Reduced-Order Short-Period Model of Flexible Aircraft
A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first p...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Giulio Avanzini [verfasserIn] |
|---|
| Format: |
Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
2017 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Journal of guidance, control, and dynamics - New York, NY, 1982, 40(2017), 8, Seite 1 |
|---|---|
| Übergeordnetes Werk: |
volume:40 ; year:2017 ; number:8 ; pages:1 |
| Links: |
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| DOI / URN: |
10.2514/1.G002387 |
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| 520 | |a A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first principles by means of a Lagrangian approach, featuring vertical (heave) and pitch degrees of freedom, together with deformation variables for flexural deformation of wing and after portion of the fuselage. As a byproduct, an explicit formulation for stability derivatives with respect to deformation variables is derived. Numerical results are reported for a configuration representative of a modern commercial jet aircraft. | ||
| 650 | 4 | |a Reduced order models | |
| 650 | 4 | |a First principles | |
| 650 | 4 | |a Flexible aircraft | |
| 650 | 4 | |a Deformation | |
| 650 | 4 | |a Disturbances | |
| 650 | 4 | |a Mathematical models | |
| 650 | 4 | |a Aircraft components | |
| 650 | 4 | |a Commercial aircraft | |
| 650 | 4 | |a Aerodynamics | |
| 650 | 4 | |a Aircraft industry | |
| 650 | 4 | |a Stability derivatives | |
| 650 | 4 | |a Jet aircraft | |
| 650 | 4 | |a Heave | |
| 700 | 0 | |a Francesco Nicassio |4 oth | |
| 700 | 0 | |a Gennaro Scarselli |4 oth | |
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10.2514/1.G002387 doi PQ20171228 (DE-627)OLC1997056437 (DE-599)GBVOLC1997056437 (PRQ)p1503-c942843c07e87cc3791d768dc9d67d2a4298d517fb3895cf89792985a209b270 (KEY)0032738720170000040000800001reducedordershortperiodmodelofflexibleaircraft DE-627 ger DE-627 rakwb eng 380 DNB Giulio Avanzini verfasserin aut Reduced-Order Short-Period Model of Flexible Aircraft 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first principles by means of a Lagrangian approach, featuring vertical (heave) and pitch degrees of freedom, together with deformation variables for flexural deformation of wing and after portion of the fuselage. As a byproduct, an explicit formulation for stability derivatives with respect to deformation variables is derived. Numerical results are reported for a configuration representative of a modern commercial jet aircraft. Reduced order models First principles Flexible aircraft Deformation Disturbances Mathematical models Aircraft components Commercial aircraft Aerodynamics Aircraft industry Stability derivatives Jet aircraft Heave Francesco Nicassio oth Gennaro Scarselli oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 8, Seite 1 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:8 pages:1 http://dx.doi.org/10.2514/1.G002387 Volltext https://search.proquest.com/docview/1897415900 https://search.proquest.com/docview/1919623131 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 8 1 |
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A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first principles by means of a Lagrangian approach, featuring vertical (heave) and pitch degrees of freedom, together with deformation variables for flexural deformation of wing and after portion of the fuselage. As a byproduct, an explicit formulation for stability derivatives with respect to deformation variables is derived. Numerical results are reported for a configuration representative of a modern commercial jet aircraft. |
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A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first principles by means of a Lagrangian approach, featuring vertical (heave) and pitch degrees of freedom, together with deformation variables for flexural deformation of wing and after portion of the fuselage. As a byproduct, an explicit formulation for stability derivatives with respect to deformation variables is derived. Numerical results are reported for a configuration representative of a modern commercial jet aircraft. |
| abstract_unstemmed |
A reduced-order short-period model is derived, which allows for representing the effects of structural flexibility on aircraft response to pilot and disturbance inputs on the basis of a minimum set of relevant information on aerodynamic and structural configuration. The model is derived from first principles by means of a Lagrangian approach, featuring vertical (heave) and pitch degrees of freedom, together with deformation variables for flexural deformation of wing and after portion of the fuselage. As a byproduct, an explicit formulation for stability derivatives with respect to deformation variables is derived. Numerical results are reported for a configuration representative of a modern commercial jet aircraft. |
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| title_short |
Reduced-Order Short-Period Model of Flexible Aircraft |
| url |
http://dx.doi.org/10.2514/1.G002387 https://search.proquest.com/docview/1897415900 https://search.proquest.com/docview/1919623131 |
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| author2 |
Francesco Nicassio Gennaro Scarselli |
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Francesco Nicassio Gennaro Scarselli |
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| doi_str |
10.2514/1.G002387 |
| up_date |
2024-07-04T02:05:31.245Z |
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