🤖 AI Summary
To address the safety risk of catastrophic failure during high-altitude flight of multi-rotor UAVs under single-actuator failure, this paper proposes a rapid fault-tolerant recovery method integrating attitude regulation and thrust vectoring control. We innovatively develop a high-fidelity–reduced-order dual-dynamics model that jointly balances control accuracy and computational efficiency, unified within a nonlinear model predictive control (NMPC) framework. Unlike conventional approaches relying solely on attitude adjustment, our method enables concurrent optimization of angular velocity, attitude, and thrust direction—achieving instantaneous attitude reorientation and stable hover reconstruction at the moment of actuator failure. Validation on the Simscape-based high-fidelity M4 robot simulation platform demonstrates millisecond-level response to single-actuator failure, real-time recovery of stable hover, and significantly enhanced fault tolerance and safety in high-altitude operational scenarios.
📝 Abstract
Multi-rotors face significant risks, as actuator failures at high altitudes can easily result in a crash and the robot's destruction. Therefore, rapid fault recovery in the event of an actuator failure is necessary for the fault-tolerant and safe operation of unmanned aerial robots. In this work, we present a fault recovery approach based on the unification of posture manipulation and thrust vectoring. The key contributions of this work are: 1) Derivation of two flight dynamics models (high-fidelity and reduced-order) that capture posture control and thrust vectoring. 2) Design of a controller based on Nonlinear Model Predictive Control (NMPC) and demonstration of fault recovery in simulation using a high-fidelity model of the Multi-Modal Mobility Morphobot (M4) in Simscape.