Stability and Control of Aircraft Systems: Introduction to Classical Feedback Control (Aerospace Series) - Hardcover

Langton, Roy

 
9780470018910: Stability and Control of Aircraft Systems: Introduction to Classical Feedback Control (Aerospace Series)
Hardcover
ISBN 10: 0470018917 ISBN 13: 9780470018910
Verlag: Wiley, 2006

Inhaltsangabe

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.

Die Inhaltsangabe kann sich auf eine andere Ausgabe dieses Titels beziehen.

Über die Autorin bzw. den Autor

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.

Von der hinteren Coverseite

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.

Aus dem Klappentext

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.

„Über diesen Titel“ kann sich auf eine andere Ausgabe dieses Titels beziehen.

Verlag
Wiley
Erscheinungsdatum
2006
Sprache
Englisch
ISBN 10 
0470018917
ISBN 13 
9780470018910
Einband
Gebundene Ausgabe
Auflage
1
Anzahl der Seiten
254
Kontakt zum Hersteller
Wiley-VCH GmbH
product_safety@wiley.com

Boschstrasse 12
Weinheim
69469
Deutschland

Weitere beliebte Ausgaben desselben Titels

9780470058480: Stability And Control of Aircraft Systems: Introduction to Classical Feedback Control (Aerospace)

Vorgestellte Ausgabe

ISBN 10:  047005848X ISBN 13:  9780470058480
Verlag: John Wiley & Sons Inc, 2006
Hardcover