Design of a flight control system for a highly maneuverable aircraft using robust dynamic

Keyphrases

• Flight Control System 100%
• Highly Maneuverable Aircraft 100%
• Loop Controller 100%
• Robust Dynamics 100%
• Controller 66%
• Handling Qualities 66%
• Angle of Attack 66%
• Dynamic Inversion 66%
• Mach number 33%
• Flight Condition 33%
• Linear Controller 33%
• Aircraft Dynamics 33%
• Flight Controller 33%
• Nonlinear Simulation 33%
• Sensor Noise 33%
• Longitudinal Control 33%
• Outer Loop 33%
• Model Uncertainty 33%
• Quality Model 33%
• Pitch Rate 33%
• Robustness to Uncertainty 33%
• Quality Requirements 33%
• Command System 33%
• Structured Singular Value 33%
• High Performance Aircraft 33%

Engineering

• Flight Control 100%
• Loop Controller 100%
• Angle-of-Attack 66%
• Controllability 66%
• Model System 33%
• Mach Number 33%
• Sensor Noise 33%
• Model Uncertainty 33%
• Performance Aircraft 33%
• Command System 33%
• Aircraft Response 33%
• Pitch Rate 33%
• Outer Loop 33%
• Flight Condition 33%
• Singular Value 33%
• Linear Controller 33%