
Flight Dynamics and System Identification for Modern Feedback Control
Avian-Inspired Robots
Description
Key Features
- Presents experimental flight data for validation and verification of modelled dynamics, thus illustrating the deficiencies and difficulties associated with modelling flapping-wing flight
- Derives a new flight dynamics model needed to model avian-inspired vehicles, based on nonlinear multibody dynamics
- Extracts aerodynamic models of flapping flight from experimental flight data and system identification techniques
Readership
Table of Contents
Dedication
List of figures
List of tables
Nomenclature
Preface
About the authors
Chapter 1: Introduction
Abstract:
1.1 Background and motivation
1.2 Bio-inspired flapping wing aircraft
1.3 Flapping-wing literature review
1.4 Scope and contributions of current research
Chapter 2: Ornithopter test platform characterizations
Abstract:
2.1 Mathematical representation of an aircraft
2.2 Ornithopter aircraft description
2.3 Measurements from flight data
2.4 Configuration-dependent mass distribution
2.5 Quasi-hover aerodynamics
2.6 Implications for flight dynamics modeling
2.7 Chapter summary
Chapter 3: Rigid multibody vehicle dynamics
Abstract:
3.1 Model configuration
3.2 Kinematic equations of motion
3.3 Dynamic equations of motion
3.4 Chapter summary
Chapter 4: System identification of aerodynamic models
Abstract:
4.1 System identification method
4.2 Tail aerodynamics
4.3 Wing aerodynamics
4.4 Chapter summary
Chapter 5: Simulation results
Abstract:
5.1 Software simulation architecture
5.2 Determining trim solutions
5.3 Numerical linearization about straight and level mean flight
5.4 Modeling implications for control
5.5 Chapter summary
Chapter 6: Concluding remarks
Abstract:
6.1 Summary of work
6.2 Summary of modeling assumptions
6.3 Summary of original contributions
6.4 Recommendations for future research
Appendix A: Field calibration of inertial measurement units
Appendix B: Actuator dynamics system identification
Appendix C: Equations of motion for single-body flight vehicles
Appendix D: Linearization of a conventional aircraft model
References
Index
Product details
- No. of pages: 160
- Language: English
- Copyright: © Woodhead Publishing 2013
- Published: August 31, 2013
- Imprint: Woodhead Publishing
- eBook ISBN: 9780857094674
- Hardcover ISBN: 9780857094667
About the Authors
Jared Grauer
Affiliations and Expertise
James Hubbard Jr.
Affiliations and Expertise
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