Parameterized modeling methodology for efficient aeroservoelastic analysis of a morphing wing

Engineering

• Closed Loop 100%
• Commercial Software 50%
• Computer Simulation 50%
• Control Law 50%
• Demonstrates 50%
• Finite Element Modeling 50%
• Frequency Response 50%
• Loop Stability 50%
• Mode Shape 50%
• Natural Frequency 50%
• Natural Mode 50%
• Special Attention 50%
• Stability Analysis 50%
• Tasks 50%