Non-linear model identification for a miniature rotorcraft preliminary results

Keyphrases

• Rotorcraft 100%
• Nonlinear Model 100%
• Control System 50%
• Estimation Method 50%
• System Dynamics 50%
• Maximum Likelihood 50%
• Explicit Model 50%
• Complex Dynamics 50%
• Matching Algorithm 50%
• UAV 50%
• Nonlinear Extensions 50%
• Parameter Identification 50%
• Sensor Fusion 50%
• Avionics 50%
• Kinematic Consistency 50%
• Data Reliability 50%
• Linear State Space Model 50%
• Estimate Model Parameter 50%
• Rotor UAV 50%
• Test Manoeuvres 50%
• Domain Matching 50%
• Time Domain Parameters 50%
• Output Error Estimation 50%

Engineering

• Rotorcraft 100%
• Nonlinear Model 100%
• Unmanned Aerial Vehicle 66%
• Time Domain 66%
• Control System 33%
• Error Estimation 33%
• Systems Dynamics 33%
• Model Parameter 33%
• Maximum Likelihood 33%
• Matching Algorithm 33%
• Flight Test 33%
• Reliability Data 33%
• Output Error 33%
• Avionics 33%
• Sensor Fusion 33%

Physics

• Rotary Wing Aircraft 100%
• Avionics 33%
• Flight Test 33%
• Multisensor Fusion 33%