The problem of the selection from measured data of an aircraft of an adequate model which v.ould he the simplest and sufficient approximation to the correct model and which would facilitate the successful determination of the unknown parameters is discussed. Two v/ays for the proper model structure verification are recommended, namely sensitivity analysis and/or testing of a hypothesis as to the significance of unknovm parameters in the model proposed, and the analysis of residuals. Finally some approaches towards the assessment of parameter and adequate model accuracies are proposed. The procedures mentioned are demonstrated in an example
Several statistical and information criteria need to be considered when selecting an adequate model....
The paper presents a successful application of the Estimation Before Modelling (EBM) methodology, kn...
This paper presents the results of system identification and state /parameter estimation of analysis...
All three steps in the identification, namely characterization parameter estimation and verificati...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN003944 / BLDSC - British Library D...
Robustness concepts are discussed in the context of helicopter system identification and model valid...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
The use of the estímation-before-modellíng (EBM) two step identification procedure for the determi...
In a fairly complex system like aircraft, modeling and parameter estimation plays a crucial role in ...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
This article gives a brief overview of procedures and of some exemplary results of validating analyt...
Several statistical and information criteria need to be considered when selecting an adequate model....
The paper presents a successful application of the Estimation Before Modelling (EBM) methodology, kn...
This paper presents the results of system identification and state /parameter estimation of analysis...
All three steps in the identification, namely characterization parameter estimation and verificati...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN003944 / BLDSC - British Library D...
Robustness concepts are discussed in the context of helicopter system identification and model valid...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
The use of the estímation-before-modellíng (EBM) two step identification procedure for the determi...
In a fairly complex system like aircraft, modeling and parameter estimation plays a crucial role in ...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
This article gives a brief overview of procedures and of some exemplary results of validating analyt...
Several statistical and information criteria need to be considered when selecting an adequate model....
The paper presents a successful application of the Estimation Before Modelling (EBM) methodology, kn...
This paper presents the results of system identification and state /parameter estimation of analysis...