Physically Integrated Reference Model Based Flight Control

Beschreibung

Abstract A novel reference model based flight control architecture with protections enables a decoupling of closed loop dynamics specification from controller design. Decoupling is facilitated by designing a reference model based on functional and handling qualities requirements. New protection algorithms using dynamic inversion and phase plane limitations are applied to the reference model, assisting non-conservative full envelope exploitation. A tracking controller is designed to keep the closed-loop dynamics within tight bounds around the specified reference behavior.

Autor*in

Fubiao Zhang

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Flight Control Physically Integrated Reference Model Phase Plane Limitations

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