Robust gain-scheduled autopilot design with anti-windup compensation for a guided projectile

INIS

• design 100%
• gain 100%
• nonlinear problems 100%
• projectiles 100%
• saturation 75%
• simulation 50%
• control 25%
• dynamics 25%
• actuators 25%
• augmentation 25%
• mechanics 25%
• aerodynamics 25%
• comparative evaluations 25%
• spin 25%
• monte carlo method 25%
• pitches 25%
• disturbances 25%
• wind 25%
• constraints 25%

Engineering

• Design 100%
• Nonlinear Model 50%
• Models 50%
• Launch Condition 50%
• Time Domain 50%
• Constraint Analysis 50%
• Compensator 50%
• Control Design 50%
• Open Loop 50%
• Flight Mechanics 50%
• Nonlinear Parameter 50%
• Aerodynamics 50%