The aim of this note is to present the activity performed by the Flight Mechanics Lab- oratory of the University of Bologna by means of Model Based Design concept; dynamic modeling, control system design, and Hardware/Software-in-the-Loop techniques for an UAS research project will be described as well as numerical and experimental results.
Modeling, control system design and hardware/software-in-the-loop simulation for UAS / DE ANGELIS E.L.; GIULIETTI F.; TURCI M.. - STAMPA. - (2011), pp. 1-21.
Modeling, control system design and hardware/software-in-the-loop simulation for UAS
DE ANGELIS, EMANUELE LUIGI;GIULIETTI, FABRIZIO;TURCI, MATTEO
2011
Abstract
The aim of this note is to present the activity performed by the Flight Mechanics Lab- oratory of the University of Bologna by means of Model Based Design concept; dynamic modeling, control system design, and Hardware/Software-in-the-Loop techniques for an UAS research project will be described as well as numerical and experimental results.File in questo prodotto:
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