2020
DOI: 10.1016/j.ijhydene.2020.09.014
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Weight optimization of hydrogen storage vessels for quadcopter UAV using genetic algorithm

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Cited by 19 publications
(4 citation statements)
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“…using the approach proposed by Angel et al 28 for geometric rectification of UAV image data. The ability to collect near-continuous data from a hovering UAV is restricted by the battery life, which is generally limited to 20–60 min for most quadcopters, although new hydrogen fuel cells for UAVs have extended hovering times to over 2 h 29 . To overcome the limitations of battery capacity, tethering of UAVs via an attached power line is a potential solution for extending hovering capabilities in future studies 30 .…”
Section: Discussionmentioning
confidence: 99%
“…using the approach proposed by Angel et al 28 for geometric rectification of UAV image data. The ability to collect near-continuous data from a hovering UAV is restricted by the battery life, which is generally limited to 20–60 min for most quadcopters, although new hydrogen fuel cells for UAVs have extended hovering times to over 2 h 29 . To overcome the limitations of battery capacity, tethering of UAVs via an attached power line is a potential solution for extending hovering capabilities in future studies 30 .…”
Section: Discussionmentioning
confidence: 99%
“…using the approach proposed by Angel et al [26] for geometric recti cation of UAV image data. The ability to collect near continuous data from a hovering UAV is restricted by the battery life, which is generally limited to 20-60 min for most quadcopters, although new hydrogen fuel cells for UAVs have extended hovering times to over 2 hours [27]. To overcome the limitations of battery capacity, tethering of UAVs via an attached power line is a potential solution for extending hovering capabilities in future studies [28].…”
Section: Discussionmentioning
confidence: 99%
“…The comparison of this method to that performed by Roh [93] indicated that the two methods reduced the weight of Type IV cylinders by 9.8 and 11.2%, respectively. Lee et al [95] optimized the winding layer and winding angle of Type IV cylinders based on the genetic algorithm, and this reduced the weight of hydrogen cylinders by 23.79%, thus increasing the hovering time of a quadrotor drone with a 650 W fuel cell by 17.73%, which is 37.85% longer than the hovering time of the battery-powered drone with the same power.…”
Section: High-pressure Gas Cylinders and Hydrogen Regulatorsmentioning
confidence: 99%