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.
DE ANGELIS E.L., GIULIETTI F., TURCI M. (2011). Modeling, control system design and hardware/software-in-the-loop simulation for UAS. RHODE-SAINT-GENÈSE : von Karman Institute for Fluid Dynamics.
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:
Eventuali allegati, non sono esposti
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.