A new heuristic approach to rotorcraft system identification

Engineering

• Rotorcraft 100%
• Models 66%
• Complexity 66%
• Stability 33%
• Simulation 33%
• Error 33%
• Nonlinearity 33%
• Dynamic Response 33%
• Good Correlation 33%
• Aerodynamics 33%
• Couplings 33%
• Interference 33%
• Test Data 33%
• Rigid Structure 33%
• Magnitude Response 33%
• Low Speed 33%
• Time Domain 33%
• Response Time 33%
• Model Parameter 33%
• Non-Linear Dynamics 33%
• Flight Dynamics 33%
• Flight Test 33%
• Proposed Nonlinear Model 33%
• Good Level 33%
• Derivative Control 33%