SiC-Based Bidirectional Cuk Converter With Differential Power Processing and MPPT for a Solar Powered Aircraft

被引:46
作者
Diab-Marzouk, Ahmad [1 ]
Trescases, Olivier [1 ]
机构
[1] Univ Toronto, Dept Elect & Comp Engn, Toronto, ON M5S 3G4, Canada
基金
加拿大创新基金会; 加拿大自然科学与工程研究理事会;
关键词
Aerospace; DC-DC converter; differential power processing (DPP); electric aircraft; lightweight; photovoltaic converters; PHOTOVOLTAIC ARRAYS; POINT TRACKING; BURST MODE; PERFORMANCE;
D O I
10.1109/TTE.2015.2505302
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
A silicon-carbide (SiC)-based dc-dc converter is developed for the solarship, a manned solar aircraft for supply delivery in remote locations. The concept of differential power processing (DPP) is utilized to realize a high-efficiency lightweight converter that performs maximum power point tracking (MPPT) to transfer power from the aircraft's wing-mounted solar array to the high-voltage lithium-battery bus. The isolated Cuk topology is augmented with an unfolder to achieve four quadrant operation and minimize the worst-case processed power. A small-signal model is derived for control design, and it is shown that the compensation strategy differs significantly based on the operating mode. The 2.7-kW prototype is verified at a high frequency (200 kHz), high efficiency (> 98%), small mass (0.604 kg), and uses no electrolytic capacitors. MPPT operation is verified on a 376-V commercial solar installation. The DPP Cuk converter is promising for emerging solar aerospace applications.
引用
收藏
页码:369 / 381
页数:13
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