- Артикул:00-01050827
- Автор: M.V. Cook
- ISBN: 978-0-7506-6927-6
- Обложка: Твердая обложка
- Издательство: Elsevier Ltd (все книги издательства)
- Город: USA
- Страниц: 490
- Год: 2007
- Вес: 1375 г
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Книга на английском языке.
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.
Contents
Preface to the first edition
Preface to the second edition
Acknowledgements
Nomenclature
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
2. Systems of axes and notation
2.1 Earth axes
2.2 Aircraft body fixed axes
2.3 Euler angles and aircraft attitude
2.4 Axes transformations
2.5 Aircraft reference geometry
2.6 Controls notation
2.7 Aerodynamic reference centres
References
Problems
3. Static equilibrium and trim
3.1 Trim equilibrium
3.2 The pitching moment equation
3.3 Longitudinal static stability
3.4 Lateral static stability
3.5 Directional static stability
3.6 Calculation of aircraft trim condition
References
Problems
4. The equations of motion
4.1 The equations of motion of a rigid symmetric aircraft
4.2 The linearised equations of motion
4.3 The decoupled equations of motion
4.4 Alternative forms of the equations of motion
References
Problems
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 controls
5.5 Acceleration response transfer functions
5.6 The state space method
5.7 State space model augmentation
References
Problems
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
Problems
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
Problems
8. Manoeuvrability
8.1 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
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
Problems
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 requirements
10.7 Control anticipation parameter
10.8 Lateral-directional flying qualities requirements
10.9 Flying qualities requirements on the s-plane
References
Problems
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
Problems
12. Aerodynamic modelling
12.1 Introduction
12.2 Quasi-static derivatives
12.3 Derivative estimation
12.4 The effects of compressibility
12.5 Limitations of aerodynamic modelling
References
13. Aerodynamic stability and control derivatives
13.1 Introduction
13.2 Longitudinal aerodynamic stability derivatives
13.3 Lateral-directional aerodynamic stability derivatives
13.4 Aerodynamic control derivatives
13.5 North American derivative coefficient notation
References
Problems
14. Coursework Studies
14.1 Introduction
14.2 Working the assignments
14.3 Reporting
Assignment 1. Stability augmentation of the North American X-hypersonic research aeroplane
Assignment 2. The stability and control characteristics of a civil transport aeroplane with relaxed longitudinal static stability
Assignment 3. Lateral-directional handling qualities design for the Lockheed F-104 Starfighter aircraft
Assignment 4. Analysis of the effects of Mach number on the longitudinal stability and control characteristics of the LTV A7-A Corsair aircraft
Appendices
1 AeroTrim - A Symmetric Trim Calculator for Subsonic Flight Conditions
2 Definitions of Aerodynamic Stability and Control Derivatives
3 Aircraft Response Transfer Functions Referred to Aircraft Body Axes
4 Units, Conversions and Constants
5 AVery Short Table of Laplace Transforms
6 The Dynamics of a Linear Second Order System
7 North American Aerodynamic Derivative Notation
8 Approximate Expressions for the Dimensionless Aerodynamic Stability and Control Derivatives
9 The Transformation of Aerodynamic Stability Derivatives from a Body Axes Reference to aWind Axes Reference
10 The Transformation of the Moments and Products of Inertia from a Body Axes Reference to aWind Axes Reference
11 The Root Locus Plot
Index
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