Add to ORKGIn this paper we describe the results of extensive analysis of flight test data of a modified transport aircraft to evaluate its handling qualities and flight simulation model. The results have been generated using modern techniques of parameter estimation Applied to dynamic maneu v ers of the aircraft. The role of simulation model validation has been highlighted
This paper provides an overview of a few selected system identification activities carried out durin...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
The Mathematical Models Using Flight Test Data With Respect To A Transport. Aircraft For The Offline...
This paper presents the results of system identification and state /parameter estimation of analysis...
IMECE2008-67482PDFResearch PaperAircraftSimulationFlight simulatorsSoftwareValidationPerformance tes...
Reliability validation of safety-critical flight control systems requires accurate simula-tion model...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
In aircraft development, it is crucial to understand and evaluate behavior, performance, safety and ...
Today's development and construction processes for aeronautical structures impose increasing demands...
Abstract:Flight simulation now becomes an approach that can effectively and safely be used for engin...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
ii A methodology is developed that uses probabilistic analysis and computational simulation to conti...
The thesis at hand addresses the evaluation of flight test data to enable subsequent handling qualit...
This paper provides an overview of a few selected system identification activities carried out durin...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...
In this paper we describe the results of extensive analysis of flight test data of a modified transp...
The Mathematical Models Using Flight Test Data With Respect To A Transport. Aircraft For The Offline...
This paper presents the results of system identification and state /parameter estimation of analysis...
IMECE2008-67482PDFResearch PaperAircraftSimulationFlight simulatorsSoftwareValidationPerformance tes...
Reliability validation of safety-critical flight control systems requires accurate simula-tion model...
Irn this report several methods for estimation of parameters and states of13; dynamical systems are ...
In aircraft development, it is crucial to understand and evaluate behavior, performance, safety and ...
Today's development and construction processes for aeronautical structures impose increasing demands...
Abstract:Flight simulation now becomes an approach that can effectively and safely be used for engin...
Abstract. With the evolution of high performance modern aircraft and spira-ling developmental and ex...
ii A methodology is developed that uses probabilistic analysis and computational simulation to conti...
The thesis at hand addresses the evaluation of flight test data to enable subsequent handling qualit...
This paper provides an overview of a few selected system identification activities carried out durin...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The aerodynamic model of an aircraft can be considered as a mathematical representation of the force...