Design of a Solar Power Management System for an Experimental UAV

doi:10.1109/TAES.2009.5310303

機構典藏 > College of Engineering > Graduate Institute & Department of Aerospace Engineering > Journal Article > Item 987654321/53763

Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/53763

Title:	Design of a Solar Power Management System for an Experimental UAV
Authors:	Shiau, Jaw-Kuen;Ma, Der-Ming;Yang, Pin-Ying;Wang, Geng-Feng;Gong, Jhij-Hua
Contributors:	淡江大學航空太空工程學系
Date:	2009-10
Issue Date:	2013-03-20 16:25:58 (UTC+8)
Publisher:	Piscataway: Institute of Electrical and Electronics Engineers
Abstract:	本論文探討無人飛行載具太陽能電力電源管理系統之設計，目的為提供機載電腦系統之電力需求。此電源管理系統主要包含太陽能電池與最大功率追蹤、電池管理與電力轉換三級。太陽能電池與最大功率追蹤，主要目的是用來收集太陽能，並且追蹤太陽能板隨著溫度與照度而改變的最大功率點，以得到最佳效率。電池管理監視及控制鋰高分子聚合物電池之充∕放電流程管理。電力轉換則將供電電壓轉換為+5V與±12V，以提供系統及機載電腦之所需。 The design of a solar power management system (SPMS) for an experimental unmanned aerial vehicle (UAV) is summarized. The system will provide power required for the on-board electronic systems on the UAV. The power management system mainly consists of the maximum power point tracking (MPPT), the battery management, and the power conversion stages. The MPPT stage attempts to obtain the maximum power available from the solar cell panels. The battery management stage monitors and controls the charge and discharge processes of the Li-ion polymer battery modules. The last stage is for power conversion that consists of dc/dc synchronous buck converters to generate +5 V and +12 V powers for the on-board computers and other electronic circuitries.
Relation:	IEEE Transactions on Aerospace and Electronic Systems 45(4), pp.1350-1360
DOI:	10.1109/TAES.2009.5310303
Appears in Collections:	[Graduate Institute & Department of Aerospace Engineering] Journal Article

Files in This Item:

File	Size	Format
index.html	0Kb	HTML	277	View/Open

Loading...