Models of the open-loop hover dynamics of the XV-15 Tilt-Rotor Aircraft are extracted from flight data using two approaches: frequency domain and time-domain identification. Both approaches are reviewed and the identification results are presented and compared in detail. The extracted models are compared favorably, with the differences associated mostly with the inherent weighing of each technique. Step responses are used to show that the predictive capability of the models from both techniques is excellent. Based on the results of this study, the relative strengths and weaknesses of the frequency and time-domain techniques are summarized and a proposal for a coordinated parameter identification approach is presented
This paper presents the implementation of a Multi-Input Single-Output fully coupled transfer functio...
The civil light helicopter domain has not fully benefited yet from the advantages system identificat...
The availability of suitable methods for system identification from flight data of rotorcraft models...
Models of the open-loop hover dynamics of the XV-15 Tilt-Rotor Aircraft are extracted from flight da...
-Models of the open-loop hover dynamics of the XV-15 Tilt-Rotor Aircraft are extracted from flight d...
Frequency-domain methods are used to extract the open-loop dynamics of the XV-15 tilt-rotor aircraft...
This paper presents the implementation of a Multi-Input Single-Output fully coupled transfer functio...
The civil light helicopter domain has not fully benefited yet from the advantages system identificat...
The timely design and development of the next generation of tilt-rotor aircraft (JVX) depend heavily...
The XV-15 Tilt-Rotor wing has six major aeroelastic modes that are close in frequency. To precisely ...
There is considerable need for the application of system identification techniques to helicopters. T...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
This paper is concerned with the development of methods for the validation of complex non-linear mod...
Current frequency-domain system identification methods require an open-loop experiment design for da...
The introduction of tilt-rotor aircraft into the existing civilian air transportation system will pr...
This paper presents the implementation of a Multi-Input Single-Output fully coupled transfer functio...
The civil light helicopter domain has not fully benefited yet from the advantages system identificat...
The availability of suitable methods for system identification from flight data of rotorcraft models...
Models of the open-loop hover dynamics of the XV-15 Tilt-Rotor Aircraft are extracted from flight da...
-Models of the open-loop hover dynamics of the XV-15 Tilt-Rotor Aircraft are extracted from flight d...
Frequency-domain methods are used to extract the open-loop dynamics of the XV-15 tilt-rotor aircraft...
This paper presents the implementation of a Multi-Input Single-Output fully coupled transfer functio...
The civil light helicopter domain has not fully benefited yet from the advantages system identificat...
The timely design and development of the next generation of tilt-rotor aircraft (JVX) depend heavily...
The XV-15 Tilt-Rotor wing has six major aeroelastic modes that are close in frequency. To precisely ...
There is considerable need for the application of system identification techniques to helicopters. T...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
This paper is concerned with the development of methods for the validation of complex non-linear mod...
Current frequency-domain system identification methods require an open-loop experiment design for da...
The introduction of tilt-rotor aircraft into the existing civilian air transportation system will pr...
This paper presents the implementation of a Multi-Input Single-Output fully coupled transfer functio...
The civil light helicopter domain has not fully benefited yet from the advantages system identificat...
The availability of suitable methods for system identification from flight data of rotorcraft models...