Stability And Control of Aircraft Systems: Introduction to Classical Feedback Control - Rilegato

Langton, Roy

 
9780470018910: Stability And Control of Aircraft Systems: Introduction to Classical Feedback Control
Rilegato
ISBN 10: 0470018917 ISBN 13: 9780470018910
Casa editrice: John Wiley & Sons Inc, 2006

Sinossi

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.

Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.

Informazioni sull?autore

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.

Dalla quarta di copertina

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.

Le informazioni nella sezione "Su questo libro" possono far riferimento a edizioni diverse di questo titolo.

Editore
John Wiley & Sons Inc
Data di pubblicazione
2006
Lingua
Inglese
ISBN 10 
0470018917
ISBN 13 
9780470018910
Rilegatura
Copertina rigida
Numero di pagine
238
Contatto del produttore
non disponibile
Persona responsabile
non disponibile

Altre edizioni note dello stesso titolo

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

Edizione in evidenza

ISBN 10:  047005848X ISBN 13:  9780470058480
Casa editrice: John Wiley & Sons Inc, 2006
Rilegato