Dynamic modelling and linear quadratic Gaussian control of a twin-rotor multi-input multi-output system

Keyphrases

• Dynamic Model 100%
• Linear Quadratic Gaussian Control 100%
• Dynamics Linear 100%
• Twin Rotor Multi-Input Multi-Output System 100%
• Stability Augmentation System 100%
• Helicopter 50%
• Tracking Capability 50%
• Hovering 50%
• Feedback Compensator 50%
• Single Degree of Freedom 50%
• Control Law 50%
• System Identification 50%
• Control Problem 50%
• Actuator Constraints 50%
• Residual Vibration 50%
• Prefilter 50%
• Linear Quadratic Gaussian 50%
• Performance Objectives 50%
• Black-box Systems 50%
• Identification Problem 50%
• Feedforward Compensator 50%
• Control Effort 50%

Engineering

• Output System 100%
• Multi-Input Multi-Output 100%
• Linear Quadratic Gaussian 100%
• Stability Augmentation 100%
• Rotors 100%
• Augmentation System 100%
• Dynamic Models 50%
• Degree of Freedom 50%
• Feedforward 50%
• Prefilter 50%
• Black Box 50%
• Command Path 50%
• Control Law 50%