An important put of building mathematical models based on measured date is calculating the accuracy associated with statistical estimates of the model parameters. Indeed, without some idea of this accuracy, the parameter estimates themselves have limited value. An expression is developed for computing quantitatively correct parameter accuracy measures for maximum likelihood parameter estimates when the output residuals are colored. This result is important because experience in analyzing flight test data reveals that the output residuals from maximum likelihood estimation are almost always colored. The calculations involved can be appended to conventional maximum likelihood estimation algorithms. Monte Carlo simulation runs were used to sho...
The information presented is based on the experience in the past 12 years at the NASA Dryden Flight ...
The NASA Generic Transport Model (GTM) nonlinear simulation was used to investigate the effects of e...
Values for the stability and control parameters for a general aviation airplane were determined from...
An important part of building mathematical models based on measured data is calculating the accuracy...
An important part of building high fidelity mathematical models based on measured data is calculatin...
Means of assessing the accuracy of maximum likelihood parameter estimates obtained from dynamic flig...
Various practical aspects of the equation-error approach to aircraft parameter estimation were exami...
A nonlinear simulation of the NASA Generic Transport Model was used to investigate the effects of er...
An iterative method, which is characterized as a maximum-likelihood minimum-variance technique, was ...
A maximum likelihood parameter estimation procedure and program were developed for the extraction of...
This paper explores the difficulties of aircraft system identification, specifically parameter estim...
Output-error parameter estimation, normally a post- ight batch technique, was applied to real-time d...
An output error estimation algorithm was used to evaluate the effects of both static and dynamic ins...
Flight data from an F-8 Corsair and a Cessna 172 was analyzed to demonstrate specific improvements i...
A new formulation of the filter-error method for estimating aerodynamic parameters in nonlinear airc...
The information presented is based on the experience in the past 12 years at the NASA Dryden Flight ...
The NASA Generic Transport Model (GTM) nonlinear simulation was used to investigate the effects of e...
Values for the stability and control parameters for a general aviation airplane were determined from...
An important part of building mathematical models based on measured data is calculating the accuracy...
An important part of building high fidelity mathematical models based on measured data is calculatin...
Means of assessing the accuracy of maximum likelihood parameter estimates obtained from dynamic flig...
Various practical aspects of the equation-error approach to aircraft parameter estimation were exami...
A nonlinear simulation of the NASA Generic Transport Model was used to investigate the effects of er...
An iterative method, which is characterized as a maximum-likelihood minimum-variance technique, was ...
A maximum likelihood parameter estimation procedure and program were developed for the extraction of...
This paper explores the difficulties of aircraft system identification, specifically parameter estim...
Output-error parameter estimation, normally a post- ight batch technique, was applied to real-time d...
An output error estimation algorithm was used to evaluate the effects of both static and dynamic ins...
Flight data from an F-8 Corsair and a Cessna 172 was analyzed to demonstrate specific improvements i...
A new formulation of the filter-error method for estimating aerodynamic parameters in nonlinear airc...
The information presented is based on the experience in the past 12 years at the NASA Dryden Flight ...
The NASA Generic Transport Model (GTM) nonlinear simulation was used to investigate the effects of e...
Values for the stability and control parameters for a general aviation airplane were determined from...