Tito Tomassi
Air segment guidance and control for the Bi-Modal Unmanned Underwater/Air System.
Rel. Manuela Battipede, Piergiovanni Marzocca, Alessio Vitali. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2019
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Abstract
Air segment guidance and control for the Bi-Modal Unmanned Underwater/Air System. The Bi-modal unmanned Underwater/Air System (BUUAS) is a vehicle designed in the RMIT University and able to perform a particular Underwater/Airborne mission profile, with the purpose to carrying airborne surveillance mission with reduced exposure risk with respect to its submarine mothership. The vehicle assumes a dual aerodynamic configuration for the two different phases of the mission. In order to investigate the guidance and control characteristics of the vehicle, a simulator has been implemented. Particular attention has been given to the presence of the Y-tail configuration, featuring an anhedral angle, and to the water-to-air transition phase, where the wing is deployed by changing its sweep angle.
The FDC simulator structure is employed and correlated to data of the BUUAS vehicle and with two different aerodynamic models
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