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Stability and Control of Aircraft Systems: Introduction to Classical Feedback

LostInWa Inc
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eBay item number:326495269528
Last updated on Jun 28, 2025 13:28:33 PDTView all revisionsView all revisions

Item specifics

Condition
Brand New: A new, unread, unused book in perfect condition with no missing or damaged pages. See the ...
Brand
Wiley
Style
ABIS_BOOK
Book Title
Does not apply
ISBN
9780470018910
Subject Area
Technology & Engineering, Science
Publication Name
Stability and Control of Aircraft Systems : Introduction to Classical Feedback Control
Publisher
Wiley & Sons, Incorporated, John
Item Length
9.2 in
Subject
System Theory, Aeronautics & Astronautics
Publication Year
2006
Series
Aerospace Ser.
Type
Textbook
Format
Hardcover
Language
English
Item Height
0.8 in
Author
Roy Langton
Item Weight
17.6 Oz
Item Width
6.2 in
Number of Pages
254 Pages
Category

About this product

Product Identifiers

Publisher
Wiley & Sons, Incorporated, John
ISBN-10
0470018917
ISBN-13
9780470018910
eBay Product ID (ePID)
53948742

Product Key Features

Number of Pages
254 Pages
Publication Name
Stability and Control of Aircraft Systems : Introduction to Classical Feedback Control
Language
English
Publication Year
2006
Subject
System Theory, Aeronautics & Astronautics
Type
Textbook
Author
Roy Langton
Subject Area
Technology & Engineering, Science
Series
Aerospace Ser.
Format
Hardcover

Dimensions

Item Height
0.8 in
Item Weight
17.6 Oz
Item Length
9.2 in
Item Width
6.2 in

Additional Product Features

Intended Audience
Scholarly & Professional
LCCN
2006-015974
Reviews
"Armed with the details in this book a new practitioner could enter any control laboratory and be effective." ( The Aeronautical Journal , March 2008)
Dewey Edition
22
Series Volume Number
10
Illustrated
Yes
Dewey Decimal
629.13236
Table Of Content
Series Preface. Preface. 1. Developing the Foundation. 1.1 Engineering Units. 1.2 Block Diagrams. 1.3 Differential Equations. 1.4 Spring-Mass System Example. 1.5 Primer on Complex Numbers. 1.6 Chapter Summary. 2. Closing the Loop. 2.1 The Generic Closed Loop System. 2.2 The Concept of Stability. 2.3 Response Testing of Control Systems. 2.4 The Integration Process. 2.5 Hydraulic Servo-actuator Example. 2.6 Calculating Frequency Response. 2.7 Aircraft Flight Control System Example. 2.8 Alternative Graphical Methods for Response Analysis. 2.9 Chapter Summary. 3. Control System Compensation Techniques. 3.1 Control System Requirements. 3.2 Compensation Methods. 3.3 Applications of Control Compensation. 3.4 Chapter Summary. 4. Introduction to Laplace Transforms. 4.1 An Overview of the Application of Laplace Transforms. 4.2 The Evolution of the Laplace Transform. 4.2.1 Proof of the General Case. 4.3 Applying Laplace Transforms to Linear Systems Analysis. 4.4 Laplace Transforms - Summary of Key Points. 4.5 Root Locus. 4.6 Root Locus Example. 4.7 Chapter Summary. 5. Dealing with Nonlinearities. 5.1 Definition of Nonlinearity Types. 5.2 Continuous Nonlinearities. 5.3 Discontinuous Nonlinearities. 5.4 The Transport Delay. 5.5 Simulation. 5.6 Chapter Summary. 6. Electronic Controls. 6.1 Analog Electronic Controls. 6.2 The Digital Computer as a Dynamic Control Element. 6.3 The Stability Impact of Digital Controls. 6.4 Digital Control Design Example. 6.5 Creating Digital Control Algorithms. 6.6 Chapter Summary. 7. Concluding Commentary. 7.1 An Overview of the Material. 7.2 Graphical Tools. 7.3 Compensation Techniques. 7.4 Laplace Transforms and Root Locus Techniques. 7.5 Nonlinearities. 7.6 Digital Electronic Control. 7.7 The Way Forward. Index.
Synopsis
Introduction to Feedback Control provides an easy to read and to understand monograph that describes control theory using minimal mathematics and focusing on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples., 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. 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.  Clarifies the design and development of feedback control systems  Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background  Illustrated throughout with figures and tables 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., 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. 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. Clarifies the design and development of feedback control systems Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background Illustrated throughout with figures and tables 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.
LC Classification Number
TL574.S7L35 2006

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