2017 6th Data Driven Control and Learning Systems (DDCLS) 2017
DOI: 10.1109/ddcls.2017.8068112
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Design and implementation of a gasoline-electric hybrid propulsion system for a micro triple tilt-rotor VTOL UAV

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Cited by 21 publications
(18 citation statements)
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“…It is a push-broom camera which provides 1024 spatial pixels and 224 spectral bands [22]. However, due to the low signal-to-noise ratio of the first and last spectral bands, they were removed (1)(2)(3)(4)(5)(6)(7)(8)(9)(10), so that 180 bands have been retained. The original image scene covers an area of 1024 × 4967 pixels, but a much shorter scene has been cropped containing the anomalies of the scene.…”
Section: A Reference Hyperspectral Datamentioning
confidence: 99%
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“…It is a push-broom camera which provides 1024 spatial pixels and 224 spectral bands [22]. However, due to the low signal-to-noise ratio of the first and last spectral bands, they were removed (1)(2)(3)(4)(5)(6)(7)(8)(9)(10), so that 180 bands have been retained. The original image scene covers an area of 1024 × 4967 pixels, but a much shorter scene has been cropped containing the anomalies of the scene.…”
Section: A Reference Hyperspectral Datamentioning
confidence: 99%
“…On one hand, a wireless power charge approach in order to reduce the stopping time [3]. On the other hand the use of alternative propulsion systems (or hybrid combinations of some of them), which alleviate the restrictions imposed by electric batteries in terms of autonomy, are attracting great attention from the scientific community [4]- [6]. Another important aspect to take into account when it comes to UAVs, being an autonomous vehicle, is the safety critical operation it implies.…”
Section: Introductionmentioning
confidence: 99%
“…In reference [24] the three different hybrid-electric power-plant configurations are considered and dynamic models are derived, with flight dynamics performance testing carried out on a UAV prototype.…”
Section: Introductionmentioning
confidence: 99%
“…A clear approach to solve the deficiencies in the quadcopter and fixed-wing UAVs would be the deployment of a hybrid design which combines the good aspects of each, thus dramatically increasing the functionality of the drone. Multiple approaches exist like the tilt-rotor [6] where the rotors can rotate between vertical and forward thrust and the tilt-wing [7] where the wings rotate along with the rotors. The tail-sitter [8] may also be considered, though it only incorporates the forward thrust motors of the fixed-wing, meaning that it is capable of VTOL but lacks any hover capability.…”
Section: Introductionmentioning
confidence: 99%