L1Adaptive Control for a Single Coaxial Rotor MAV

This paper investigates the application of L1 adaptive augmentation to the experimental flight of a Single Coaxial Rotor (SCR) Micro Aerial Vehicle (MAV) conducted in the indoor flight facility of the National Defense Academy (NDA) of Japan. In this work, L1 adaptive controller parameters are determined by the use of multi-objective optimization. The adaptive controller is applied to the translational motion control while performing an experimental flight including heave motion, hovering, and hover-to-hover maneuvers to evaluate the controller. The results provide precise tracking performance and validate the feasibility of the adaptive controller.

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