Study of wing camber for optimal flight efficiency of a long-endurance solar-powered unmanned aircraft

Keyphrases

• Flyer 100%
• Solar Power 100%
• Unmanned Aircraft 100%
• Long Endurance 100%
• Flight Efficiency 100%
• Optimal Flight 100%
• Wing Camber 100%
• UAV 66%
• High Performance 33%
• Precision Control 33%
• High Power 33%
• Actuation 33%
• Control Surface 33%
• Airframe 33%
• Computationally Intensive 33%
• Finite Energy 33%
• High-throughput Computation 33%
• Embedded Systems 33%
• Flap 33%
• Energy Consumption Reduction 33%
• Widespread Adoption 33%
• Flight Time 33%
• Power Consumption 33%
• Minimizing Cost 33%
• Traditional Design 33%
• Data Transmission 33%
• Propulsion System 33%
• Energy Resources 33%
• Power Data 33%
• Power Required 33%
• Capture Data 33%
• Flight Testing 33%
• Airfoil Shape 33%
• Powered Flight 33%
• Flight Simulation 33%
• Aileron 33%
• On-board Processing 33%
• Aircraft Power 33%
• Aircraft Size 33%

Engineering

• Unmanned Aerial Vehicle 100%
• Unmanned Aircraft 100%
• Actuation 50%
• Control Surfaces 50%
• Airframe 50%
• Flaps 50%
• Electric Power Utilization 50%
• Endurance Limit 50%
• Finite Energy 50%
• Flight Time 50%
• Data Link 50%
• Propulsion System 50%
• Flight Test 50%
• Computer System 50%
• Reduce Power Consumption 50%
• Airfoil Shape 50%
• Powered Flight 50%
• Energy Resource 50%