Add to ORKGIn this document two step methodology to estimate aerodynamic derivatives of a transport aircraft from dynamic maneuvers is thoroughly described. The results of parameter with maximum likelihood method and different types of dynamic maneuvers or their combination are presented. The approach enhances confidence in the methods as well as in the result
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
This paper presents the results of system identification and state /parameter estimation of analysis...
This paper presents the results of system identification and state /parameter estimation of analysis...
This paper presents the results of estimation of the longitudinal and lateral aerodynamic derivative...
This paper presents the results of estimation of the longitudinal and lateral aerodynamic derivative...
To reduce the aircraft development cost it is required to obtain information about the stability and...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
THE effects of flexibility on the flight dynamics of large transport aircraft have been shown to be ...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
Determination of the aerodynamic characteristics of the ATTAS aircraft from flight test data is of c...
The represented investigations are concerned with simulations of unsteady aircraft aerodynamics and ...
The paper presents a successful application of the Estimation Before Modelling (EBM) methodology, kn...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
This paper presents the results of system identification and state /parameter estimation of analysis...
This paper presents the results of system identification and state /parameter estimation of analysis...
This paper presents the results of estimation of the longitudinal and lateral aerodynamic derivative...
This paper presents the results of estimation of the longitudinal and lateral aerodynamic derivative...
To reduce the aircraft development cost it is required to obtain information about the stability and...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
THE effects of flexibility on the flight dynamics of large transport aircraft have been shown to be ...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
Determination of the aerodynamic characteristics of the ATTAS aircraft from flight test data is of c...
The represented investigations are concerned with simulations of unsteady aircraft aerodynamics and ...
The paper presents a successful application of the Estimation Before Modelling (EBM) methodology, kn...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...
The maximum likelihood parameter estimation method for13; nonlinear systems is applied to estimate f...