Flight dynamics principles: a linear systems approach to aircraft stability and control
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
Amsterdam ; Boston ; Heidelberg ; London ; New York ; Oxford ; Paris ; San Diego ; San Francisco ; Singapore ; Sydney ; Tokio
Butterworth-Heinemann
2013
|
Ausgabe: | Third edition |
Schlagworte: | |
Online-Zugang: | BTU01 FLA01 FUBA1 TUM01 UBY01 Volltext |
Beschreibung: | 1 Online-Ressource (xxxi, 575 Seiten) |
ISBN: | 0080982425 9780080982762 008098276X |
Internformat
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505 | 8 | |a The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. About the author: After graduating Michael Cook joined Elliott Flight Automation as a Systems Engineer and contributed flight control systems design to several major projects. Later he joined the College of Aeronautics to research and teach flight dynamics, experimental flight mechanics and flight control. Previously leader of the Dynamics, Simulation and Control Research Group he is now retired and continues to provide part time support. In 2003 the Group was recognised as the Preferred Academic Capability Partner for Flight Dynamics by BAE SYSTEMS and in 2007 he received a Chairman's Bronze award for his contribution to a joint UAV research programme. New to this edition: Additional examples to illustrate the application of computational procedures using tools such as MATLABª, MathCadª and Program CCª. Improved compatibility with, and more expansive coverage of the North American notational style. Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence. An additional coursework study on flight control design for an unmanned air vehicle (UAV) | |
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Datensatz im Suchindex
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---|---|
any_adam_object | |
author | Cook, Mike |
author_facet | Cook, Mike |
author_role | aut |
author_sort | Cook, Mike |
author_variant | m c mc |
building | Verbundindex |
bvnumber | BV042315057 |
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contents | The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. About the author: After graduating Michael Cook joined Elliott Flight Automation as a Systems Engineer and contributed flight control systems design to several major projects. Later he joined the College of Aeronautics to research and teach flight dynamics, experimental flight mechanics and flight control. Previously leader of the Dynamics, Simulation and Control Research Group he is now retired and continues to provide part time support. In 2003 the Group was recognised as the Preferred Academic Capability Partner for Flight Dynamics by BAE SYSTEMS and in 2007 he received a Chairman's Bronze award for his contribution to a joint UAV research programme. New to this edition: Additional examples to illustrate the application of computational procedures using tools such as MATLABª, MathCadª and Program CCª. Improved compatibility with, and more expansive coverage of the North American notational style. Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence. An additional coursework study on flight control design for an unmanned air vehicle (UAV) |
ctrlnum | (OCoLC)818173505 (DE-599)BVBBV042315057 |
dewey-full | 629.132/3 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.132/3 |
dewey-search | 629.132/3 |
dewey-sort | 3629.132 13 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehrstechnik Verkehr / Transport |
edition | Third edition |
format | Electronic eBook |
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id | DE-604.BV042315057 |
illustrated | Not Illustrated |
indexdate | 2024-07-10T01:18:11Z |
institution | BVB |
isbn | 0080982425 9780080982762 008098276X |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027752048 |
oclc_num | 818173505 |
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physical | 1 Online-Ressource (xxxi, 575 Seiten) |
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publishDate | 2013 |
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publisher | Butterworth-Heinemann |
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spelling | Cook, Mike Verfasser aut Flight dynamics principles a linear systems approach to aircraft stability and control Mike Cook Third edition Amsterdam ; Boston ; Heidelberg ; London ; New York ; Oxford ; Paris ; San Diego ; San Francisco ; Singapore ; Sydney ; Tokio Butterworth-Heinemann 2013 1 Online-Ressource (xxxi, 575 Seiten) txt rdacontent c rdamedia cr rdacarrier The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. About the author: After graduating Michael Cook joined Elliott Flight Automation as a Systems Engineer and contributed flight control systems design to several major projects. Later he joined the College of Aeronautics to research and teach flight dynamics, experimental flight mechanics and flight control. Previously leader of the Dynamics, Simulation and Control Research Group he is now retired and continues to provide part time support. In 2003 the Group was recognised as the Preferred Academic Capability Partner for Flight Dynamics by BAE SYSTEMS and in 2007 he received a Chairman's Bronze award for his contribution to a joint UAV research programme. New to this edition: Additional examples to illustrate the application of computational procedures using tools such as MATLABª, MathCadª and Program CCª. Improved compatibility with, and more expansive coverage of the North American notational style. Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence. An additional coursework study on flight control design for an unmanned air vehicle (UAV) Flugmechanik (DE-588)4154760-3 gnd rswk-swf Flugzeugaerodynamik (DE-588)4135410-2 gnd rswk-swf Flugmechanik (DE-588)4154760-3 s DE-604 Flugzeugaerodynamik (DE-588)4135410-2 s 1\p DE-604 Erscheint auch als Druck-Ausgabe 978-0-08-098242-7 http://www.sciencedirect.com/science/book/9780080982427 Verlag Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
spellingShingle | Cook, Mike Flight dynamics principles a linear systems approach to aircraft stability and control The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. About the author: After graduating Michael Cook joined Elliott Flight Automation as a Systems Engineer and contributed flight control systems design to several major projects. Later he joined the College of Aeronautics to research and teach flight dynamics, experimental flight mechanics and flight control. Previously leader of the Dynamics, Simulation and Control Research Group he is now retired and continues to provide part time support. In 2003 the Group was recognised as the Preferred Academic Capability Partner for Flight Dynamics by BAE SYSTEMS and in 2007 he received a Chairman's Bronze award for his contribution to a joint UAV research programme. New to this edition: Additional examples to illustrate the application of computational procedures using tools such as MATLABª, MathCadª and Program CCª. Improved compatibility with, and more expansive coverage of the North American notational style. Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence. An additional coursework study on flight control design for an unmanned air vehicle (UAV) Flugmechanik (DE-588)4154760-3 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd |
subject_GND | (DE-588)4154760-3 (DE-588)4135410-2 |
title | Flight dynamics principles a linear systems approach to aircraft stability and control |
title_auth | Flight dynamics principles a linear systems approach to aircraft stability and control |
title_exact_search | Flight dynamics principles a linear systems approach to aircraft stability and control |
title_full | Flight dynamics principles a linear systems approach to aircraft stability and control Mike Cook |
title_fullStr | Flight dynamics principles a linear systems approach to aircraft stability and control Mike Cook |
title_full_unstemmed | Flight dynamics principles a linear systems approach to aircraft stability and control Mike Cook |
title_short | Flight dynamics principles |
title_sort | flight dynamics principles a linear systems approach to aircraft stability and control |
title_sub | a linear systems approach to aircraft stability and control |
topic | Flugmechanik (DE-588)4154760-3 gnd Flugzeugaerodynamik (DE-588)4135410-2 gnd |
topic_facet | Flugmechanik Flugzeugaerodynamik |
url | http://www.sciencedirect.com/science/book/9780080982427 |
work_keys_str_mv | AT cookmike flightdynamicsprinciplesalinearsystemsapproachtoaircraftstabilityandcontrol |