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The Resource Advanced UAV aerodynamics, flight stability, and control : novel concepts, theory and applications, edited by Pascual Marques, Andrea Da Ronch

Advanced UAV aerodynamics, flight stability, and control : novel concepts, theory and applications, edited by Pascual Marques, Andrea Da Ronch

Label
Advanced UAV aerodynamics, flight stability, and control : novel concepts, theory and applications
Title
Advanced UAV aerodynamics, flight stability, and control
Title remainder
novel concepts, theory and applications
Statement of responsibility
edited by Pascual Marques, Andrea Da Ronch
Contributor
Subject
Language
eng
Member of
Dewey number
629.13339
Index
index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
http://library.link/vocab/relatedWorkOrContributorName
  • Marques, Pascual
  • Da Ronch, Andrea
Series statement
Aerospace series
http://library.link/vocab/subjectName
Drone aircraft
Label
Advanced UAV aerodynamics, flight stability, and control : novel concepts, theory and applications, edited by Pascual Marques, Andrea Da Ronch
Instantiates
Publication
Antecedent source
unknown
Bibliography note
Includes bibliographical references and index
Color
multicolored
Contents
  • Title Page ; Copyright Page; Contents; List of Contributors; Series Preface; Preface; Companion Website; Chapter 1 Advanced UAV Aerodynamics, Flight Stability and Control:: An Introduction; 1.1 Unmanned Aircraft Aerodynamics; 1.2 UAV Flight Stability and Control; Chapter 2 Aerodynamics of UAV Configurations ; 2.1 Introduction; 2.2 Emerging Technologies in UAV Aerodynamics; 2.3 Aerodynamics and Stealth Compromises; 2.4 Rotor Blade Tip Aerodynamics; 2.5 Flight Dynamics of Canard Aircraft; 2.6 Aerodynamics of the UCAV 1303 Delta‐wing Configuration
  • 2.7 Flow Structure Modification using Plasma Actuators2.8 Conclusion; References; Part I Novel Concepts in Unmanned Aircraft Aerodynamics ; 1.1 Fixed-wing (airplanes); Chapter 3 Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles ; 3.1 Introduction; 3.2 Vehicle Description; 3.3 Flight Scenario and Flow‐regime Assessment; 3.4 Rarefied and Transitional Regimes; 3.5 Viscous-interaction Regime ; 3.6 High-temperature Real-gas Regime ; 3.7 Laminar-to-turbulent Transition Assessment ; 3.8 Design Approach and Tools; 3.9 Aerodynamic Characterization
  • 3.10 Low-order Methods Aerodynamic Results 3.11 CFD-based Aerodynamic Results ; References; Chapter 4 Nonlinear Reduced-order Aeroservoelastic Analysis of Very Flexible Aircraft ; 4.1 Introduction; 4.2 Large Coupled Computational Models; 4.3 Coupled Reduced-order Models ; 4.4 Control System Design; 4.5 Conclusion; 4.6 Exercises; References; Chapter 5 Unmanned Aircraft Wind Tunnel Testing ; 5.1 Introduction; 5.2 The Diana UAV Project; 5.3 Experimental Facility; 5.4 Force and Moment Measurements; 5.5 Wind Tunnel and CFD Comparisons; 5.6 Flow Visualization; 5.7 Summary and Conclusions
  • AcknowledgmentsReferences; Chapter 6 Chord-dominated Ground-effect Aerodynamics of Fixed-wing UAVs ; 6.1 Introduction; 6.2 Categories of Ground Effect; 6.3 Chord-dominated Static Ground Effect ; 6.4 Chord-dominated Dynamic Ground Effect ; 6.5 Chord-dominated Mutational Ground Effect ; Acknowledgments; References; 1.2 Rotary-wing (helicopter) ; Chapter 7 Dynamics Modelling and System Identification of Small Unmanned Helicopters ; 7.1 Introduction; 7.2 Model Development; 7.3 System Identification; 7.4 Basic Control Design; 7.5 Conclusion; Bibliography
  • Chapter 8 Aerodynamic Derivative Calculation Using Radial Basis Function Neural Networks 8.1 Introduction; 8.2 Helicopter Aerodynamic Derivatives; 8.3 Radial Basis Function Neural Networks; 8.4 The Delta Method; 8.5 Parameter Estimation Using Simulated Data; 8.6 Parameter Estimation Using Flight Data; 8.7 Delta Method with Flight Data; 8.8 Summary; Acknowledgements; References; Chapter 9 Helicopter BERP Tip: Literature Review of Helicopter Blade Shape Optimisation Methods ; 9.1 Introduction; 9.2 Literature Review; 9.3 Summary; Bibliography
Control code
ocn983834089
Dimensions
unknown
Edition
First edition
Extent
1 online resource (xvii, 754 pages)
File format
unknown
Form of item
online
Isbn
9781118928691
Level of compression
unknown
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
(OCoLC)983834089
Label
Advanced UAV aerodynamics, flight stability, and control : novel concepts, theory and applications, edited by Pascual Marques, Andrea Da Ronch
Publication
Antecedent source
unknown
Bibliography note
Includes bibliographical references and index
Color
multicolored
Contents
  • Title Page ; Copyright Page; Contents; List of Contributors; Series Preface; Preface; Companion Website; Chapter 1 Advanced UAV Aerodynamics, Flight Stability and Control:: An Introduction; 1.1 Unmanned Aircraft Aerodynamics; 1.2 UAV Flight Stability and Control; Chapter 2 Aerodynamics of UAV Configurations ; 2.1 Introduction; 2.2 Emerging Technologies in UAV Aerodynamics; 2.3 Aerodynamics and Stealth Compromises; 2.4 Rotor Blade Tip Aerodynamics; 2.5 Flight Dynamics of Canard Aircraft; 2.6 Aerodynamics of the UCAV 1303 Delta‐wing Configuration
  • 2.7 Flow Structure Modification using Plasma Actuators2.8 Conclusion; References; Part I Novel Concepts in Unmanned Aircraft Aerodynamics ; 1.1 Fixed-wing (airplanes); Chapter 3 Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles ; 3.1 Introduction; 3.2 Vehicle Description; 3.3 Flight Scenario and Flow‐regime Assessment; 3.4 Rarefied and Transitional Regimes; 3.5 Viscous-interaction Regime ; 3.6 High-temperature Real-gas Regime ; 3.7 Laminar-to-turbulent Transition Assessment ; 3.8 Design Approach and Tools; 3.9 Aerodynamic Characterization
  • 3.10 Low-order Methods Aerodynamic Results 3.11 CFD-based Aerodynamic Results ; References; Chapter 4 Nonlinear Reduced-order Aeroservoelastic Analysis of Very Flexible Aircraft ; 4.1 Introduction; 4.2 Large Coupled Computational Models; 4.3 Coupled Reduced-order Models ; 4.4 Control System Design; 4.5 Conclusion; 4.6 Exercises; References; Chapter 5 Unmanned Aircraft Wind Tunnel Testing ; 5.1 Introduction; 5.2 The Diana UAV Project; 5.3 Experimental Facility; 5.4 Force and Moment Measurements; 5.5 Wind Tunnel and CFD Comparisons; 5.6 Flow Visualization; 5.7 Summary and Conclusions
  • AcknowledgmentsReferences; Chapter 6 Chord-dominated Ground-effect Aerodynamics of Fixed-wing UAVs ; 6.1 Introduction; 6.2 Categories of Ground Effect; 6.3 Chord-dominated Static Ground Effect ; 6.4 Chord-dominated Dynamic Ground Effect ; 6.5 Chord-dominated Mutational Ground Effect ; Acknowledgments; References; 1.2 Rotary-wing (helicopter) ; Chapter 7 Dynamics Modelling and System Identification of Small Unmanned Helicopters ; 7.1 Introduction; 7.2 Model Development; 7.3 System Identification; 7.4 Basic Control Design; 7.5 Conclusion; Bibliography
  • Chapter 8 Aerodynamic Derivative Calculation Using Radial Basis Function Neural Networks 8.1 Introduction; 8.2 Helicopter Aerodynamic Derivatives; 8.3 Radial Basis Function Neural Networks; 8.4 The Delta Method; 8.5 Parameter Estimation Using Simulated Data; 8.6 Parameter Estimation Using Flight Data; 8.7 Delta Method with Flight Data; 8.8 Summary; Acknowledgements; References; Chapter 9 Helicopter BERP Tip: Literature Review of Helicopter Blade Shape Optimisation Methods ; 9.1 Introduction; 9.2 Literature Review; 9.3 Summary; Bibliography
Control code
ocn983834089
Dimensions
unknown
Edition
First edition
Extent
1 online resource (xvii, 754 pages)
File format
unknown
Form of item
online
Isbn
9781118928691
Level of compression
unknown
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
(OCoLC)983834089

Library Locations

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