Feasibility study of a solar powered hybrid micro-aerial vehicle

Engineering

• Feasibility Study 100%
• Solar Panel 100%
• Takeoff 100%
• Flight Time 50%
• Low Aspect Ratio Wings 50%
• Fixed Wings 50%
• Preliminary Analysis 50%
• Flux Density 50%
• Quadcopter 50%
• Health Monitoring 50%
• Aerodynamic Effect 50%
• Organic Solar Cells 50%
• Air Ratio 50%

Keyphrases

• Solar Power 100%
• Micro Aerial Vehicle 100%
• Power-to-weight Ratio 33%
• Vertical Takeoff 33%
• Solar Panel 33%
• Swift 33%
• Energy Conservation 16%
• Ultrahigh Power 16%
• Wing Configurations 16%
• Aerodynamic Effect 16%
• Fixed-wing Aircraft 16%
• Vehicle Configuration 16%
• Flight Time 16%
• Ultrathin 16%
• Civil Structures 16%
• Air-stable 16%
• Energy Density 16%
• Low Reynolds number 16%
• Structure Health Monitoring 16%
• High Power 16%
• Cruise Travel 16%
• Fan-in 16%
• Square Shape 16%
• Low Aspect Ratio Wing 16%
• Organic Photovoltaics 16%
• Quadcopter 16%