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What is Lateral Control Design for Cessna X about?

This conference paper presents a methodology for designing a lateral flight control system for the Cessna Citation X that meets robustness and handling qualities requirements. The system comprises a Stability Augmented System (SAS) and a Command Augmented System (CAS), utilizing optimal control theory and guardian maps for performance and robustness analysis. The methodology was validated through simulations using a full nonlinear aircraft model, addressing over 100 flight conditions to ensure effectiveness

Author

Daniele Cetrullo

Language

EN