Trajectory Tracking Control Design for Autonomous Helicopters with Guaranteed Error Bounds
Abstract
This paper presents a systematic framework for computing formally guaranteed trajectory tracking error bounds for autonomous helicopters based on Robust Positive Invariant (RPI) sets. The approach focuses on establishing a closed-loop translational error dynamics which is cast into polytopic linear parameter-varying form with bounded additive and state-dependent disturbances. Ellipsoidal RPI sets are computed, yielding explicit position error bounds suitable as certified buffer zones in upper-level trajectory planning. Three controller architectures are compared with respect to the conservatism of their error bounds and tracking performance. Simulation results on a nonlinear helicopter model demonstrate that all architectures respect the derived bounds, while highlighting trade-offs between dynamical fidelity and conservatism in invariant set computation.
Cite
@article{arxiv.2603.08045,
title = {Trajectory Tracking Control Design for Autonomous Helicopters with Guaranteed Error Bounds},
author = {Philipp Schitz and Johann C. Dauer and Paolo Mercorelli},
journal= {arXiv preprint arXiv:2603.08045},
year = {2026}
}
Comments
Submitted to the 2026 International Conference on Unmanned Aircraft Systems (ICUAS)