small unmanned aircraft systems

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Cited by 110 publications
(100 citation statements)
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“…We consider the UAV to be a low-altitude autonomous multi-rotor drone. The previous studies, 30,42,43 reveal that the power consumed by such a drone while in the air does 30 ). Also, we assume that after leaving for the mission, the drone stays all the time in the air, even when transferring the energy to the EDs.…”
Section: Energy Consumption and Wireless Power Transfer Modelsmentioning
confidence: 93%
“…We consider the UAV to be a low-altitude autonomous multi-rotor drone. The previous studies, 30,42,43 reveal that the power consumed by such a drone while in the air does 30 ). Also, we assume that after leaving for the mission, the drone stays all the time in the air, even when transferring the energy to the EDs.…”
Section: Energy Consumption and Wireless Power Transfer Modelsmentioning
confidence: 93%
“…1 Ground speed is the horizontal speed of an aircraft relative to the ground [33]. 2 The positioning errors of fourth-generation long-term evolution (4G LTE) network devices are typically in the range between 10 and 50 meters, depending on the adopted positioning protocol [36].…”
Section: User Location Modelmentioning
confidence: 99%
“…Here, W u = m u g 0 is the weight of the UAV, and m u and g 0 denote the mass of the UAV and the gravitational acceleration, respectively. c 1 , c 2 , c 3 , and c 4 are UAV aerodynamic power consumption parameters [33].…”
Section: F Aerodynamic Power Consumptionmentioning
confidence: 99%
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“…We can compute the energy cost of traveling from a node i to a node j, denoted e k d,total,ij , as a sum of the energy cost associated with ascending to that height, denoted e k a,ij , descending from that height, denoted e k d,ij , flying the distance between the two nodes, denoted e k t,ij , and the costs associated with performing the rendezvous maneuver (if applicable). We use the energy model described in [19] in which the authors reported results within 10% of tested quadrotors. We stress that our future analysis is not dependent on this model, but requires an energy model that is dependent on the changing mass of the quadrotor.…”
Section: Edge Energy Costs Of the Uav In Flightmentioning
confidence: 99%