The aerodynamic coefficients are important in the evaluation of an aircraft performance and stability-control characteristics. These coefficients also can be used in the automatic flight control systems and mathematical model of flight simulator. The study of the aerodynamic aspect of flying systems is a reserved domain and inaccessible for the developers. Doing tests in a wind tunnel to extract aerodynamic forces and moments requires a specific and expensive means. Besides, the glaring lack of published documentation in this field of study makes the aerodynamic coefficients determination complicated. This work is devoted to the identification of an aerodynamic model, by using an aircraft in virtual simulated environment. We deal with the i...
This work describes the design and implementation of a real-time aerodynamic parameter estimation al...
The aerodynamic model identification of a novel aircraft configuration known as the “Flying V” is pr...
All three steps in the identification, namely characterization parameter estimation and verificati...
The least squares method has been applied to estimate parameters inan aerodynamic model of a simulat...
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...
This paper presents the identification of the aerodynamic model of the "Flying-V", a novel aircraft ...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
This paper provides an overview of a few selected system identification activities carried out durin...
The Flying V is a tailless flying wing with a V-shaped planform, where the passenger cabin has been ...
Commercialized flight simulators are considered as a training tool for aircrafts, validated by pilot...
An aerodynamic model of a 4.6% scaled version of the Flying-V is estimatedusing flight data gathered...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
This paper explores the difficulties of aircraft system identification, specifically parameter estim...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
This work describes the design and implementation of a real-time aerodynamic parameter estimation al...
The aerodynamic model identification of a novel aircraft configuration known as the “Flying V” is pr...
All three steps in the identification, namely characterization parameter estimation and verificati...
The least squares method has been applied to estimate parameters inan aerodynamic model of a simulat...
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...
This paper presents the identification of the aerodynamic model of the "Flying-V", a novel aircraft ...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
This paper provides an overview of a few selected system identification activities carried out durin...
The Flying V is a tailless flying wing with a V-shaped planform, where the passenger cabin has been ...
Commercialized flight simulators are considered as a training tool for aircrafts, validated by pilot...
An aerodynamic model of a 4.6% scaled version of the Flying-V is estimatedusing flight data gathered...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
This paper explores the difficulties of aircraft system identification, specifically parameter estim...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
This work describes the design and implementation of a real-time aerodynamic parameter estimation al...
The aerodynamic model identification of a novel aircraft configuration known as the “Flying V” is pr...
All three steps in the identification, namely characterization parameter estimation and verificati...