Genetic Algorithm Enabled Multi-Objective Design Optimization of Current Source Converters for Turboelectric Aircraft Propulsion

Engineering

• Aircraft 100%
• Aircraft Propulsion System 50%
• Aviation 50%
• Current Source 100%
• Design 100%
• Design Objective 50%
• Design Optimization 100%
• Design Process 50%
• Energy Conservation 50%
• Energy Efficiency 50%
• Energy Engineering 50%
• Engineering 50%
• Genetic Algorithm 100%
• Larger Quantity 50%
• Optimisation Problem 50%
• Pareto Front 50%
• Power Conversion System 50%
• Power Density 50%
• Reliability 100%