Controller design for the F-14 pitch axis control problem using the quantitative feedback theory approach

Keyphrases

• Control Problem 100%
• Controller Design 100%
• Pitch Axis 100%
• Quantitative Feedback Theory 100%
• Controller 50%
• Parameter Variation 50%
• Design Specification 50%
• Angle of Attack 50%
• Pitch Angle 50%
• Attack Rate 50%
• Robust Controller 50%
• Plant Parameters 50%
• Pitch Rate 50%
• Step Response 50%
• Block Diagram 50%

Engineering

• Controller Design 100%
• Design Specification 50%
• Angle-of-Attack 50%
• Parameter Variation 50%
• Pitch Rate 50%
• System Block Diagram 50%
• Step Response 50%