A Control Design Oriented Mathematical Model for the Scirocco Plasma Wind Tunnel

DOI10.1076/MCMD.7.1.109.3635zbMath0997.93078OpenAlexW1979188885MaRDI QIDQ2721613

G. Ambrosino, Giovanni Celentano, Massimiliano Mattei

Publication date: 10 July 2001

Published in: Mathematical and Computer Modelling of Dynamical Systems (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/10.1076/mcmd.7.1.109.3635

zbMATH Keywords

trackinghypersonic flowssimulation modelspace vehiclesre-entry phasethermal processesplasma wind tunnelprocess-control integrated designtest control algorithm

Mathematics Subject Classification ID

Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51) Hypersonic flows (76K05) Ionized gas flow in electromagnetic fields; plasmic flow (76X05)

Related Items (2)

An LMI approach to the design of a robust observer with application to a temperature control problem for space vehicle testing ⋮ Robust control of a plasma wind tunnel: an LPV discrete-time system depending on fast/slowly-varying parameters

Uses Software

• Neural Network Toolbox

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