Sparse nonlinear system identification for hypersonic aerothermoelastic analysis with stochastic loads

Keyphrases

• Governing Equation 100%
• Nonlinear System Identification 100%
• Hypersonic 100%
• Aerothermoelastic Analysis 100%
• High Mach number 50%
• Experimental Testing 50%
• Dynamical Systems 50%
• Optimization Problem 50%
• Approximate Solution 50%
• Unified Framework 50%
• Limited Ability 50%
• Dynamical Model 50%
• Degree of Uncertainty 50%
• Mission Profile 50%
• Aerothermodynamics 50%
• Hypersonic Vehicle 50%
• Flight Test Data 50%
• Norm Approximation 50%
• Well-posed 50%
• Automatic Framework 50%
• Aerothermoelastic 50%
• Ground Test 50%

Engineering

• Nonlinear System Identification 100%
• Hypersonic Vehicle 100%
• Collected Data 50%
• Test Data 50%
• High Mach Number 50%
• Measurement Data 50%
• Optimisation Problem 50%
• Breathing 50%
• Flight Test 50%
• Approximation Solution 50%
• Norm Approximation 50%
• Aerothermodynamics 50%

Material Science

• Mach Number 100%