Coordinated Incremental Trajectory Tracking of a Tailsitter Drone
arXiv:2607.11651
The paper presents an analytical differential flatness transform for tailsitter UAVs in coordinated flight, using rotation matrices to avoid Euler angle issues, and validates the approach experimentally for trajectories with significant vertical motion.
Abstract
This paper derives an analytical differential flatness transform for a tailsitter Unmanned Aerial Vehicle (UAV) under coordinated flight conditions using a simplified aerodynamic model. The proposed framework is formulated exclusively using rotation matrices, avoiding the ambiguities inherent to Euler angle representations. The method extends the applicability of an existing state-of-the-art differential flatness-based controller to flight regimes involving a significant vertical velocity component, where the previous approach becomes inapplicable. The proposed framework is validated experimentally with trajectories that highlight its advantages in these regimes.