Performance and stability of an agile tail-less MAV with flexible articulated wings

Keyphrases

• Turning Performance 100%
• Axial Tension 66%
• Elastic Properties 33%
• Dihedral Angle 33%
• Steady State 33%
• Controlled Experiment 33%
• Twist Angle 33%
• Control Mechanism 33%
• Two-degree-of-freedom 33%
• Heave 33%
• Flight Mechanics 33%
• Novel Actuator 33%
• Wing Stiffness 33%

Engineering

• Axial Tension 100%
• Control System 50%
• Twist Angle 50%
• Two Degree of Freedom 50%
• Flight Mechanics 50%
• Actuator 50%
• Dihedral Angle 50%