TY - GEN
T1 - Sparse nonlinear system identification for hypersonic aerothermoelastic analysis with stochastic loads
AU - Guého, Damien
AU - Singla, Puneet
AU - Huang, Daning
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - Air-breathing hypersonic vehicles is a class of vehicles that operates at high Mach number in the atmosphere for the entire mission profile and are exposed to an extreme aerothermodynamic environment involving stochastic loads. Due to current limited capability of ground tests and the lack of available flight test data, there is a significant degree of uncertainty associated with the aerothermoelastic modeling of hypersonic vehicles and limited ability to alleviate this uncertainty through experimental testing. This work aims to provide a unified and automatic framework to discover governing equations underlying an unknown dynamical system from data measurements. In an appropriate basis, and based on the assumption that the structure of the dynamical model is governed by only a few important terms, the equations are sparse in nature and the resulting model is parsimonious. Solving a well-posed constrained onenorm optimization problem, we obtain a satisfactory zero-norm approximation solution and determine the most prevalent terms in the dynamic governing equations required to accurately represent the collected data.
AB - Air-breathing hypersonic vehicles is a class of vehicles that operates at high Mach number in the atmosphere for the entire mission profile and are exposed to an extreme aerothermodynamic environment involving stochastic loads. Due to current limited capability of ground tests and the lack of available flight test data, there is a significant degree of uncertainty associated with the aerothermoelastic modeling of hypersonic vehicles and limited ability to alleviate this uncertainty through experimental testing. This work aims to provide a unified and automatic framework to discover governing equations underlying an unknown dynamical system from data measurements. In an appropriate basis, and based on the assumption that the structure of the dynamical model is governed by only a few important terms, the equations are sparse in nature and the resulting model is parsimonious. Solving a well-posed constrained onenorm optimization problem, we obtain a satisfactory zero-norm approximation solution and determine the most prevalent terms in the dynamic governing equations required to accurately represent the collected data.
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U2 - 10.2514/6.2021-1609
DO - 10.2514/6.2021-1609
M3 - Conference contribution
AN - SCOPUS:85099966248
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 15
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -