Demonstrates a systematic pathway for developing high-power converters for aviation applications.
This paper presents a structured end-to-end design and development methodology for a 150 kW DC–DC boost converter intended for fuel-cell-propelled aircraft. The proposed workflow progresses from requirements capture and device specification through system modelling, scaled prototyping, and software design, enabling early validation of performance and control, specific to aerospace fuel-cell systems. Detailed electromechanical design, component selection, and model-based testing are integrated with custom hardware development, software integration, and equipment-level testing to ensure robustness and scalability. The methodology culminates in construction and Technology Readiness Level (TRL) testing, demonstrating a systematic pathway for delivering high-power, aviation-grade power converters suitable for electrified propulsion architectures.
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Ibrahim et al. (2026) studied this question.
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