Emanuele Luigi De Angelis

Prof. de Angelis primarily focuses on topics related to atmospheric and space flight mechanics, with particular attention to modeling, simulation, state estimation, and control aspects. With a PhD thesis centered on the analysis and control of nonlinear systems, his publications range from the study of stability in underactuated systems applied to the magnetic control of satellites in low orbit, to the analysis of fixed-wing and rotary-wing aircraft in solitary flight, formation flight, or carrying suspended loads. Go to the Curriculum vitae