Implementation and validation of a 6 degrees-of-freedom nonlinear helicopter model

Keyphrases

• Hovering 100%
• Six Degrees of Freedom 100%
• Forward Flight 100%
• Helicopter Model 100%
• Helicopter 50%
• Quality Assessment 50%
• Coupling Effect 50%
• Nonlinear Model 50%
• Motion-based 50%
• Flight Condition 50%
• Standardized Tests 50%
• Flight Data 50%
• Handling Qualities 50%
• Design Standards 50%
• Flight Test Data 50%
• Control Augmentation System 50%
• Model Fidelity 50%

Engineering

• Degree of Freedom 100%
• Forward Flight 100%
• Frequency Domain 50%
• Test Data 50%
• Time Domain 50%
• Nonlinear Model 50%
• Coupling Effect 50%
• Flight Test 50%
• Flight Condition 50%
• Augmentation System 50%
• Handling Quality Evaluation 50%
• Physical Vehicle 50%
• Model Fidelity 50%
• Flight Data 50%