Optimal power management and mission profile for a Hybrid Aircraft

Engineering

• Aircraft 100%
• Hybrid 100%
• Power Management 100%
• Objective Function 75%
• Models 50%
• Engine 50%
• Simulators 50%
• Combustion 50%
• Power Source 50%
• Optimal Control 50%
• Fuel 50%
• Module 50%
• Energy Engineering 50%
• Flight Time 25%
• Efficiency 25%
• Degree of Freedom 25%
• Houses 25%
• Minimum Time 25%
• Limitations 25%
• Flight Envelope 25%
• Optimal Value 25%
• Maps 25%
• Battery (Electrochemical Energy Engineering) 25%
• Hybrid Powertrains 25%
• Algorithm 25%
• Powertrain 25%
• Systems Dynamics 25%
• Fuel Cell 25%
• Energy Source 25%
• Minimum Energy 25%
• Architecture 25%
• Approach Phase 25%
• Delivered Power 25%
• Energy Minimum 25%

INIS

• power 100%
• hybrids 100%
• management 100%
• aircraft 100%
• energy 50%
• fuels 33%
• combustion 33%
• optimal control 33%
• simulators 33%
• engines 33%
• control 16%
• dynamics 16%
• operation 16%
• efficiency 16%
• maps 16%
• values 16%
• mission analysis 16%
• comparative evaluations 16%
• burns 16%
• degrees of freedom 16%
• architecture 16%
• fuel cells 16%
• solutions 16%
• propulsion 16%
• algorithms 16%
• houses 16%
• energy consumption 16%
• constraints 16%

Keyphrases

• Classic Solution 33%
• Parallel Architecture 33%
• Optimal Contol 33%
• Parameter Management 33%