book

Advanced UAV Aerodynamics, Flight Stability and Control

by Pascual Marqués, Andrea Da Ronch

April 2017

Intermediate to advanced

776 pages

25h 50m

English

Wiley

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1.1 Unmanned Aircraft Aerodynamics1.2 UAV Flight Stability and Control
2.1 Introduction2.2 Emerging Technologies in UAV Aerodynamics2.3 Aerodynamics and Stealth Compromises2.4 Rotor Blade Tip Aerodynamics2.5 Flight Dynamics of Canard Aircraft2.6 Aerodynamics of the UCAV 1303 Delta‐wing Configuration2.7 Flow Structure Modification using Plasma Actuators2.8 ConclusionReferences
1.1 Fixed‐wing (airplanes)
3.1 Introduction3.2 Vehicle Description3.3 Flight Scenario and Flow‐regime Assessment3.4 Rarefied and Transitional Regimes3.5 Viscous‐interaction Regime3.6 High‐temperature Real‐gas Regime3.7 Laminar‐to‐turbulent Transition Assessment3.8 Design Approach and Tools3.9 Aerodynamic Characterization3.10 Low‐order Methods Aerodynamic Results3.11 CFD‐based Aerodynamic ResultsReferences

4.1 Introduction4.2 Large Coupled Computational Models4.3 Coupled Reduced‐order Models4.4 Control System Design4.5 Conclusion4.6 ExercisesReferences
5.1 Introduction5.2 The Diana UAV Project5.3 Experimental Facility5.4 Force and Moment Measurements5.5 Wind Tunnel and CFD Comparisons5.6 Flow Visualization5.7 Summary and ConclusionsAcknowledgmentsReferences
6.1 Introduction6.2 Categories of Ground Effect6.3 Chord‐dominated Static Ground Effect6.4 Chord‐dominated Dynamic Ground Effect6.5 Chord‐dominated Mutational Ground EffectAcknowledgmentsReferences
7.1 Introduction7.2 Model Development7.3 System Identification7.4 Basic Control Design7.5 ConclusionBibliography
8.1 Introduction8.2 Helicopter Aerodynamic Derivatives8.3 Radial Basis Function Neural Networks8.4 The Delta Method8.5 Parameter Estimation Using Simulated Data8.6 Parameter Estimation Using Flight Data8.7 Delta Method with Flight Data8.8 SummaryAcknowledgementsReferences
9.1 Introduction9.2 Literature Review9.3 SummaryBibliography
10.1 Introduction10.2 Numerical Methods10.3 Optimisation Method10.4 Parameterisation Technique10.5 Grid and Geometry Generation10.6 Flight Conditions10.7 Hover Results10.8 Forward Flight Results10.9 Planform Optimisation10.10 Summary and ConclusionsBibliography
11.1 Introduction11.2 Actuation Concepts11.3 Integral Twist Actuation11.4 SummaryReferences
12.1 Why Hover‐to‐Dash Conversion is Important12.2 Aircraft Mission Profiles and Sizing Chart Structure12.3 Convertible Coleopter Design, Wind Tunnel and Flight Testing12.4 Future: Convertible QuadCopter Design and Flight Testing12.5 The Extreme: Hover‐to‐Supersonic Dash AircraftReferences
2.1 Fixed‐wing (airplanes)
13.1 Introduction13.2 Objectives13.3 Actuators13.4 Linear System13.5 Plant Model Identification13.6 Controller Architecture13.7 ConclusionsAcknowledgementReferences
14.1 Introduction14.2 The Composite Spar14.3 The Energy‐harvesting and Storage Component14.4 Reduced Energy Control Law14.5 Gust Modelling14.6 Experimental Validation14.7 Performance14.8 Other Considerations14.9 Summary and DiscussionAcknowledgementReferences
15.1 Introduction15.2 Aerodynamic Model for Flight Simulation15.3 Generation of Tabular Aerodynamic Model15.4 Time‐accurate CFD for Flight Simulations15.5 ConclusionsReferences
16.1 Introduction16.2 Aerodynamic Flow Control16.3 Plasma Actuators16.4 Dielectric Barrier Discharge16.5 Experimental Setup16.6 Results and Analysis16.7 ConclusionsAcknowledgmentsReferences
17.1 Introduction17.2 UAV Dynamics and Internal Constraints17.3 Environmental Constraints17.4 Off‐line CMP17.5 Real‐time CMP17.6 Variable Objective CMP17.7 Summary and ConclusionsReferences
18.1 Introduction and Problem Statement18.2 Concurrent Orbit and Attitude Determination18.3 Concurrent Attitude and System Identification18.4 Summary and ConclusionsReferences
19.1 Introduction19.2 Mathematical Model of Flexible Spacecraft and Problem Formulation19.3 Adaptive Backstepping Fault‐Tolerant Controller Design19.4 Numerical Simulations19.5 ConclusionReferences
20.1 Introduction20.2 Multi‐rotors20.3 Novel Quad‐rotor Concepts20.4 ConclusionsReferencesFurther reading
21.1 Introduction21.2 Quadrotor System and Experimental Infrastructure Overview21.3 System Identification Using CIFER21.4 Flight Testing21.5 System Identification Results and Discussion21.6 Controller Modeling and Validation21.7 Controller Optimization in CONDUIT21.8 ConclusionReferences

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2.2 Quad‐rotor Aircraft

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