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Flight dynamics of aeroelastic vehicles
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Outgoing claims: the papers this work cites, builds on, or argues with.
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Vibrations of shells and plates
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Dynamics of Flight: Stability and Control
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Some remarks on the dynamics of deformable bodies.
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Quadratic synthhesis of integrated active controls for an aeroelastic forward-swept-wing aircraft
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DYNAMIC MODELING UNCERTAINTY AFFECTING CONTROL SYSTEM DESIGN
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Vibrations of Shells and Plates
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Mathematical theory of elasticity
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Aeroservoelastic Design Optimization of a Flexible Wing
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Retrospective and Recent Examples of Aircraft and Rotorcraft System Identification at DLR
inferred← citeshttps://doi.org/10.2514/1.c037820openalex-snapshot
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter
inferred← citeshttps://doi.org/10.2514/1.c038528openalex-snapshot
Analysis of Structural Flexibility Effects on Handling Qualities Using Variable Stability Simulations
inferred← citeshttps://doi.org/10.2514/1.g003980openalex-snapshot
Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion
inferred← citeshttps://doi.org/10.2514/1.g004024openalex-snapshot
Influence of Airframe Flexibility on Pilot-Induced Oscillations
inferred← citeshttps://doi.org/10.2514/1.g004846openalex-snapshot
Robust Modal Damping Control for Active Flutter Suppression
inferred← citeshttps://doi.org/10.2514/1.g005778openalex-snapshot
Data-Driven Retrospective Cost Adaptive Control for Flight Control Applications
inferred← citeshttps://doi.org/10.2514/1.g005783openalex-snapshot
Design of Stability Augmentation Systems for Flexible Aircraft Using Projective Control
inferred← citeshttps://doi.org/10.2514/1.g005870openalex-snapshot
Seamless Active Morphing Wing Simultaneous Gust and Maneuver Load Alleviation
inferred← citeshttps://doi.org/10.2514/1.g005921openalex-snapshot
Nonlinear Incremental Control for Flexible Aircraft Trajectory Tracking and Load Alleviation
inferred← citeshttps://doi.org/10.2514/1.g006084openalex-snapshot
Robust Gust Load Alleviation of Flexible Aircraft Equipped with Lidar
inferred← citeshttps://doi.org/10.2514/1.g007099openalex-snapshot
Reduced-Order Identification of Aeroelastic Systems with Constrained and Imposed Poles
inferred← citeshttps://doi.org/10.2514/1.g007665openalex-snapshot
Flexible Quadrotor Unmanned Aerial Vehicles: Spatially Distributed Modeling and Delay-Resistant Control
inferred← citeshttps://doi.org/10.2514/1.g007984openalex-snapshot
Boosted Incremental Nonlinear Dynamic Inversion for Flexible Airplane Gust Load Alleviation
inferred← citeshttps://doi.org/10.2514/1.g008400openalex-snapshot
Model Reference Control for Reducing Pilot-Induced Oscillation Tendencies
inferred← citeshttps://doi.org/10.2514/1.g009267openalex-snapshot
Combined Design of Gain-Scheduled C-Star and Maneuver Load Alleviation Laws
inferred← citeshttps://doi.org/10.2514/1.j051447openalex-snapshot
Dynamics and Performance of Tailless Micro Aerial Vehicle with Flexible Articulated Wings
inferred← citeshttps://doi.org/10.2514/1.j052316openalex-snapshot
Consistent Structural Linearization in Flexible Aircraft Dynamics with Large Rigid-Body Motion
inferred← citeshttps://doi.org/10.2514/1.j054023openalex-snapshot
Experimental Validation of a Flight Simulation Model for Slightly Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.j054752openalex-snapshot
Formulation of the Flight Dynamics of Flexible Aircraft Using General Body Axes
inferred← citeshttps://doi.org/10.2514/1.j058019openalex-snapshot
Reduced-Order Dynamic Model of a Morphing Airborne Wind Energy Aircraft
inferred← citeshttps://doi.org/10.2514/1.j058243openalex-snapshot
Nonintrusive Computation of Rigid-Body/Flexible-Body Coupling Integrals
inferred← citeshttps://doi.org/10.2514/1.j058976openalex-snapshot
Coupled Flight Dynamics and Thermoelasticity Model of Maneuvering Aircraft
inferred← citeshttps://doi.org/10.2514/1.j059102openalex-snapshot
Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization
inferred← citeshttps://doi.org/10.2514/1.j059621openalex-snapshot
Concurrent Design and Flight Mission Optimization of Morphing Airborne Wind Energy Wings
inferred← citeshttps://doi.org/10.2514/1.j060960openalex-snapshot
Flexible Aircraft Simulation Validation with Flight Test Data
inferred← citeshttps://doi.org/10.2514/1.j065498openalex-snapshot
Unified Aeroelastic and Flight Dynamics Formulation Based on State-Space Unsteady Aerodynamics
inferred← citeshttps://doi.org/10.2514/1.j066068openalex-snapshot
Rigid–Elastic Coupling Aeroelastic Modeling for Flexible Aircraft: From a Gibbs Function Perspective
inferred← citeshttps://doi.org/10.2514/2.2419openalex-snapshot
Integrated Aeroservoelastic Optimization: Status and Direction
inferred← citeshttps://doi.org/10.2514/2.2685openalex-snapshot
Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow
inferred← citeshttps://doi.org/10.2514/2.2738openalex-snapshot
Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
inferred← citeshttps://doi.org/10.2514/2.3012openalex-snapshot
Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks
inferred← citeshttps://doi.org/10.2514/2.3013openalex-snapshot
Flight Testing Radar Detection of the Saab 105 in Level Flight
inferred← citeshttps://doi.org/10.2514/2.4170openalex-snapshot
Analytical Relationships for Linear Quadratic Aeroelastic Flight Control Eigenvalues
inferred← citeshttps://doi.org/10.2514/2.4727openalex-snapshot
Output-Rate Weighted Optimal Control of Aeroelastic Systems
inferred← citeshttps://doi.org/10.2514/2.4744openalex-snapshot
Modeling and Simulation of Flexible Flight Vehicles
inferred← citeshttps://doi.org/10.2514/2.7639openalex-snapshot
Horizontal Control Effector Sizing for Supersonic Transport Aircraft
inferred← citeshttps://doi.org/10.2514/2.838openalex-snapshot
Coupled Helicopter Rotor/Flexible Fuselage Aeroelastic Model for Control of Structural Response
inferred← citeshttps://doi.org/10.2514/3.20735openalex-snapshot
Numerical and literal aeroelastic-vehicle-model reduction for feedback control synthesis
inferred← citeshttps://doi.org/10.2514/3.21326openalex-snapshot
Aeroelastic vehicle multivariable control synthesis with analytical robustness evaluation
inferred← citeshttps://doi.org/10.2514/3.21505openalex-snapshot
Flexible vehicle control using quantitative feedback theory
inferred← citeshttps://doi.org/10.2514/3.21507openalex-snapshot
Unified literal approximations for longitudinal dynamics of flexible flight vehicles
inferred← citeshttps://doi.org/10.2514/3.45972openalex-snapshot
Towards integrated multidisciplinary synthesis of actively controlled fiber composite wings
inferred← citeshttps://doi.org/10.2514/3.46510openalex-snapshot
Parameter estimates of an aeroelastic aircraft as affected by model simplifications
inferred← citeshttps://doi.org/10.2514/3.46511openalex-snapshot
Effects of model scale on flight characteristics and design parameters
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