000			05634cam a2200325 a 4500
999			_c8094 _d8094
001			201202157
005			20201001164425.0
008			120724s2013 ne a b 001 0 eng d
010			_a2012021575
020			_a9780080982427
020			_a0080982425
040			_aDLC _cDLC _dDLC _erda
082	0	0	_a629.1323 _223 _bC.M.F
100	1		_aCook, M. V. _eauthor
245	1	0	_aFlight dynamics principles : _ba linear systems approach to aircraft stability and control / _cMichael V. Cook.
250			_aThirrd edition
264			_aAmsterdam ; _aBoston : _bButterworth-Heinemann, _c[2013]
264		4	_a©2013
300			_axxxi, 575 pages : _billustrations ; _c25 cm.
336			_2rdacontent _atext
337			_2rdamedia _aunmediated
338			_2rdacarrier _avolume
490	0		_aElsevier aerospace engineering series.
504			_aIncludes bibliographical references and index.
505	0		_aFront Cover ; Flight Dynamics Principles; Copyright Page ; Table of Contents; Preface; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aeroplane body fixed axes; 2.3 Euler angles and aeroplane attitude; 2.4 Axes transformations; 2.5 Aeroplane reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres; References. Chapter 3. Static equilibrium and trim3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; References; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aeroplane; 4.2 The linearized equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Chapter 5. The solution of the equations of motion; 5.1 Methods of solution; 5.2 Cramer's rule; 5.3 Aircraft response transfer functions. 5.4 Response to controls5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Chatper 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models; 7.4 Frequency response; 7.5 Flying and handling qualities; 7.6 Mode excitation; References. Chapter 8. Manoeuvrability8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chatper 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Chatper 10. Flying and handling qualities; 10.1 Introduction; 10.2 Short term dynamic models; 10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating. 10.6 Longitudinal flying qualities requirements10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method; References; Chatper 12. Aerodynamic modelling; 12.1 Introduction; 12.2 Quasi-static derivatives; 12.3 Derivative estimation.
520			_aThe 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).
650		0	_aAerodynamics.
942			_cBK _2ddc