
Flight Dynamics Principles
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Content
- Front cover
- Flight Dynamics Principles
- Copyright page
- Contents
- Preface to the first edition
- Preface to the second edition
- 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 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
- Chapter 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
- Chapter 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
- 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 controls
- 5.5 Acceleration response transfer functions
- 5.6 The state space method
- 5.7 State space model augmentation
- References
- Problems
- Chapter 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
- 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
- Problems
- Chapter 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
- Chapter 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
- Chapter 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
- 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
- Problems
- Chapter 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
- Chapter 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
- Chapter 14. Coursework Studies
- 14.1 Introduction
- 14.2 Working the assignments
- 14.3 Reporting
- Assignment 1. Stability augmentation of the North American X-15 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 A Very 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 a Wind Axes Reference
- 10 The Transformation of the Moments and Products of Inertia from a Body Axes Reference to a Wind Axes Reference
- 11 The Root Locus Plot
- Index
- A
- B
- C
- D
- E
- F
- G
- H
- I
- J
- K
- L
- M
- N
- O
- P
- Q
- R
- S
- T
- U
- V
- W
- Y
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