Modeling and control of a fixed-wing UAV powered by solar energy: An electric array reconfiguration approach

Grano-Romero, C.; García-Juárez, Mercedes; Guerrero-Castellanos, J.F.; Guerrero-Sánchez, W. F.; Ambrosio, Roberto; Mino‐Aguilar, Gerardo

doi:10.1109/ciep.2016.7530730

Cited by 10 publications

(2 citation statements)

References 8 publications

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“…Достаточно перспективным направлением в решении задач энергопотребления дронов является использование солнечных батарей на борту [11][12][13][14][15]. Как отмечается в работе [16], эффективность процесса превращения солнечной энергии в электроэнергию зависит от двух факторов: эффективность самого процесса физического преобразования оп-тических лучей Солнца в электроэнергию и соблюдение угловых соотношений для обеспечения попадания в фотоэлементы прямых солнечных лучей под прямым углом.…”

Section: аннотация статья посвящена оптимизации использования солнечн...unclassified

Issues of Optimizing the Use of Solar Panels for Uav Power Supply

Aslanova¹

2022

Gorn. oborud. èlektromeh.

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Section: аннотация статья посвящена оптимизации использования солнечн...unclassified

Issues of Optimizing the Use of Solar Panels for Uav Power Supply

Aslanova¹

2022

Gorn. oborud. èlektromeh.

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“…A high-fidelity, low-order power model for electric, fixed-wing UAVs was developed [52] and subsequently integrated into the uavEE emulation environment and the propulsion system component optimization tool. Previous works have separately looked at aircraft power modeling [103][104][105][106][107][108] and propulsion system modeling [109][110][111][112][113] with varying degrees of assumptions and verification. Compared to existing works, the propulsion power model developed provides a more holistic approach to UAV propulsion power modeling and has been tested under realistic flight conditions (described below).…”

Section: Electric Aircraft Power Consumption Modelmentioning

confidence: 99%

A Cyber-Physical Prototyping and Testing Framework to Enable the Rapid Development of UAVs

2022

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In this work, a cyber-physical prototyping and testing framework to enable the rapid development of UAVs is conceived and demonstrated. The UAV Development Framework is an extension of the typical iterative engineering design and development process, specifically applied to the rapid development of UAVs. Unlike other development frameworks in the literature, the presented framework allows for iteration throughout the entire development process from design to construction, using a mixture of simulated and real-life testing as well as cross-aircraft development. The framework presented includes low- and high-order methods and tools that can be applied to a broad range of fixed-wing UAVs and can either be combined and executed simultaneously or be executed sequentially. As part of this work, seven novel and enhanced methods and tools were developed that apply to fixed-wing UAVs in the areas of: flight testing, measurement, modeling and emulation, and optimization. A demonstration of the framework to quickly develop an unmanned aircraft for agricultural field surveillance is presented.

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