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Modern flexible multi-body dynamics modeling methodology for flapping wing vehicles /
Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles presents research on the implementation of a flexible multi-body dynamic representation of a flapping wing ornithopter that considers aero-elasticity. This effort brings advances in the understanding of flapping wing...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
London :
Academic Press,
2018.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; MODERN FLEXIBLE MULTI-BODY DYNAMICS MODELING METHODOLOGY FOR FLAPPING WING VEHICLES; MODERN FLEXIBLE MULTI-BODY DYNAMICS MODELING METHODOLOGY FOR FLAPPING WING VEHICLES ; Copyright; Dedication; CONTENTS; PREFACE; LIST OF FIGURES; LIST OF TABLES; LIST OF NOMENCLATURE; ROMAN SYMBOLS; CAPITAL ROMAN SYMBOLS; GREEK SYMBOLS; SUPERSCRIPTS AND SUBSCRIPTS; ACRONYMS; ACKNOWLEDGMENTS; SUMMARY; One
- Bioinspired Flight Robotics Systems; 1.1 INTRODUCTION OF THIS BODY OF WORK; 1.2 THE BACKGROUND OF FLAPPING WING FLIGHT TECHNOLOGY; 1.2.1 Aerial Vehicles and Natural Flapping Wing Flyers.
- 1.3 A MODEL OF AN ORNITHOPTER FOR PERFORMANCE OPTIMIZATION1.3.1 Desired Improvements in Flight Platforms; 1.3.2 Background and Flapping Wing Flight Aerodynamics; 1.3.2.1 Motion Profile and Wing Gates; 1.3.2.2 Wing Flexibility; 1.3.2.3 Wing Geometry; 1.4 HISTORICAL CONSIDERATIONS FOR BIOINSPIRED FLAPPING WINGS AVIAN FLIGHT AND ROBOTICS; 1.5 OBJECTIVES IN THE DEVELOPMENT OF FLEXIBLE MULTI-BODY DYNAMICS THE MODELING METHODOLOGY DESCRIBED IN THIS BODY OF WORK; REFERENCES; Two
- Flexible Multi-Body Dynamics Modeling Methodology's for Flapping Wing Vehicles; 2.1 CLASSIC MODELING METHODOLOGY'S.
- 2.1.1 The Classification of Flexible Multi-Body Systems2.1.2 Flexible Multi-Body Dynamics Modeling; 2.1.3 The Implementation in Available Code and Software; 2.1.4 The Vehicle Dynamics Modeling of Ornithopter; 2.1.5 An Aeroelastic Analysis of Flapping Wing Vehicles; 2.1.6 Related Avian Scale Aerodynamics and Models; 2.2 MODERN MODELING METHODOLOGY; REFERENCES; Three
- Bioinspired Flapping Wing Test Platform Used to Implement Modern Modeling Methodology; 3.1 DETAILS OF THE TEST PLATFORM; 3.2 EXPERIMENTAL DATA SETS OF BIOINSPIRED FLAPING WING ROBOTIC SYSTEM FOR MODEL VERIFICATION.
- 3.2.1 The Clamped Test Experiment-E13.2.1.1 Results of Experiment and Integrated Forces-E1; 3.2.1.2 Wing Kinematics-E-1; 3.2.2 The System-ID Experiment-E1-I; 3.2.2.1 Integrated Aerodynamic Force-E1-I; 3.2.3 Free-Flight Experiment-E2; 3.2.3.1 Results for Wing Kinematics-E-2; 3.2.3.1.1 Total Forces-E2; 3.2.4 Vacuum Camber Experiment-E3; 3.2.4.1 Integrated Inertial Forces-E3; REFERENCES; Four
- Flexible Multi-Body Dynamics Modeling Methodology Implementation Avian Scale Flapping Wing Flyer; 4.1 LINEAR ELASTIC MULTI-BODY SYSTEMS; 4.1.1 A Floating Frame of Reference Formulation.
- 4.2 THE FIVE-BODY MULTI-BODY DYNAMICS MODEL4.3 RELEVANT COORDINATE SYSTEMS; 4.4 AN UNDERLYING ARTICULATED RIGID-BODY MODEL; 4.4.1 The Kinematic Relations; 4.4.1.1 Angular Velocity; 4.4.1.2 Linear Velocity; 4.5 LAGRANGE FORMULATION OF EQUATIONS OF MOTION; 4.5.1 Kinetic Energy Formulation; 4.5.2 Potential Energy Formulation; 4.5.3 The Position Vector and Rigid-Body Equations of Motion; 4.5.4 The Position Vector and Flexible Body Equations of Motion; 4.5.5 The Use of Modal Superposition; 4.6 FORMULATION OF FIVE-BODY FLEXIBLE MULTI-BODY DYNAMICS MODEL.