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

机译:太阳能固定翼无人机的建模和控制:电子阵列重构方法

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摘要

In this paper the mathematical model of a fixed-wing UAV powered by solar energy is presented, the aim is to show the performance of a longitudinal control for this UAV, using successive loop closure. Also is presented a methodology for a photovoltaic (PV) array reconfiguration allowing the load to be matched and delivering the maximum power. The system model the longitudinal controller together with the PV reconfiguration methodology is validated using numerical simulations.
机译:在本文中,提出了一种由太阳能驱动的固定翼无人机的数学模型,目的是通过连续闭环展示该无人机的纵向控制性能。还提出了一种用于光伏(PV)阵列重新配置的方法,该方法允许负载匹配并提供最大功率。使用数值模拟验证了纵向控制器和PV重新配置方法的系统模型。

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