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Development of a Control Augmentation System for a Tilt-Rotor Aircraft

Alessandro Briamonte

Development of a Control Augmentation System for a Tilt-Rotor Aircraft.

Rel. Giorgio Guglieri, Pierluigi Capone. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2022

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This thesis focus on a control augmentation system development for XV-15 Tilt-Rotor Aircraft. The main control actions are holding pitch, roll, together with a turn hold. These features are relevant for autonomous navigation and guidance purposes, in order to satisfy the mission requirements. Proportional-Integral-Derivative (PID) is one of the traditional control algorithms and plays key role in the achievement of given requirements. LEAD-LAG compensators features are cheked. The project is implemented on the simulator, in order to test the system and assess the handling qualities.

Relators: Giorgio Guglieri, Pierluigi Capone
Academic year: 2021/22
Publication type: Electronic
Number of Pages: 157
Corso di laurea: Corso di laurea magistrale in Ingegneria Aerospaziale
Classe di laurea: New organization > Master science > LM-20 - AEROSPATIAL AND ASTRONAUTIC ENGINEERING
Ente in cotutela: ZHAW (SVIZZERA)
Aziende collaboratrici: ZHAW Zurich University of Applied Sciences
URI: http://webthesis.biblio.polito.it/id/eprint/23326
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