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Lie-Group Modeling and Numerical Simulation of a Helicopter

Alessandro Tarsi and Simone Fiori
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Alessandro Tarsi: School of Automation Engineering, Alma Mater Studiorum—Università di Bologna, Viale del Risorgimento 2, I-40136 Bologna, Italy
Simone Fiori: Department of Information Engineering, Marches Polytechnic University, Brecce Bianche Rd., I-60131 Ancona, Italy

Mathematics, 2021, vol. 9, issue 21, 1-34

Abstract: Helicopters are extraordinarily complex mechanisms. Such complexity makes it difficult to model, simulate and pilot a helicopter. The present paper proposes a mathematical model of a fantail helicopter type based on Lie-group theory. The present paper first recalls the Lagrange–d’Alembert–Pontryagin principle to describe the dynamics of a multi-part object, and subsequently applies such principle to describe the motion of a helicopter in space. A good part of the paper is devoted to the numerical simulation of the motion of a helicopter, which was obtained through a dedicated numerical method. Numerical simulation was based on a series of values for the many parameters involved in the mathematical model carefully inferred from the available technical literature.

Keywords: Lagrange–d’Alembert principle; non-conservative dynamical system; Euler–Poincaré equation; helicopter model; Lie group (search for similar items in EconPapers)
JEL-codes: C (search for similar items in EconPapers)
Date: 2021
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