Control Design and Simulation Validation for High-Force Aerial Physical Interaction with a Tilting and Center-of-Mass-Shifting UAV

Ulissi, Brando (2026) Control Design and Simulation Validation for High-Force Aerial Physical Interaction with a Tilting and Center-of-Mass-Shifting UAV. [Laurea magistrale], Università di Bologna, Corso di Studio in Automation engineering / ingegneria dell’automazione [LM-DM270], Documento ad accesso riservato.
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Abstract

Unmanned aerial vehicles capable of physical interaction with the environment are increasingly relevant for inspection and maintenance where human access is hazardous or costly. The Aerobull platform, an H-shaped coaxial octocopter developed at DTU, addresses the force–attitude coupling that limits conventional multirotors by combining tiltable rear rotors with an internal shifting-mass mechanism. During contact, the centre of mass is displaced forward, enabling the rear rotors to reorient thrust horizontally. This thesis extends Aerobull's simulation-based control framework along three axes: sensing, control, and simulation infrastructure. The previous contact model is replaced by four distributed uniaxial load cells, enabling a passive orientation strategy on inclined surfaces and mitigating the lateral sliding of the earlier architecture. A dual-mode high-level controller is developed to manage both free-flight navigation and force regulation during pushing, coordinated with a platform controller commanding the shifting-mass displacement upon contact; the overall framework is validated on flat and inclined surfaces, including under wind disturbances. A feedforward compensation for the pitching moment of a future Cartesian end-effector is also integrated into the allocation pipeline. A super-twisting sliding mode controller is adapted from a planar formulation to the full six-degree-of-freedom Simscape model. Finally, a co-simulation pipeline coupling Simulink with PX4, ROS 2, and Gazebo is built to bring the control loop closer to real-flight conditions. Simscape results demonstrate stable 20 N pushing on flat and 15° inclined surfaces under aerodynamic disturbances, with pitch deviations below 0.3° during end-effector loading of 3 N·m. The Gazebo pipeline validates the free-flight behaviour and achieves preliminary force tracking, identifying the tilt servo transient and load-cell signal quality as the main open points before hardware transfer.

Abstract
Tipologia del documento
Tesi di laurea (Laurea magistrale)
Autore della tesi
Ulissi, Brando
Relatore della tesi
Correlatore della tesi
Scuola
Corso di studio
Indirizzo
AUTOMATION ENGINEERING
Ordinamento Cds
DM270
Parole chiave
Aerial physical interaction, Coaxial octocopter, Shifting-mass mechanism, Force control, Sliding mode control, over-actuated UAV
Data di discussione della Tesi
25 Marzo 2026
URI

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