Add to ORKGThis paper presents the results of system identification and state /parameter estimation of analysis of flight data of a transport aircraft. The techniques, combined in a two-step methodology, provide an efficient and useful procedure for characterizing the dynamical behavior of aerospace vehicles as well as general systems. The results of kinematic consistency checking and combining of maneuvers for analysis and handling quality evaluation are presented
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
This paper presents the identification of the aerodynamic model of the "Flying-V", a novel aircraft ...
This paper presents the results of system identification and state /parameter estimation of analysis...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
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...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
This paper presents the identification of the aerodynamic model of the "Flying-V", a novel aircraft ...
This paper presents the results of system identification and state /parameter estimation of analysis...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft fr...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
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...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
This paper presents the identification of the aerodynamic model of the "Flying-V", a novel aircraft ...