2018 23rd International Conference on Methods &Amp; Models in Automation &Amp; Robotics (MMAR) 2018
DOI: 10.1109/mmar.2018.8485805
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MARAAL: A Low Altitude Long Endurance Solar Powered UAV For Surveillance and Mapping Applications

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Cited by 18 publications
(11 citation statements)
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“…Payload defines the maximum amount of weight that a UAV can transport, which has a direct effect on the endurance capabilities, communication, coverage, and an operational altitude of the UAV [94]. The more payload that a UAV can carry, the more accessories can be carried.…”
Section: H Payloadmentioning
confidence: 99%
“…Payload defines the maximum amount of weight that a UAV can transport, which has a direct effect on the endurance capabilities, communication, coverage, and an operational altitude of the UAV [94]. The more payload that a UAV can carry, the more accessories can be carried.…”
Section: H Payloadmentioning
confidence: 99%
“…It is important to mention here that, for solar UAV design studies discussed in the preceding section, structural weight was quoted for very few prototypes. The most common wing structural layouts are double circular spare [16], single circular spare [7,18] and D-box [5,20,21]. Even for a specific structural layout, there can be many variations in the numbers of ribs, stringers, the diameter and thickness of spares and the thickness of ribs and skin.…”
Section: Structural Massmentioning
confidence: 99%
“…For the current study, the materials considered are 3 k carbon fiber, light density balsa wood and plywood. Several prototypes such as MARAAL [16], Sky-Sailor [5], AtlantikSolar [7], SunSailor [33] and LEEUAV [20] also used carbon fiber and balsa wood as primary materials.…”
Section: Structural Massmentioning
confidence: 99%
“…The experimental results on charging capabilities for an engineering ground model with test UAVs in [154] showed excellent efficiency for more than 24 h of continuous operation. Meanwhile, the solar-based UAV prototypes developed in [155], [156] demonstrated a continuous flight potential of up to 28 h. In [157], Dwivedi et al experimented with a day flight for a solar-based UAV on April 1, 2017, where the test time was from 9:30 to 18:00. From these measurement results, it is recognized that the generated power is less than the power required by the UAV system from approximately 15:30 to 17:10.…”
Section: A Energy Refillsmentioning
confidence: 99%
“…Commercial T-UAVs with the various supported maximum tethered lengths up to 130 m as well as the capability of unlimited flight duration [59], [136] The significant out-performance is achieved when using the help from T-UAVs' energy replenishment perspectives compared to U-UAVs [148] Inductive charging A planar coil misalignment to recharge UAV batteries and reduce weight of UAV onboard components [149] Fast wireless charging prototype for HAP components at 450-W power recharging in the 85-kHz band [150] Magnetic resonance charging Powering UAV batteries and solving the problems of endurance [151] An optimal design for UAVs to maintain stable energy transmission efficiency [154] Solar EH More than 24 h of continuous operation for UAVs [156] Up to 28 h of continuous UAV operation [157] The impact of daytime hours of flight for a solar-powered UAV [158] The impact of light intensity and ambient temperature on solar EH efficiency of UAVs [159] The impact of temperature and solar irradiance intensity on solar-based UAVs for optimal operation [160] Joint optimal path scheduling and power allocation for a UAV with PV cells [161] Joint optimal 3-D position, power, and subcarrier for a solar-powered UAV [162] Joint optimal solar EH, power consumption, onboard energy storage, and users' QoS requirements [153] The intelligent power mechanism using ML regarding the flight altitude of solar-based UAVs [163] Thermal EH Harvesting the waste thermal energy from a UAV processor to prolong flight time [164] Wind EH A dynamic soaring technique to harvest wind energy and reduce the UAVs energy consumption [166] Vibration EH A piezoelectric harvester integrated into UAV platforms to extend the flight duration [167] Solar and vibration EH An onboard UAV hybrid model to support higher energy efficiency [172] EH and RF wireless charging Prolongation of the continuous operating lifetime of ABSs via combination frameworks [170] RF wireless charging Replenishing batteries via an integrated rectifier antenna with approximately 5-W transmission power [171] More than 77% energy conversion efficiency via power on the receiving side of ABSs [173] Joint optimal ABSs' trajectory and the recharging station power [174] At least six laser beaming directors are required to ensure the ABSs coverage probability per...…”
Section: Refmentioning
confidence: 99%