Robust Aeroservoelastic Stability Analysis: Flight Test Applications
The series Advances in Industrial Control aims to report and encourage technology transfer in control engineering. The rapid development of control technology impacts all areas of the control discipline. New theory, new controllers, actuators, sensors, new industrial processes, computer methods, new...
Gespeichert in:
Hauptverfasser: | , |
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Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
London
Springer London
1999
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Schriftenreihe: | Advances in Industrial Control
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Schlagworte: | |
Online-Zugang: | BTU01 Volltext |
Zusammenfassung: | The series Advances in Industrial Control aims to report and encourage technology transfer in control engineering. The rapid development of control technology impacts all areas of the control discipline. New theory, new controllers, actuators, sensors, new industrial processes, computer methods, new applications, new philosophies, . . . . , new challenges. Much of this deVelopment work resides in industrial reports, feasibility study papers and the reports of advanced collaborative projects. The series offers an opportunity for researchers to present an extended exposition of such new work in all aspects of industrial control for wider and rapid dissemination. The high performance control systems applications in aerospace and astronautics almost have a tradition of exploiting the most advanced control theoretical developments first. The optimal control and ffitering paradigm associated with the names of Kalman, Bucy, Anderson and Moore found application in the astronautics of the 1960'S and 1970'S. At the beginning of the 1980'S, control theory moved on to robustness, singular values and mu-analysis. This new work was associated with the names of Zames, Doyle, Glover, Balas among others. The Advances in Industrial Control monograph series have published several volumes over the years which have archived the applications experience garnered from applying robust control to the aerospace sector problems. Rick Lind and Marty Brenner add to this set with their volume on robust aeroservoelastic stability. This volume reports the application of the structured singular value to aeroelastic and aeroservoelastic aerospace problems |
Beschreibung: | 1 Online-Ressource (XV, 205 p) |
ISBN: | 9781447108498 |
DOI: | 10.1007/978-1-4471-0849-8 |
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Datensatz im Suchindex
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any_adam_object | |
author | Lind, Rick Brenner, Marty |
author_facet | Lind, Rick Brenner, Marty |
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id | DE-604.BV045187934 |
illustrated | Not Illustrated |
indexdate | 2024-07-10T08:11:00Z |
institution | BVB |
isbn | 9781447108498 |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030577111 |
oclc_num | 1053845835 |
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owner | DE-634 |
owner_facet | DE-634 |
physical | 1 Online-Ressource (XV, 205 p) |
psigel | ZDB-2-ENG ZDB-2-ENG_Archiv ZDB-2-ENG ZDB-2-ENG_Archiv |
publishDate | 1999 |
publishDateSearch | 1999 |
publishDateSort | 1999 |
publisher | Springer London |
record_format | marc |
series2 | Advances in Industrial Control |
spelling | Lind, Rick Verfasser aut Robust Aeroservoelastic Stability Analysis Flight Test Applications by Rick Lind, Marty Brenner London Springer London 1999 1 Online-Ressource (XV, 205 p) txt rdacontent c rdamedia cr rdacarrier Advances in Industrial Control The series Advances in Industrial Control aims to report and encourage technology transfer in control engineering. The rapid development of control technology impacts all areas of the control discipline. New theory, new controllers, actuators, sensors, new industrial processes, computer methods, new applications, new philosophies, . . . . , new challenges. Much of this deVelopment work resides in industrial reports, feasibility study papers and the reports of advanced collaborative projects. The series offers an opportunity for researchers to present an extended exposition of such new work in all aspects of industrial control for wider and rapid dissemination. The high performance control systems applications in aerospace and astronautics almost have a tradition of exploiting the most advanced control theoretical developments first. The optimal control and ffitering paradigm associated with the names of Kalman, Bucy, Anderson and Moore found application in the astronautics of the 1960'S and 1970'S. At the beginning of the 1980'S, control theory moved on to robustness, singular values and mu-analysis. This new work was associated with the names of Zames, Doyle, Glover, Balas among others. The Advances in Industrial Control monograph series have published several volumes over the years which have archived the applications experience garnered from applying robust control to the aerospace sector problems. Rick Lind and Marty Brenner add to this set with their volume on robust aeroservoelastic stability. This volume reports the application of the structured singular value to aeroelastic and aeroservoelastic aerospace problems Engineering Engineering Design Manufacturing, Machines, Tools Automotive Engineering Engineering design Automotive engineering Manufacturing industries Machines Tools Mathematisches Modell (DE-588)4114528-8 gnd rswk-swf Robustheit (DE-588)4126481-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Aeroelastizität (DE-588)4202469-9 gnd rswk-swf Dynamische Stabilität (DE-588)4226399-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 s Aeroelastizität (DE-588)4202469-9 s Robustheit (DE-588)4126481-2 s Dynamische Stabilität (DE-588)4226399-2 s Mathematisches Modell (DE-588)4114528-8 s 1\p DE-604 Brenner, Marty aut Erscheint auch als Druck-Ausgabe 9781447112150 https://doi.org/10.1007/978-1-4471-0849-8 Verlag URL des Erstveröffentlichers Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
spellingShingle | Lind, Rick Brenner, Marty Robust Aeroservoelastic Stability Analysis Flight Test Applications Engineering Engineering Design Manufacturing, Machines, Tools Automotive Engineering Engineering design Automotive engineering Manufacturing industries Machines Tools Mathematisches Modell (DE-588)4114528-8 gnd Robustheit (DE-588)4126481-2 gnd Flugzeug (DE-588)4017672-1 gnd Aeroelastizität (DE-588)4202469-9 gnd Dynamische Stabilität (DE-588)4226399-2 gnd |
subject_GND | (DE-588)4114528-8 (DE-588)4126481-2 (DE-588)4017672-1 (DE-588)4202469-9 (DE-588)4226399-2 |
title | Robust Aeroservoelastic Stability Analysis Flight Test Applications |
title_auth | Robust Aeroservoelastic Stability Analysis Flight Test Applications |
title_exact_search | Robust Aeroservoelastic Stability Analysis Flight Test Applications |
title_full | Robust Aeroservoelastic Stability Analysis Flight Test Applications by Rick Lind, Marty Brenner |
title_fullStr | Robust Aeroservoelastic Stability Analysis Flight Test Applications by Rick Lind, Marty Brenner |
title_full_unstemmed | Robust Aeroservoelastic Stability Analysis Flight Test Applications by Rick Lind, Marty Brenner |
title_short | Robust Aeroservoelastic Stability Analysis |
title_sort | robust aeroservoelastic stability analysis flight test applications |
title_sub | Flight Test Applications |
topic | Engineering Engineering Design Manufacturing, Machines, Tools Automotive Engineering Engineering design Automotive engineering Manufacturing industries Machines Tools Mathematisches Modell (DE-588)4114528-8 gnd Robustheit (DE-588)4126481-2 gnd Flugzeug (DE-588)4017672-1 gnd Aeroelastizität (DE-588)4202469-9 gnd Dynamische Stabilität (DE-588)4226399-2 gnd |
topic_facet | Engineering Engineering Design Manufacturing, Machines, Tools Automotive Engineering Engineering design Automotive engineering Manufacturing industries Machines Tools Mathematisches Modell Robustheit Flugzeug Aeroelastizität Dynamische Stabilität |
url | https://doi.org/10.1007/978-1-4471-0849-8 |
work_keys_str_mv | AT lindrick robustaeroservoelasticstabilityanalysisflighttestapplications AT brennermarty robustaeroservoelasticstabilityanalysisflighttestapplications |