Sinossi
1. MOTIVATION In many physical situations, a plant model is often provided with a qualitative or quantitative measure of associated model uncertainties. On the one hand, the validity of the model is guaranteed only inside a frequency band, so that nearly nothing can be said about the behavior of the real plant at high frequencies. On the other hand, if the model is derived on the basis of physical equations, it can be parameterized as a function of a few physical parameters, which are usually not perfectly known in practice. This is e.g. the case in aeronautical systems: as an example, the ae- dynamic model of an airplane is derived from the flight mechanics eq- tions. When synthesizing the aircraft control law, it is then necessary to take into account uncertainties in the values of the stability derivatives, which correspond to the physical coefficients of the aerodynamic model. Moreover, this airplane model does not perfectly represent the be- vior of the real aircraft. As a simple example, the flight control system or the autopilot are usually synthesized just using the aerodynamic model, thus without accounting for the flexible mechanicalstructure: the c- responding dynamics are indeed considered as high frequency neglected 1 dynamics, with respect to the dynamics of the rigid model .
Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.
Contenuti
1. Introduction. I: Preliminaries. 2. Introduction to mu and LFTs. 3. Applicative examples. II: Obtention of a standard LFT structure. 4. Realization of uncertain systems under an LFT form. 5. Applications. III: mu applications. 6. Computation of mu bounds. 7. Applications of the mu tools. IV: Skewed mu applications. 8. Skewed mu problems in robustness analysis. 9. Computation of skewed mu bounds. 10. Application of the skewed mu tools. V: Non standard mu applications. 11. Robustness analysis for flexible structures. 12. Robustness analysis in the presence of time delays. 13. Nonlinear analysis in the presence of parametric uncertainties. A: Numerical data. B: Proofs. Summary.
Le informazioni nella sezione "Su questo libro" possono far riferimento a edizioni diverse di questo titolo.
Altre edizioni note dello stesso titolo
Risultati della ricerca per A Practical Approach to Robustness Analysis with Aeronautica...
Foto dell'editore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Da: Lucky's Textbooks, Dallas, TX, U.S.A.
Valutazione del venditore 5 su 5 stelle
Condizione: New. Codice articolo ABLIING23Mar2716030093944
Compra nuovo
EUR 157,61
Spese di spedizione:
EUR 3,42
In U.S.A.
Quantità: Più di 20 disponibili
Foto dell'editore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Da: Ria Christie Collections, Uxbridge, Regno Unito
Valutazione del venditore 5 su 5 stelle
Condizione: New. In. Codice articolo ria9781475772524_new
Compra nuovo
EUR 158,27
Spese di spedizione:
EUR 13,71
Da: Regno Unito a: U.S.A.
Quantità: Più di 20 disponibili
Immagini fornite dal venditore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Print on DemandDa: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -1. MOTIVATION In many physical situations, a plant model is often provided with a qualitative or quantitative measure of associated model uncertainties. On the one hand, the validity of the model is guaranteed only inside a frequency band, so that nearly nothing can be said about the behavior of the real plant at high frequencies. On the other hand, if the model is derived on the basis of physical equations, it can be parameterized as a function of a few physical parameters, which are usually not perfectly known in practice. This is e.g. the case in aeronautical systems: as an example, the ae- dynamic model of an airplane is derived from the flight mechanics eq- tions. When synthesizing the aircraft control law, it is then necessary to take into account uncertainties in the values of the stability derivatives, which correspond to the physical coefficients of the aerodynamic model. Moreover, this airplane model does not perfectly represent the be- vior of the real aircraft. As a simple example, the flight control system or the autopilot are usually synthesized just using the aerodynamic model, thus without accounting for the flexible mechanicalstructure: the c- responding dynamics are indeed considered as high frequency neglected 1 dynamics, with respect to the dynamics of the rigid model . 236 pp. Englisch. Codice articolo 9781475772524
Compra nuovo
EUR 160,49
Spese di spedizione:
EUR 23,00
Da: Germania a: U.S.A.
Quantità: 2 disponibili
Immagini fornite dal venditore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Print on DemandDa: moluna, Greven, Germania
Valutazione del venditore 4 su 5 stelle
Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. 1. MOTIVATION In many physical situations, a plant model is often provided with a qualitative or quantitative measure of associated model uncertainties. On the one hand, the validity of the model is guaranteed only inside a frequency band, so that nearly no. Codice articolo 4207756
Compra nuovo
EUR 136,16
Spese di spedizione:
EUR 48,99
Da: Germania a: U.S.A.
Quantità: Più di 20 disponibili
Foto dell'editore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Da: Books Puddle, New York, NY, U.S.A.
Valutazione del venditore 4 su 5 stelle
Condizione: New. pp. 236. Codice articolo 2697860124
Compra nuovo
EUR 204,73
Spese di spedizione:
EUR 3,42
In U.S.A.
Quantità: 4 disponibili
Immagini fornite dal venditore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Da: preigu, Osnabrück, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. A Practical Approach to Robustness Analysis with Aeronautical Applications | Gilles Ferreres | Taschenbuch | xxvi | Englisch | 2013 | Springer US | EAN 9781475772524 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu. Codice articolo 105650104
Compra nuovo
EUR 141,90
Spese di spedizione:
EUR 70,00
Da: Germania a: U.S.A.
Quantità: 5 disponibili
Immagini fornite dal venditore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Editore:
Springer US, Springer US Mär 2013, 2013
ISBN 10: 1475772521
ISBN 13: 9781475772524
Nuovo
Taschenbuch
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -1. MOTIVATION In many physical situations, a plant model is often provided with a qualitative or quantitative measure of associated model uncertainties. On the one hand, the validity of the model is guaranteed only inside a frequency band, so that nearly nothing can be said about the behavior of the real plant at high frequencies. On the other hand, if the model is derived on the basis of physical equations, it can be parameterized as a function of a few physical parameters, which are usually not perfectly known in practice. This is e.g. the case in aeronautical systems: as an example, the ae- dynamic model of an airplane is derived from the flight mechanics eq- tions. When synthesizing the aircraft control law, it is then necessary to take into account uncertainties in the values of the stability derivatives, which correspond to the physical coefficients of the aerodynamic model. Moreover, this airplane model does not perfectly represent the be- vior of the real aircraft. As a simple example, the flight control system or the autopilot are usually synthesized just using the aerodynamic model, thus without accounting for the flexible mechanicalstructure: the c- responding dynamics are indeed considered as high frequency neglected 1 dynamics, with respect to the dynamics of the rigid model .Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 236 pp. Englisch. Codice articolo 9781475772524
Compra nuovo
EUR 160,49
Spese di spedizione:
EUR 60,00
Da: Germania a: U.S.A.
Quantità: 1 disponibili
Immagini fornite dal venditore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Editore:
Springer US, Springer US, 2013
ISBN 10: 1475772521
ISBN 13: 9781475772524
Nuovo
Taschenbuch
Da: AHA-BUCH GmbH, Einbeck, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - 1. MOTIVATION In many physical situations, a plant model is often provided with a qualitative or quantitative measure of associated model uncertainties. On the one hand, the validity of the model is guaranteed only inside a frequency band, so that nearly nothing can be said about the behavior of the real plant at high frequencies. On the other hand, if the model is derived on the basis of physical equations, it can be parameterized as a function of a few physical parameters, which are usually not perfectly known in practice. This is e.g. the case in aeronautical systems: as an example, the ae- dynamic model of an airplane is derived from the flight mechanics eq- tions. When synthesizing the aircraft control law, it is then necessary to take into account uncertainties in the values of the stability derivatives, which correspond to the physical coefficients of the aerodynamic model. Moreover, this airplane model does not perfectly represent the be- vior of the real aircraft. As a simple example, the flight control system or the autopilot are usually synthesized just using the aerodynamic model, thus without accounting for the flexible mechanicalstructure: the c- responding dynamics are indeed considered as high frequency neglected 1 dynamics, with respect to the dynamics of the rigid model . Codice articolo 9781475772524
Compra nuovo
EUR 164,49
Spese di spedizione:
EUR 62,27
Da: Germania a: U.S.A.
Quantità: 1 disponibili
Foto dell'editore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Print on DemandDa: Majestic Books, Hounslow, Regno Unito
Valutazione del venditore 4 su 5 stelle
Condizione: New. Print on Demand pp. 236 66:B&W 7 x 10 in or 254 x 178 mm Perfect Bound on White w/Gloss Lam. Codice articolo 94537155
Compra nuovo
EUR 220,07
Spese di spedizione:
EUR 7,44
Da: Regno Unito a: U.S.A.
Quantità: 4 disponibili
Foto dell'editore
A Practical Approach to Robustness Analysis with Aeronautical Applications
Print on DemandDa: Biblios, Frankfurt am main, HESSE, Germania
Valutazione del venditore 4 su 5 stelle
Condizione: New. PRINT ON DEMAND pp. 236. Codice articolo 1897860118
Compra nuovo
EUR 221,97
Spese di spedizione:
EUR 9,95
Da: Germania a: U.S.A.
Quantità: 4 disponibili