Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
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 compare favorably, with the differences associated mostly with the inherent weighting 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. (Author).
Modeling XV-15 Tilt-rotor Aircraft Dynamics by Frequency and Time-domain Identification Techniques
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
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 compare favorably, with the differences associated mostly with the inherent weighting 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. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
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 compare favorably, with the differences associated mostly with the inherent weighting 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. (Author).
The History of the XV-15 Tilt Rotor Research Aircraft
Author: Martin D. Maisel
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 222
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 222
Book Description
Scientific and Technical Aerospace Reports
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1346
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1346
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 780
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 780
Book Description
Applied Mechanics Reviews
NASA SP.
Author: Martin D. Maisel
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 232
Book Description
Frequency-response Identification of XV-15 Tilt-rotor Aircraft Dynamics
Author: Mark B. Tischler
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 200
Book Description
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 200
Book Description
Journal of the American Helicopter Society
Author: American Helicopter Society
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 324
Book Description
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 324
Book Description
Identification Modeling and Characteristics of Miniature Rotorcraft
Author: Bernard Mettler
Publisher: Springer Science & Business Media
ISBN: 1475737858
Category : Technology & Engineering
Languages : en
Pages : 237
Book Description
Identification Modeling and Characteristics of Miniature Rotorcraft introduces an approach to developing a simple and effective linear parameterized model of vehicle dynamics using the CIFERâ identification tool created by the Army/NASA Rotorcraft Division. It also presents the first application of the advanced control system optimization tool CONDUITâ to systematically and efficiently tune control laws for a model-scale UAV helicopter against multiple and competing dynamic response criteria. Identification Modeling and Characteristics of Miniature Rotorcraft presents the detailed account of how the theory was developed, the experimentation performed, and how the results were used. This book will serve as a basic and illustrative guide for all students that are interested in developing autonomous flying helicopters.
Publisher: Springer Science & Business Media
ISBN: 1475737858
Category : Technology & Engineering
Languages : en
Pages : 237
Book Description
Identification Modeling and Characteristics of Miniature Rotorcraft introduces an approach to developing a simple and effective linear parameterized model of vehicle dynamics using the CIFERâ identification tool created by the Army/NASA Rotorcraft Division. It also presents the first application of the advanced control system optimization tool CONDUITâ to systematically and efficiently tune control laws for a model-scale UAV helicopter against multiple and competing dynamic response criteria. Identification Modeling and Characteristics of Miniature Rotorcraft presents the detailed account of how the theory was developed, the experimentation performed, and how the results were used. This book will serve as a basic and illustrative guide for all students that are interested in developing autonomous flying helicopters.