All Stories

  1. Flight dynamics of aircraft incorporating the semi-aeroelastic hinge
  2. Design and Experimental Investigation of a Benchmark Aeroelastic Wing Model
  3. Experimental and numerical analysis of the bifurcation behaviour of a very flexible wing
  4. Airliner upset — improving our understanding through sub-scale flight testing
  5. Development of a Pressurised Wind Tunnel Mount for Testing Novel Flow Controls for AVT-350-RTG
  6. Wind Tunnel Investigations of a Pitch-Free Flexible High Aspect Ratio Aircraft Model
  7. Aeroelastic scaling of a high aspect ratio wing incorporating semi aeroelastic hinge
  8. Isola in a linear one‐degree‐of‐freedom feedback system with actuator rate saturation
  9. A Graphical Approach to Examining Classical Extremum Seeking Using Bifurcation Analysis
  10. Off‐setting climate change through formation flying of aircraft, a feasibility study reliant on high fidelity gas‐phase chemical kinetic data
  11. Numerical Investigations of Subscale Flexible High Aspect Ratio Aircraft on a Dynamic Wind Tunnel Rig
  12. Modeling Flexible Multi-Body Systems Within the Udwadia–Kalaba Framework, a Lumped Parameter Approach
  13. The Emissions of Water Vapour and NOx from Modelled Hydrogen-Fuelled Aircraft and the Impact of NOx Reduction on Climate Compared with Kerosene-Fuelled Aircraft
  14. Assessing Performance of an Extremum Seeking Controller Using Continuation Methods
  15. Aircraft Emissions, Their Plume-Scale Effects, and the Spatio-Temporal Sensitivity of the Atmospheric Response: A Review
  16. Evaluating Longitudinal Unsteady Aerodynamic Effects in Stall for a T-Tail Transport Model
  17. Derivation of control inputs for deep stall recovery using nonlinear frequency analysis
  18. Analysing dynamic deep stall recovery using a nonlinear frequency approach
  19. Capturing nonlinear time-dependent aircraft dynamics using a wind tunnel manoeuvre rig
  20. Evaluation of Unsteady Aerodynamic Effects in Stall Region for a T-Tail Transport Model
  21. A Frequency-Domain Approach to Analysing Dynamic Deep Stall Recovery
  22. Design and Assessment of Subscale Flexible High Aspect Ratio Cantilever Wings
  23. Low-order Aeroelastic Modelling of a High Aspect Ratio Wing Aircraft Under Constrained Motion
  24. Folding Wingtips for Improved Roll Performance
  25. Abundance of NO3 Derived Organo-Nitrates and Their Importance in the Atmosphere
  26. Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach
  27. Identifying limits of linear control design validity in nonlinear systems: a continuation-based approach
  28. Effect of Actuator Saturation on Pilot-Induced Oscillation: A Nonlinear Bifurcation Analysis
  29. Eigenvector similarity metrics for the identification and quantitative study of aircraft dynamic modes
  30. Towards development of a nonlinear and flexible multi-body helicopter inceptor model: a resonant frequency tuning study.
  31. Folding Wingtips for Improved Roll Performance
  32. Flying qualities assessment using nonlinear frequency response analysis
  33. On the effect of model uncertainty on the Hopf bifurcation of aeroelastic systems
  34. An extension of the structured singular value to nonlinear systems with application to robust flutter analysis
  35. Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator
  36. Frequency-Domain Bifurcation Analysis of a Nonlinear Flight Dynamics Model
  37. Nonlinear Frequency Response Analysis to Inform Aircraft Control Law Design
  38. Industrially Inspired Gust Loads Analysis of Various-Aspect-Ratio Wings Featuring Geometric Nonlinearity
  39. Computation of Bifurcation Margins Based on Robust Control Concepts
  40. Nonlinear Blade Stability for a Scaled Autogyro Rotor at High Advance Ratios
  41. Enhanced Evolutionary-Based Optimization Techniques Applied to a Nonlinear Landing Gear Design Problem
  42. Sizing High-Aspect-Ratio Wings with a Geometrically Nonlinear Beam Model
  43. Efficient aeroelastic beam modelling and the selection of a structural shape basis
  44. Robust estimations of the Region of Attraction using invariant sets
  45. Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant
  46. Minimally Constrained Flight Simulation in Wind Tunnel
  47. Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig
  48. Flight control design for a highly flexible flutter demonstrator
  49. Identifying the Mode and Impact of Technological Substitutions
  50. Slender-Wing Beam Reduction Method for Gradient-Based Aeroelastic Design Optimization
  51. Algorithms for the estimation of the region of attraction with positively invariant sets
  52. On the geometrically exact low-order modelling of a flexible beam: formulation and numerical tests
  53. Numerical Continuation of Limit Cycle Oscillations and Bifurcations in High-Aspect-Ratio Wings
  54. Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools
  55. Flight Performance and Stability Analysis of Impaired Aircraft Using Constrained Bifurcation and Continuation Method
  56. Uncertainty and Sensitivity Analysis of Bifurcation Loci Characterizing Nonlinear Landing-Gear Dynamics
  57. Estimating the region of attraction of uncertain systems with invariant sets
  58. Limit Cycle Oscillation Amplitude Tailorng Based on Describing Functions and $$\mu $$ Analysis
  59. Nonlinear stability and post-critical analysis of an uncertain plant with describing functions and integral quadratic constraints
  60. Aeroelastic modeling and stability analysis: A robust approach to the flutter problem
  61. Worst Case Gust Prediction of Highly Flexible Wings
  62. Optimization of Aerospace Structures under Uncertainty using an Iterative Distribution Evolutionary Algorithm
  63. Modeling and robust Body Freedom Flutter Analysis of flexible aircraft configurations
  64. The impact of global aviation NOx emissions on tropospheric composition changes from 2005 to 2011
  65. Substructurability: the effect of interface location on a real-time dynamic substructuring test
  66. A mitigation strategy for commercial aviation impact on NOx‐related O3 change
  67. Investigation into the Interaction of Nose Landing Gear and Fuselage Dynamics
  68. A Commercial Aircraft Fuel Burn and Emissions Inventory for 2005–2011
  69. A cloned linguistic decision tree controller for real-time path planning in hostile environments
  70. Impact of Controller Delays on the Nonlinear Dynamics of Remotely Piloted Aircraft
  71. Wind Tunnel Manoeuvre Rig: A Multi-DOF Test Platform for Model Aircraft
  72. Aircraft Loads Prediction using Enhanced Simulation (ALPES)
  73. Bifurcation Analysis of a Nose Landing Gear System
  74. Aeroelastic Modelling of Highly Flexible Wings
  75. Dynamical Systems Methods for Evaluating Aircraft Ground Manoeuvres
  76. Comparison of Aeroelastic Modeling and Robust Flutter Analysis of a Typical Section**This work has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No 636307, project FLEXOP
  77. Nonlinear Dynamics of Aircraft Controller Characteristics Outside the Standard Flight Envelope
  78. Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models
  79. Numerical continuation and bifurcation analysis in aircraft design: an industrial perspective
  80. On the nonlinear dynamics of a rotor in autorotation: a combined experimental and numerical approach
  81. Wind Tunnel Wall Interference Effects on an Oscillating Aerofoil in the Stall Regime
  82. An aircraft performance model implementation for the estimation of global and regional commercial aviation fuel burn and emissions
  83. Evaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rig
  84. Efficient Prediction and Uncertainty Propagation of Correlated Loads
  85. EVALUATION AND UNCERTAINTY QUANTIFICATION OF BIFURCATION DIAGRAM: LANDING GEAR, A CASE STUDY
  86. A bifurcation study to guide the design of a landing gear with a combined uplock/downlock mechanism
  87. Bifurcation analysis using rigorous branch and bound methods
  88. Dynamic gain-scheduled control and extended linearisation: extensions, explicit formulae and stability
  89. Continuation and Bifurcation Analysis in Helicopter Aeroelastic Stability Problems
  90. Computational and Experimental Validation of the Active Morphing Wing
  91. Sensitivity of the Generic Transport Model upset dynamics to time delay
  92. Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism
  93. Bifurcation Analysis of a Coupled Nose-Landing-Gear–Fuselage System
  94. Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis
  95. Effects of Freeplay on Dynamic Stability of an Aircraft Main Landing Gear
  96. Investigation of Poststall Pitch Oscillations of an Aircraft Wind-Tunnel Model
  97. Spin Susceptibility of the NASA Generic Transport Model
  98. Bifurcation Analysis of the Generic Transport Model for Open-Loop and Closed-Loop Configurations
  99. Experimental Implementation of a Nonlinear Dynamic Inversion Controller with Antiwindup
  100. Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification
  101. Continuation Analysis of Aircraft Ground Loads During High-Speed Turns
  102. Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear
  103. Two-state dynamic gain scheduling control applied to an F16 aircraft model
  104. Numerical continuation analysis of a three-dimensional aircraft main landing gear mechanism
  105. Multi-parameter bifurcation study of shimmy oscillations in a dual-wheel aircraft nose landing gear
  106. Numerical Continuation Analysis of a Dual-sidestay Main Landing Gear Mechanism
  107. Bifurcation analysis of a flapping wing MAV in longitudinal flight
  108. Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems
  109. Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System
  110. Bifurcation Analysis of the NASA GTM with a View to Upset Recovery
  111. Effects of Freeplay on Aircraft Main Landing Gear Stability
  112. Analysis of Medium-Speed Runway Exit Maneuvers
  113. Synthesis of flatness control for a multi-axis robot manipulator: An experimental approach
  114. Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles
  115. Numerical Continuation Applied to Landing Gear Mechanism Analysis
  116. Analysis of Flexible Aircraft Dynamics Using Bifurcation Methods
  117. Canard cycles in aircraft ground dynamics
  118. Dynamic gain scheduled control in a multi-variable control framework
  119. Nonlinear Analysis of Lateral Loading During Taxiway Turns
  120. Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy
  121. Numerical Continuation Applied to Landing Gear Mechanism Analysis
  122. Analysis of Medium-Speed Runway Exit Maneuvers
  123. Application of Bifurcation Methods to the Prediction of Low-Speed Aircraft Ground Performance
  124. Dynamic gain scheduled control of a satellite with a robot manipulator
  125. Operational Parameter Study of Aircraft Dynamics on the Ground
  126. Bifurcation Analysis of Nose-Landing-Gear Shimmy with Lateral and Longitudinal Bending
  127. A Combined Numerical/Experimental Continuation Approach Applied to Nonlinear Rotor Dynamics
  128. Geometric Nonlinearities of Aircraft Systems
  129. Minisymposium Dynamical Systems Methods in Aerospace Engineering
  130. Operational Parameter Study of an Aircraft Turning on the Ground
  131. Nonlinear Analysis of Lateral Loading During Ground Manoeuvres
  132. Nonlinear Analysis of the Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy
  133. Application of Bifurcation Methods for the Prediction of Low-Speed Aircraft Ground Performance
  134. Application of Bifurcation and Continuation Methods to Nonlinear Flexible Aircraft Dynamics
  135. A Multi-Degree-of-Freedom Rig for the Wind Tunnel Determination of Dynamic Data
  136. Bifurcation and Stability Analysis of Aircraft Turning on the Ground
  137. Methods for Conceptual Flight Control System Design
  138. Operational Parameter Study of Aircraft Ground Dynamics
  139. Experimental Evaluation of Numerical Continuation and Bifurcation Methods Applied to Autogyro Rotor Blade Aeromechanical Stability
  140. Interaction of torsion and lateral bending in aircraft nose landing gear shimmy
  141. Dynamic Gain Scheduled Control of an F16 Model
  142. Dynamic Wind Tunnel Rig Implementation of Nonlinear Dynamic Inversion-Based Anti-Windup Scheme
  143. Modelling Continuously Morphing Aircraft for Flight Control
  144. Nonlinear Ground Dynamics of Aircraft: Bifurcation Analysis of Turning Solutions
  145. Modeling of Nose Landing Gear Shimmy with Lateral and Longitudinal Bending and a Non-Zero Rake Angle
  146. Nonlinear Dynamic Inversion Based Anti-windup - An Aerospace Application
  147. An Analysable Nonlinear Criterion for Clearance of Flight Control Laws
  148. Modelling the Dynamic Response of a Morphing Wing with Active Winglets
  149. Evaluation of a Three Degree of Freedom Test Rig for Stability Derivative Estimation
  150. Tailored Dynamic Gain-Scheduled Control
  151. Flight Dynamics Analysis of Periodically Forced Rotorcraft Model
  152. Integration of Control Allocation Methods in Bifurcation Analysis Framework
  153. Design of a Gain-Scheduled Flight Control System Using Bifurcation Analysis
  154. Fuzzy Decision Tree Cloning of Flight Trajectory Optimisation for Rapid Path Planning
  155. Stability and Control Assessment of a Blended-Wing-Body Airliner Configuration
  156. Tailored dynamic gain-scheduled control of a nonlinear UCAV model
  157. Wind-Tunnel Testing of a Dynamic State-Feedback Gain Scheduled Control System
  158. Non-Linear Vehicle Dynamics Using Bifurcation Methods
  159. Comparative Evaluation of Unsteady Aerodynamic Modelling Approaches
  160. Bifurcation Analysis of Rotorcraft Dynamics with an Underslung Load
  161. Dynamic State-Feedback Gain Scheduled Control of the ICE 101-TV
  162. Continuation Methods for Aircraft Models Subject to Integrator Wind-Up
  163. Modelling Non-linear Behaviour in a Single Degree-of-Freedom Dynamic Wind Tunnel Rig
  164. Control of Nonlinear Aircraft Models Using Dynamic State-Feedback Gain Scheduling
  165. Aircraft Control Law Clearance Analysis Using Bifurcation and Continuation Methods
  166. Experimental Analysis and Modeling of Limit Cycles in a Dynamic Wind-Tunnel Rig
  167. BIFURCATION TAILORING VIA NEWTON FLOW-AIDED ADAPTIVE CONTROL
  168. Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus
  169. Aircraft Flight Dynamics Analysis and Controller Design Using Bifurcation Tailoring
  170. The continuation design framework for nonlinear aircraft control
  171. MEASURING AND IMPROVING NEURAL NETWORK GENERALIZATION FOR MODEL UPDATING
  172. Nonlinear sensitivity studies for flight mechanics design
  173. Derivation of non-linear control strategies via numerical continuation
  174. Bifurcation analysis of multiple–attractor flight dynamics
  175. Development of control schedules to modify spin behaviour
  176. Bifurcation analysis as a tool for post-departure stability enhancement
  177. Stability and controllability evaluation of sustained flight manoeuvres
  178. Model selection for high incidence flight mechanics analysis
  179. Bifurcation-Based Clearance of Linear Stability Criteria
  180. Bifurcation and Continuation Method
  181. Continuation based control of aircraft dynamics