Immersion and Invariance Adaptive Fault-Tolerant Attitude Control for a Coaxial Tilt-Rotor eVTOL Aircraft
Abstract
This paper proposes an adaptive fault-tolerant attitude control strategy based on the Immersion and Invariance (I&I) methodology for a Coaxial Tilt-Rotor (CTR) eVTOL aircraft. The CTR-eVTOL, equipped with two pairs of CTR modules and a rear rotor, exhibiting strong nonlinearity, underactuated, and strong coupling characteristics, faces significant challenges in maintaining stable attitude control
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