Real-time shape estimation for a flexible unmanned air vehicle via kalman filtering

Keyphrases

• Wingtip 100%
• Unmanned Air Vehicle 100%
• Kalman Filtering 100%
• Real-time Shape Estimation 100%
• Structural Mode 66%
• Shape Estimation 66%
• Inertial Measurement Unit 66%
• Shape Control 66%
• Tip Deflection 66%
• Aircraft Design 66%
• Closed-loop 33%
• Rigid Body Modes 33%
• Measure Data 33%
• Flight Envelope 33%
• Visual Data 33%
• System Identification 33%
• Feedback Device 33%
• Sampling Rate 33%
• Filter Method 33%
• Heave 33%
• Centerbody 33%
• Visual Information 33%
• Kalman Filter 33%
• Estimation Approaches 33%
• Vehicle Characteristics 33%
• Dynamic Coupling 33%
• Dynamic Stability 33%
• Measurement Update 33%
• Weighted Averaging 33%
• Airframe 33%
• Aircraft Control 33%
• Modern Aircraft 33%
• Aeroelasticity 33%
• Wing-body 33%
• Aerodynamic Shape 33%
• Flying Wing 33%
• Suppression Control 33%
• State Propagation 33%
• Propagation Measurements 33%
• Camera Data 33%
• Structural Shape 33%
• Vehicle Dynamics Model 33%
• Distributed Sensors 33%
• Mode Control 33%
• Flexible Airframe 33%
• Modal Suppression 33%
• Aircraft Modeling 33%
• Linear Kalman Filter 33%

Engineering

• Drone (Aircraft) 100%
• Aircraft 66%
• Kalman Filter 66%
• Airframe 66%
• Inertial Measurement Unit 66%
• Closed Loop 33%
• Rigid Structure 33%
• Vehicle Dynamics 33%
• Flight Envelope 33%
• Flight Test 33%
• Feedback Signal 33%
• Distributed Sensor 33%
• Body Centre 33%
• Measurement Data 33%
• Dynamic Models 33%
• Sampling Rate 33%
• Dynamic Stability 33%
• Aerodynamics 33%