Real-time system identification of a small multi-engine aircraft

Keyphrases

• Regression Method 100%
• Real-time System Identification 100%
• Fourier Transform Regression 100%
• Multi-engine 100%
• Sine 50%
• Dynamic Model 50%
• Closed-loop 50%
• Model Change 50%
• Six Degrees of Freedom 50%
• Aircraft Model 50%
• Updating Model 50%
• Aerodynamic Stability 50%
• Aircraft Dynamics 50%
• Adaptive Control Strategy 50%
• Parameter Identification 50%
• Stability Derivatives 50%
• Real-time Parameters 50%
• Fixed-wing Unmanned Aerial Vehicles 50%
• Flight Test Data 50%
• Flight Identification 50%
• On-board Controller 50%
• Recursive Discrete Fourier Transform 50%
• Real Flight Data 50%
• Twin-engine 50%

Engineering

• Fourier Transform 100%
• Frequency Domain 100%
• Dynamic Models 100%
• Aircraft Engine 100%
• Unmanned Aerial Vehicle 50%
• Adaptive Control 50%
• Degree of Freedom 50%
• Control Scheme 50%
• Closed Loop 50%
• Recursive 50%
• Flight Test 50%
• Aerodynamic Stability 50%
• Fixed Wings 50%
• Test Data 50%
• Flight Data 50%