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Author Cook, M. V.

Title Flight dynamics principles : a linear systems approach to aircraft stability and control / Mike Cook.

Imprint Waltham, MA : Butterworth-Heinemann, ©2013.

Copies

Location Call No. OPAC Message Status
 Axe Elsevier ScienceDirect Ebook  Electronic Book    ---  Available
Edition 3rd ed.
Description 1 online resource
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series Elsevier aerospace engineering series
Elsevier aerospace engineering series.
Summary 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).
Note Print version record.
Bibliography Includes bibliographical references and index.
Contents A Preface Chapter 1 -- Introduction Chapter 2 -- Systems of axes and notation Chapter 3 -- Static equilibrium and trim Chapter 4 -- The equations of motion Chapter 5 -- The solution of the equations of motion Chapter 6 -- Longitudinal dynamics Chapter 7 -- Lateral-directional dynamics Chapter 8 -- Manoeuvrability Chapter 9 -- Stability Chapter 10 -- Flying and handling qualities Chapter 11 -- Stability augmentation Chapter 12 -- Aerodynamic modelling Chapter 13 -- Aerodynamic stability and control derivatives Chapter 14 -- Coursework studies Chapter 15 -- Flight in a non-steady atmosphere Appendices Index.
Language English.
Subject Aerodynamics.
Aérodynamique.
aerodynamics.
Aerodynamics
Other Form: Print version: Cook, M.V. Flight dynamics principles. Waltham, MA : Butterworth-Heinemann, ©2013 9780080982427 (OCoLC)795763193
ISBN 9780080982762 (electronic bk.)
008098276X (electronic bk.)
9780080982427
0080982425
Standard No. AU@ 000050608399
CHNEW 001010796
DEBBG BV042315057
DEBSZ 405345879
NZ1 15190905
AU@ 000068588637

 
    
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