Add to ORKG18 figs., 2 tabs., 32 refs.SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman
With 8 figs., 5 tabs., 32 refs.Copy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fa...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
The large quantities of data generated at the Institute for Flight Mechanics of the German Aerospace...
Two methods for maximum-likelihood estimation of flight mechanics parameters have been developed. Th...
Two methods for maximum-likelihood estimation of flight mechanics parameters have been developed. Th...
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...
"A method of parameter extraction for stability and control derivatives of aircraft from flight test...
The paper presents the modeling of nonlinear longitudinal aerodynamics using flight data of Hansa-3 ...
The first version of a new online parameter estimation tool is presented. Based on the maximum likel...
A maximum likelihood parameter estimation procedure and program were developed for the extraction of...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
This work describes the application of the output-error method using the Levenberg-Marquardt optimiz...
An important put of building mathematical models based on measured date is calculating the accuracy ...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
With 8 figs., 5 tabs., 32 refs.Copy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fa...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
The large quantities of data generated at the Institute for Flight Mechanics of the German Aerospace...
Two methods for maximum-likelihood estimation of flight mechanics parameters have been developed. Th...
Two methods for maximum-likelihood estimation of flight mechanics parameters have been developed. Th...
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...
"A method of parameter extraction for stability and control derivatives of aircraft from flight test...
The paper presents the modeling of nonlinear longitudinal aerodynamics using flight data of Hansa-3 ...
The first version of a new online parameter estimation tool is presented. Based on the maximum likel...
A maximum likelihood parameter estimation procedure and program were developed for the extraction of...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
This work describes the application of the output-error method using the Levenberg-Marquardt optimiz...
An important put of building mathematical models based on measured date is calculating the accuracy ...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
With 8 figs., 5 tabs., 32 refs.Copy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fa...
The flight testing and evaluation of collected data must be efficient during intensive flight-test p...
The large quantities of data generated at the Institute for Flight Mechanics of the German Aerospace...
