Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles
- Author
- JACKSON, T1 ; LIVNE, E1
[1] University of Washington, Seattle 98195-2400, Washington, United States - Conference name
- AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (46 ; Austin, TX 2005-04-20)
- Source
AIAA journal. 2014, Vol 52, Num 6, pp 1105-1123, 19 p ; ref : 46 ref
- CODEN
- AIAJAH
- ISSN
- 0001-1452
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- Analyse sensibilité Aérodynamique Aéronef Aéroélasticité Commande vol Conception ingénierie Conception intégrée Contrainte Contrôle vibration Engin volant autonome Microaéronef Modélisation Mécanique fluide numérique Méthode domaine temps fréquence Méthode élément fini Optimisation Processus conception Programmation non linéaire Système actif Variabilité réponse
- Keyword (en)
- Sensitivity analysis Aerodynamics Aircraft Aeroelasticity Flight control Engineering design Integrated design Constraint Vibration control Unmanned aerial vehicle Microaircraft Modeling Computational fluid dynamics Time frequency domain method Finite element method Optimization Design process Non linear programming Active system Response variability
- Keyword (es)
- Análisis sensibilidad Aerodinámica Aeronave Aeroelasticidad Control vuelo Concepción ingeniería Concepción integrada Coacción Control vibración Máquina autónoma voleando Microaeronave Modelización Mecánica fluido numérica Método dominio tiempo frecuencia Método elemento finito Optimización Proceso concepcion Programación no lineal Sistema activo Variabilidad respuesta
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30M Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G11 Computational methods in fluid dynamics
- Discipline
- Physics : fluid mechanics Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 28599034
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Access to the document
Install on your browser
DOI
10.2514/1.J050941 
https://dx.doi.org/10.2514/1.J050941
"O:13:\"PanistOpenUrl\":36:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000idc\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:9:\"\u0000*\u0000jtitle\";s:12:\"AIAA journal\";s:9:\"\u0000*\u0000stitle\";s:6:\"AIAA j\";s:7:\"\u0000*\u0000date\";s:4:\"2014\";s:9:\"\u0000*\u0000volume\";s:2:\"52\";s:8:\"\u0000*\u0000issue\";s:1:\"6\";s:8:\"\u0000*\u0000spage\";s:4:\"1105\";s:8:\"\u0000*\u0000epage\";s:4:\"1123\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0001-1452\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"JACKSON\";s:10:\"\u0000*\u0000aufirst\";s:1:\"T\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:8:\"LIVNE, E\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"AIAJAH\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"19\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Panist access
"O:12:\"IstexOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:9:\"\u0000*\u0000jtitle\";s:12:\"AIAA journal\";s:9:\"\u0000*\u0000stitle\";s:6:\"AIAA j\";s:7:\"\u0000*\u0000date\";s:4:\"2014\";s:9:\"\u0000*\u0000volume\";s:2:\"52\";s:8:\"\u0000*\u0000issue\";s:1:\"6\";s:8:\"\u0000*\u0000spage\";s:4:\"1105\";s:8:\"\u0000*\u0000epage\";s:4:\"1123\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0001-1452\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"JACKSON\";s:10:\"\u0000*\u0000aufirst\";s:1:\"T\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:8:\"LIVNE, E\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"AIAJAH\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"19\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Istex access
"O:16:\"UnpaywallOpenUrl\":35:{s:8:\"\u0000*\u0000email\";s:27:\"assistance-portail@inist.fr\";s:6:\"\u0000*\u0000fmt\";N;s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";N;s:7:\"\u0000*\u0000pmid\";N;s:9:\"\u0000*\u0000atitle\";N;s:9:\"\u0000*\u0000jtitle\";N;s:9:\"\u0000*\u0000stitle\";N;s:7:\"\u0000*\u0000date\";N;s:9:\"\u0000*\u0000volume\";N;s:8:\"\u0000*\u0000issue\";N;s:8:\"\u0000*\u0000spage\";N;s:8:\"\u0000*\u0000epage\";N;s:8:\"\u0000*\u0000pages\";N;s:7:\"\u0000*\u0000issn\";N;s:8:\"\u0000*\u0000eissn\";N;s:9:\"\u0000*\u0000aulast\";N;s:10:\"\u0000*\u0000aufirst\";N;s:9:\"\u0000*\u0000auinit\";N;s:10:\"\u0000*\u0000auinitm\";N;s:5:\"\u0000*\u0000au\";N;s:9:\"\u0000*\u0000aucorp\";N;s:7:\"\u0000*\u0000isbn\";N;s:8:\"\u0000*\u0000coden\";N;s:8:\"\u0000*\u0000genre\";N;s:7:\"\u0000*\u0000part\";N;s:9:\"\u0000*\u0000btitle\";N;s:8:\"\u0000*\u0000title\";N;s:8:\"\u0000*\u0000place\";N;s:6:\"\u0000*\u0000pub\";N;s:10:\"\u0000*\u0000edition\";N;s:9:\"\u0000*\u0000tpages\";N;s:9:\"\u0000*\u0000series\";N;s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";N;}"
Unpaywall access
"O:16:\"EuropePMCOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:9:\"\u0000*\u0000jtitle\";s:12:\"AIAA journal\";s:9:\"\u0000*\u0000stitle\";s:6:\"AIAA j\";s:7:\"\u0000*\u0000date\";s:4:\"2014\";s:9:\"\u0000*\u0000volume\";s:2:\"52\";s:8:\"\u0000*\u0000issue\";s:1:\"6\";s:8:\"\u0000*\u0000spage\";s:4:\"1105\";s:8:\"\u0000*\u0000epage\";s:4:\"1123\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0001-1452\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"JACKSON\";s:10:\"\u0000*\u0000aufirst\";s:1:\"T\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:8:\"LIVNE, E\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"AIAJAH\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"19\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Europe PubMed Central access
"O:11:\"BaseOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:9:\"\u0000*\u0000jtitle\";s:12:\"AIAA journal\";s:9:\"\u0000*\u0000stitle\";s:6:\"AIAA j\";s:7:\"\u0000*\u0000date\";s:4:\"2014\";s:9:\"\u0000*\u0000volume\";s:2:\"52\";s:8:\"\u0000*\u0000issue\";s:1:\"6\";s:8:\"\u0000*\u0000spage\";s:4:\"1105\";s:8:\"\u0000*\u0000epage\";s:4:\"1123\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0001-1452\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"JACKSON\";s:10:\"\u0000*\u0000aufirst\";s:1:\"T\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:8:\"LIVNE, E\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"AIAJAH\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"19\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Base Search access
"O:12:\"ArXivOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:17:\"10.2514\/1.J050941\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:9:\"\u0000*\u0000jtitle\";s:12:\"AIAA journal\";s:9:\"\u0000*\u0000stitle\";s:6:\"AIAA j\";s:7:\"\u0000*\u0000date\";s:4:\"2014\";s:9:\"\u0000*\u0000volume\";s:2:\"52\";s:8:\"\u0000*\u0000issue\";s:1:\"6\";s:8:\"\u0000*\u0000spage\";s:4:\"1105\";s:8:\"\u0000*\u0000epage\";s:4:\"1123\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0001-1452\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"JACKSON\";s:10:\"\u0000*\u0000aufirst\";s:1:\"T\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:8:\"LIVNE, E\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"AIAJAH\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:102:\"Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"19\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
arXiv access
