This dissertation discusses the mathematical existence and the numerical identification of linear and nonlinear aerodynamic impulse response functions. Differences between continuous-time and discrete-time system theories, which permit the identification and efficient use of these functions, will be detailed. Important input/output definitions and the concept of linear and nonlinear systems with memory will also be discussed. It will be shown that indicial (step or steady) responses (such as Wagner\u27s function), forced harmonic responses (such as Theodorsen\u27s function or those from doublet lattice theory), and responses to random inputs (such as gusts) can all be obtained from an aerodynamic impulse response function. This will establi...
Volterra series is one of the powerful system identification methods for representing the nonlinear ...
We present the results of extending the methodology of system identication techniques as proposed by...
In this work, a continuous time Volterra kernel identification method is presented, based on non-uni...
This dissertation discusses the mathematical existence and the numerical identification of linear an...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses a method for the identification and application of reduced-order models based o...
This paper discusses a method for the identification and application of reduced-order models based o...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.Al...
The numerical investigation of dynamic responses to atmospheric turbulence is an important task duri...
In computational aeroelasticity, unsteady aerodynamics is computationally expensive compared to the ...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
Non-linear unsteady aerodynamic effects present major modelling difficulties in the analysis of aero...
Volterra series is one of the powerful system identification methods for representing the nonlinear ...
We present the results of extending the methodology of system identication techniques as proposed by...
In this work, a continuous time Volterra kernel identification method is presented, based on non-uni...
This dissertation discusses the mathematical existence and the numerical identification of linear an...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses the mathematical existence and the numerically-correct identification of linear...
This paper discusses a method for the identification and application of reduced-order models based o...
This paper discusses a method for the identification and application of reduced-order models based o...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.Al...
The numerical investigation of dynamic responses to atmospheric turbulence is an important task duri...
In computational aeroelasticity, unsteady aerodynamics is computationally expensive compared to the ...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
ABSTRACTOne key task in computational aeroelasticity is to calculate frequency response functions of...
Non-linear unsteady aerodynamic effects present major modelling difficulties in the analysis of aero...
Volterra series is one of the powerful system identification methods for representing the nonlinear ...
We present the results of extending the methodology of system identication techniques as proposed by...
In this work, a continuous time Volterra kernel identification method is presented, based on non-uni...