| 000 -LEADER |
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| fixed length control field |
04909cam a22004454a 4500 |
| 001 - CONTROL NUMBER |
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| control field |
14374735 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
CITU |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20230217172058.0 |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION |
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| fixed length control field |
cr an aaaaa |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
060512s2006 enka 001 0 eng |
| 010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
|---|
| LC control number |
2006015974 |
| 015 ## - NATIONAL BIBLIOGRAPHY NUMBER |
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| National bibliography number |
GBA657245 |
| Source |
bnb |
| 016 7# - NATIONAL BIBLIOGRAPHIC AGENCY CONTROL NUMBER |
|---|
| Record control number |
013499600 |
| Source |
Uk |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9780470058480 (ebook) |
| 035 ## - SYSTEM CONTROL NUMBER |
|---|
| System control number |
(OCoLC)ocm68800121 |
| 035 ## - SYSTEM CONTROL NUMBER |
|---|
| System control number |
(OCoLC)68800121 |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
DLC |
| Transcribing agency |
DLC |
| Modifying agency |
BAKER |
| -- |
UKM |
| -- |
YDXCP |
| -- |
BWKUK |
| -- |
YDX |
| -- |
BTCTA |
| -- |
COO |
| -- |
IXA |
| -- |
DLC |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng. |
| 042 ## - AUTHENTICATION CODE |
|---|
| Authentication code |
pcc |
| 050 00 - LIBRARY OF CONGRESS CALL NUMBER |
|---|
| Classification number |
TL574.S7 |
| Item number |
L35 2006 |
| 082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
629.13236 |
| Edition number |
22 |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
|---|
| Preferred name for the person |
Langton, Roy. |
| Relator term |
author. |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Stability and control of aircraft systems : |
| Remainder of title |
introduction to classical feedback control / |
| Statement of responsibility, etc |
Roy Langton. |
| 264 #1 - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication, distribution, etc |
Hoboken, New Jersey : |
| Name of publisher, distributor, etc |
John Wiley & Sons, Ltd., |
| Date of publication, distribution, etc |
c2006. |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
1 online resource (254 pages). |
| 336 ## - CONTENT TYPE |
|---|
| Source |
rdacontent |
| Content type term |
text |
| Content type code |
txt |
| 337 ## - MEDIA TYPE |
|---|
| Source |
rdamedia |
| Media type term |
computer |
| Media type code |
c |
| 338 ## - CARRIER TYPE |
|---|
| Source |
rdacarrier |
| Carrier type term |
online resource |
| Carrier type code |
cr |
| 490 0# - SERIES STATEMENT |
|---|
| Series statement |
Aerospace series |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Includes index. |
| 500 ## - GENERAL NOTE |
|---|
| General note |
ABOUT THE AUTHOR<br/>Roy Langton has recently retired from his position as Vice-President, Engineering & Integrity at Parker Aerospace, where he was responsible for internal seminars & training into feedback control. |
| 505 0# - CONTENTS |
|---|
| Formatted contents note |
Series Preface.<br/>Preface.<br/><br/>1. Developing the Foundation.<br/><br/>1.1 Engineering Units.<br/><br/>1.2 Block Diagrams.<br/><br/>1.3 Differential Equations.<br/><br/>1.4 Spring–Mass System Example.<br/><br/>1.5 Primer on Complex Numbers.<br/><br/>1.6 Chapter Summary.<br/><br/>2. Closing the Loop.<br/><br/>2.1 The Generic Closed Loop System.<br/><br/>2.2 The Concept of Stability.<br/><br/>2.3 Response Testing of Control Systems.<br/><br/>2.4 The Integration Process.<br/><br/>2.5 Hydraulic Servo-actuator Example.<br/><br/>2.6 Calculating Frequency Response.<br/><br/>2.7 Aircraft Flight Control System Example.<br/><br/>2.8 Alternative Graphical Methods for Response Analysis.<br/><br/>2.9 Chapter Summary.<br/><br/>3. Control System Compensation Techniques.<br/><br/>3.1 Control System Requirements.<br/><br/>3.2 Compensation Methods.<br/><br/>3.3 Applications of Control Compensation.<br/><br/>3.4 Chapter Summary.<br/><br/>4. Introduction to Laplace Transforms.<br/><br/>4.1 An Overview of the Application of Laplace Transforms.<br/><br/>4.2 The Evolution of the Laplace Transform.<br/><br/>4.2.1 Proof of the General Case.<br/><br/>4.3 Applying Laplace Transforms to Linear Systems Analysis.<br/><br/>4.4 Laplace Transforms – Summary of Key Points.<br/><br/>4.5 Root Locus.<br/><br/>4.6 Root Locus Example.<br/><br/>4.7 Chapter Summary.<br/><br/>5. Dealing with Nonlinearities.<br/><br/>5.1 Definition of Nonlinearity Types.<br/><br/>5.2 Continuous Nonlinearities.<br/><br/>5.3 Discontinuous Nonlinearities.<br/><br/>5.4 The Transport Delay.<br/><br/>5.5 Simulation.<br/><br/>5.6 Chapter Summary.<br/><br/>6. Electronic Controls.<br/><br/>6.1 Analog Electronic Controls.<br/><br/>6.2 The Digital Computer as a Dynamic Control Element.<br/><br/>6.3 The Stability Impact of Digital Controls.<br/><br/>6.4 Digital Control Design Example.<br/><br/>6.5 Creating Digital Control Algorithms.<br/><br/>6.6 Chapter Summary.<br/><br/>7. Concluding Commentary.<br/><br/>7.1 An Overview of the Material.<br/><br/>7.2 Graphical Tools.<br/><br/>7.3 Compensation Techniques.<br/><br/>7.4 Laplace Transforms and Root Locus Techniques.<br/><br/>7.5 Nonlinearities.<br/><br/>7.6 Digital Electronic Control.<br/><br/>7.7 The Way Forward.<br/><br/>Index.<br/> |
| 520 ## - SUMMARY, ETC. |
|---|
| Summary, etc |
In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today’s products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood.<br/>Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.<br/><br/>Clarifies the design and development of feedback control systems<br/>Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background<br/>Illustrated throughout with figures and tables<br/>Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance. |
| 526 ## - STUDY PROGRAM INFORMATION NOTE |
|---|
| -- |
600-699 |
| -- |
629 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name as entry element |
Stability of airplanes. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name as entry element |
Airplanes |
| General subdivision |
Control. |
| 655 #4 - INDEX TERM--GENRE/FORM |
|---|
| Genre/form data or focus term |
Electronic books. |
| 856 ## - ELECTRONIC LOCATION AND ACCESS |
|---|
| Link text |
Full text available at Wiley Online Library Click here to view |
| Uniform Resource Identifier |
https://onlinelibrary.wiley.com/doi/book/10.1002/9780470058480 |
| 942 ## - ADDED ENTRY ELEMENTS |
|---|
| Source of classification or shelving scheme |
|
| Item type |
EBOOK |