All Stories

  1. Experimental Testing and Analysis of a Very Flexible Wing Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Fintan Healy, Professor Mark Lowenberg

  2. NATO AVT-350 Task Group: Comparison of Experimental and CFD Results of Forebody Blowing on the Bristol-ICE Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  3. Computational and Experimental Study of Deep Stall in a Generic T-Tail Transport Aircraft

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Duc Nguyen, Professor Mark Lowenberg

  4. Flight dynamics of aircraft incorporating the semi-aeroelastic hinge

    Article • Aerospace Science and Technology, April 2024, Elsevier

    Professor Mark Lowenberg

  5. Design and Experimental Investigation of a Benchmark Aeroelastic Wing Model

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Benjamin KS Woods, Professor Mark Lowenberg

  6. Experimental and numerical analysis of the bifurcation behaviour of a very flexible wing

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  7. Airliner upset — improving our understanding through sub-scale flight testing

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, Daniel Pusztai

  8. Development of a Pressurised Wind Tunnel Mount for Testing Novel Flow Controls for AVT-350-RTG

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  9. Wind Tunnel Investigations of a Pitch-Free Flexible High Aspect Ratio Aircraft Model

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  10. Aeroelastic scaling of a high aspect ratio wing incorporating semi aeroelastic hinge

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  11. Isola in a linear one‐degree‐of‐freedom feedback system with actuator rate saturation

    Article • International Journal of Mechanical System Dynamics, August 2023, Wiley

    Professor Mark Lowenberg

  12. A Graphical Approach to Examining Classical Extremum Seeking Using Bifurcation Analysis

    Article • IEEE Transactions on Control Systems Technology, May 2023, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  13. Off‐setting climate change through formation flying of aircraft, a feasibility study reliant on high fidelity gas‐phase chemical kinetic data

    Article • International Journal of Chemical Kinetics, April 2023, Wiley

    Professor Mark Lowenberg

  14. Numerical Investigations of Subscale Flexible High Aspect Ratio Aircraft on a Dynamic Wind Tunnel Rig

    Article • January 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  15. Modeling Flexible Multi-Body Systems Within the Udwadia–Kalaba Framework, a Lumped Parameter Approach

    Article • Journal of Computational and Nonlinear Dynamics, October 2022, ASME International

    Professor Mark Lowenberg

  16. 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

    Article • Atmosphere, October 2022, MDPI AG

    Professor Mark Lowenberg

  17. Assessing Performance of an Extremum Seeking Controller Using Continuation Methods

    Article • August 2022, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  18. Aircraft Emissions, Their Plume-Scale Effects, and the Spatio-Temporal Sensitivity of the Atmospheric Response: A Review

    Article • Aerospace, July 2022, MDPI AG

    Professor Mark Lowenberg

  19. Evaluating Longitudinal Unsteady Aerodynamic Effects in Stall for a T-Tail Transport Model

    Article • Journal of Aircraft, July 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  20. Derivation of control inputs for deep stall recovery using nonlinear frequency analysis

    Article • The Aeronautical Journal, May 2022, Cambridge University Press

    Professor Mark Lowenberg

  21. Analysing dynamic deep stall recovery using a nonlinear frequency approach

    Article • Nonlinear Dynamics, February 2022, Springer Science + Business Media

    Professor Mark Lowenberg

  22. Capturing nonlinear time-dependent aircraft dynamics using a wind tunnel manoeuvre rig

    Article • Aerospace Science and Technology, February 2022, Elsevier

    Professor Mark Lowenberg

  23. Evaluation of Unsteady Aerodynamic Effects in Stall Region for a T-Tail Transport Model

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  24. A Frequency-Domain Approach to Analysing Dynamic Deep Stall Recovery

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  25. Design and Assessment of Subscale Flexible High Aspect Ratio Cantilever Wings

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  26. Low-order Aeroelastic Modelling of a High Aspect Ratio Wing Aircraft Under Constrained Motion

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  27. Folding Wingtips for Improved Roll Performance

    Article • Journal of Aircraft, January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  28. Abundance of NO3 Derived Organo-Nitrates and Their Importance in the Atmosphere

    Article • Atmosphere, October 2021, MDPI AG

    Professor Mark Lowenberg

  29. Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach

    Article • Journal of Guidance Control and Dynamics, September 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  30. Identifying limits of linear control design validity in nonlinear systems: a continuation-based approach

    Article • Nonlinear Dynamics, March 2021, Springer Science + Business Media

    Professor Mark Lowenberg

  31. Effect of Actuator Saturation on Pilot-Induced Oscillation: A Nonlinear Bifurcation Analysis

    Article • Journal of Guidance Control and Dynamics, March 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Duc Nguyen, Professor Mark Lowenberg

  32. Eigenvector similarity metrics for the identification and quantitative study of aircraft dynamic modes

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  33. Towards development of a nonlinear and flexible multi-body helicopter inceptor model: a resonant frequency tuning study.

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, Edward Yap

  34. Folding Wingtips for Improved Roll Performance

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, Fintan Healy, Theodor Neofet

  35. Flying qualities assessment using nonlinear frequency response analysis

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Duc Nguyen, Professor Mark Lowenberg

  36. On the effect of model uncertainty on the Hopf bifurcation of aeroelastic systems

    Article • Nonlinear Dynamics, January 2021, Springer Science + Business Media

    Professor Mark Lowenberg

  37. An extension of the structured singular value to nonlinear systems with application to robust flutter analysis

    Article • CEAS Aeronautical Journal, September 2020, Springer Science + Business Media

    Professor Mark Lowenberg

  38. Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator

    Article • Experimental Techniques, September 2020, Springer Science + Business Media

    Professor Mark Lowenberg

  39. Frequency-Domain Bifurcation Analysis of a Nonlinear Flight Dynamics Model

    Article • Journal of Guidance Control and Dynamics, September 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Duc Nguyen, Professor Mark Lowenberg

  40. Nonlinear Frequency Response Analysis to Inform Aircraft Control Law Design

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  41. Industrially Inspired Gust Loads Analysis of Various-Aspect-Ratio Wings Featuring Geometric Nonlinearity

    Article • Journal of Aircraft, January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  42. Computation of Bifurcation Margins Based on Robust Control Concepts

    Article • SIAM Journal on Applied Dynamical Systems, January 2020, Society for Industrial & Applied Mathematics (SIAM)

    Professor Mark Lowenberg

  43. Nonlinear Blade Stability for a Scaled Autogyro Rotor at High Advance Ratios

    Article • Journal of the American Helicopter Society, January 2020, American Helicopter Society

    Professor Mark Lowenberg

  44. Enhanced Evolutionary-Based Optimization Techniques Applied to a Nonlinear Landing Gear Design Problem

    Article • Journal of Aircraft, September 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  45. Sizing High-Aspect-Ratio Wings with a Geometrically Nonlinear Beam Model

    Article • Journal of Aircraft, July 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  46. Efficient aeroelastic beam modelling and the selection of a structural shape basis

    Article • International Journal of Non-Linear Mechanics, June 2019, Elsevier

    Professor Mark Lowenberg

  47. Robust estimations of the Region of Attraction using invariant sets

    Article • Journal of the Franklin Institute, May 2019, Elsevier

    Professor Mark Lowenberg

  48. Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant

    Article • IEEE Transactions on Control Systems Technology, March 2019, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  49. Minimally Constrained Flight Simulation in Wind Tunnel

    Article • Journal of Aircraft, January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  50. Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig

    Article • Journal of Aircraft, January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, SERGIO ANGEL SA ARAUJO-ESTRADA, Dr Mikhail G Goman

  51. Flight control design for a highly flexible flutter demonstrator

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Daniel Ossmann, Dr Balint Vanek, Professor Mark Lowenberg

  52. Identifying the Mode and Impact of Technological Substitutions

    Article • IEEE Access, January 2019, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  53. Slender-Wing Beam Reduction Method for Gradient-Based Aeroelastic Design Optimization

    Article • AIAA Journal, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, Miss Olivia Stodieck

  54. Algorithms for the estimation of the region of attraction with positively invariant sets

    Article • October 2018, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  55. On the geometrically exact low-order modelling of a flexible beam: formulation and numerical tests

    Article • Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences, August 2018, Royal Society Publishing

    Professor Mark Lowenberg

  56. Numerical Continuation of Limit Cycle Oscillations and Bifurcations in High-Aspect-Ratio Wings

    Article • Aerospace, July 2018, MDPI AG

    Professor Mark Lowenberg

  57. Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools

    Article • Journal of Guidance Control and Dynamics, May 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  58. Flight Performance and Stability Analysis of Impaired Aircraft Using Constrained Bifurcation and Continuation Method

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  59. Uncertainty and Sensitivity Analysis of Bifurcation Loci Characterizing Nonlinear Landing-Gear Dynamics

    Article • Journal of Aircraft, January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  60. Estimating the region of attraction of uncertain systems with invariant sets

    Article • IFAC-PapersOnLine, January 2018, Elsevier

    Professor Mark Lowenberg

  61. Limit Cycle Oscillation Amplitude Tailorng Based on Describing Functions and $$\mu $$ Analysis

    Article • December 2017, Springer Science + Business Media

    Professor Mark Lowenberg

  62. Nonlinear stability and post-critical analysis of an uncertain plant with describing functions and integral quadratic constraints

    Article • December 2017, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  63. Aeroelastic modeling and stability analysis: A robust approach to the flutter problem

    Article • International Journal of Robust and Nonlinear Control, August 2017, Wiley

    Professor Mark Lowenberg

  64. Worst Case Gust Prediction of Highly Flexible Wings

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  65. Optimization of Aerospace Structures under Uncertainty using an Iterative Distribution Evolutionary Algorithm

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  66. Modeling and robust Body Freedom Flutter Analysis of flexible aircraft configurations

    Article • September 2016, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  67. The impact of global aviation NOx emissions on tropospheric composition changes from 2005 to 2011

    Article • Atmospheric Research, September 2016, Elsevier

    Professor Mark Lowenberg

  68. Substructurability: the effect of interface location on a real-time dynamic substructuring test

    Article • Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences, August 2016, Royal Society Publishing

    Professor Mark Lowenberg

  69. A mitigation strategy for commercial aviation impact on NOx‐related O3 change

    Article • Journal of Geophysical Research Atmospheres, July 2016, American Geophysical Union (AGU)

    Professor Mark Lowenberg

  70. Investigation into the Interaction of Nose Landing Gear and Fuselage Dynamics

    Article • Journal of Aircraft, July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  71. A Commercial Aircraft Fuel Burn and Emissions Inventory for 2005–2011

    Article • Atmosphere, June 2016, MDPI AG

    Professor Mark Lowenberg

  72. A cloned linguistic decision tree controller for real-time path planning in hostile environments

    Article • Fuzzy Sets and Systems, June 2016, Elsevier

    Professor Mark Lowenberg

  73. Impact of Controller Delays on the Nonlinear Dynamics of Remotely Piloted Aircraft

    Article • Journal of Guidance Control and Dynamics, February 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  74. Wind Tunnel Manoeuvre Rig: A Multi-DOF Test Platform for Model Aircraft

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    SERGIO ANGEL SA ARAUJO-ESTRADA, Dr Mikhail G Goman, Professor Mark Lowenberg

  75. Aircraft Loads Prediction using Enhanced Simulation (ALPES)

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  76. Bifurcation Analysis of a Nose Landing Gear System

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  77. Aeroelastic Modelling of Highly Flexible Wings

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  78. Dynamical Systems Methods for Evaluating Aircraft Ground Manoeuvres

    Article • January 2016, Springer Science + Business Media

    Professor Mark Lowenberg

  79. 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

    Article • IFAC-PapersOnLine, January 2016, Elsevier

    Professor Mark Lowenberg

  80. Nonlinear Dynamics of Aircraft Controller Characteristics Outside the Standard Flight Envelope

    Article • Journal of Guidance Control and Dynamics, December 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  81. Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models

    Article • CEAS Aeronautical Journal, October 2015, Springer Science + Business Media

    Professor Mark Lowenberg

  82. Numerical continuation and bifurcation analysis in aircraft design: an industrial perspective

    Article • Philosophical Transactions of the Royal Society A Mathematical Physical and Engineering Sciences, September 2015, Royal Society Publishing

    Professor Mark Lowenberg

  83. On the nonlinear dynamics of a rotor in autorotation: a combined experimental and numerical approach

    Article • Philosophical Transactions of the Royal Society A Mathematical Physical and Engineering Sciences, August 2015, Royal Society Publishing

    Professor Mark Lowenberg

  84. Wind Tunnel Wall Interference Effects on an Oscillating Aerofoil in the Stall Regime

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  85. An aircraft performance model implementation for the estimation of global and regional commercial aviation fuel burn and emissions

    Article • Transportation Research Part D Transport and Environment, March 2015, Elsevier

    Professor Mark Lowenberg

  86. Evaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rig

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    SERGIO ANGEL SA ARAUJO-ESTRADA, Dr Mikhail G Goman, Professor Mark Lowenberg

  87. Efficient Prediction and Uncertainty Propagation of Correlated Loads

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  88. EVALUATION AND UNCERTAINTY QUANTIFICATION OF BIFURCATION DIAGRAM: LANDING GEAR, A CASE STUDY

    Article • January 2015, ECCOMAS

    Professor Mark Lowenberg

  89. A bifurcation study to guide the design of a landing gear with a combined uplock/downlock mechanism

    Article • Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences, October 2014, Royal Society Publishing

    Professor Mark Lowenberg

  90. Bifurcation analysis using rigorous branch and bound methods

    Article • October 2014, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  91. Dynamic gain-scheduled control and extended linearisation: extensions, explicit formulae and stability

    Article • International Journal of Control, September 2014, Taylor & Francis

    Professor Mark Lowenberg

  92. Continuation and Bifurcation Analysis in Helicopter Aeroelastic Stability Problems

    Article • Journal of Guidance Control and Dynamics, May 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  93. Computational and Experimental Validation of the Active Morphing Wing

    Article • Journal of Aircraft, May 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  94. Sensitivity of the Generic Transport Model upset dynamics to time delay

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  95. Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism

    Article • Journal of Aircraft, January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg, Jonathan Knowles

  96. Bifurcation Analysis of a Coupled Nose-Landing-Gear–Fuselage System

    Article • Journal of Aircraft, January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  97. Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis

    Article • Journal of Aircraft, November 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  98. Effects of Freeplay on Dynamic Stability of an Aircraft Main Landing Gear

    Article • Journal of Aircraft, November 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  99. Investigation of Poststall Pitch Oscillations of an Aircraft Wind-Tunnel Model

    Article • Journal of Aircraft, November 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  100. Spin Susceptibility of the NASA Generic Transport Model

    Article • August 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  101. Bifurcation Analysis of the Generic Transport Model for Open-Loop and Closed-Loop Configurations

    Article • August 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  102. Experimental Implementation of a Nonlinear Dynamic Inversion Controller with Antiwindup

    Article • Journal of Guidance Control and Dynamics, July 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  103. Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification

    Article • Journal of Aircraft, March 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  104. Continuation Analysis of Aircraft Ground Loads During High-Speed Turns

    Article • Journal of Aircraft, January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  105. Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear

    Article • SIAM Journal on Applied Dynamical Systems, January 2013, Society for Industrial & Applied Mathematics (SIAM)

    Professor Mark Lowenberg

  106. Two-state dynamic gain scheduling control applied to an F16 aircraft model

    Article • International Journal of Non-Linear Mechanics, December 2012, Elsevier

    Professor Mark Lowenberg

  107. Numerical continuation analysis of a three-dimensional aircraft main landing gear mechanism

    Article • Nonlinear Dynamics, November 2012, Springer Science + Business Media

    Professor Mark Lowenberg

  108. Multi-parameter bifurcation study of shimmy oscillations in a dual-wheel aircraft nose landing gear

    Article • Nonlinear Dynamics, August 2012, Springer Science + Business Media

    Professor Mark Lowenberg

  109. Numerical Continuation Analysis of a Dual-sidestay Main Landing Gear Mechanism

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  110. Bifurcation analysis of a flapping wing MAV in longitudinal flight

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  111. Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  112. Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  113. Bifurcation Analysis of the NASA GTM with a View to Upset Recovery

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  114. Effects of Freeplay on Aircraft Main Landing Gear Stability

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  115. Analysis of Medium-Speed Runway Exit Maneuvers

    Article • Journal of Aircraft, September 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  116. Synthesis of flatness control for a multi-axis robot manipulator: An experimental approach

    Article • September 2011, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  117. Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles

    Article • August 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  118. Numerical Continuation Applied to Landing Gear Mechanism Analysis

    Article • Journal of Aircraft, July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  119. Analysis of Flexible Aircraft Dynamics Using Bifurcation Methods

    Article • Journal of Guidance Control and Dynamics, May 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  120. Canard cycles in aircraft ground dynamics

    Article • Nonlinear Dynamics, January 2011, Springer Science + Business Media

    Professor Mark Lowenberg

  121. Dynamic gain scheduled control in a multi-variable control framework

    Article • December 2010, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  122. Nonlinear Analysis of Lateral Loading During Taxiway Turns

    Article • Journal of Guidance Control and Dynamics, November 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  123. Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy

    Article • Journal of Aircraft, September 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  124. Numerical Continuation Applied to Landing Gear Mechanism Analysis

    Article • August 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  125. Analysis of Medium-Speed Runway Exit Maneuvers

    Article • August 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  126. Application of Bifurcation Methods to the Prediction of Low-Speed Aircraft Ground Performance

    Article • Journal of Aircraft, July 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  127. Dynamic gain scheduled control of a satellite with a robot manipulator

    Article • June 2010, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  128. Operational Parameter Study of Aircraft Dynamics on the Ground

    Article • Journal of Computational and Nonlinear Dynamics, February 2010, ASME International

    Professor Mark Lowenberg

  129. Bifurcation Analysis of Nose-Landing-Gear Shimmy with Lateral and Longitudinal Bending

    Article • Journal of Aircraft, January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  130. A Combined Numerical/Experimental Continuation Approach Applied to Nonlinear Rotor Dynamics

    Article • January 2010, Springer Science + Business Media

    Professor Mark Lowenberg

  131. Geometric Nonlinearities of Aircraft Systems

    Article • January 2010, Springer Science + Business Media

    Professor Mark Lowenberg

  132. Minisymposium Dynamical Systems Methods in Aerospace Engineering

    Article • January 2010, Springer Science + Business Media

    Professor Mark Lowenberg

  133. Operational Parameter Study of an Aircraft Turning on the Ground

    Article • January 2010, Springer Science + Business Media

    Professor Mark Lowenberg

  134. Nonlinear Analysis of Lateral Loading During Ground Manoeuvres

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  135. Nonlinear Analysis of the Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  136. Application of Bifurcation Methods for the Prediction of Low-Speed Aircraft Ground Performance

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  137. Application of Bifurcation and Continuation Methods to Nonlinear Flexible Aircraft Dynamics

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  138. A Multi-Degree-of-Freedom Rig for the Wind Tunnel Determination of Dynamic Data

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  139. Bifurcation and Stability Analysis of Aircraft Turning on the Ground

    Article • Journal of Guidance Control and Dynamics, March 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  140. Methods for Conceptual Flight Control System Design

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  141. Operational Parameter Study of Aircraft Ground Dynamics

    Article • January 2009, ASME International

    Professor Mark Lowenberg

  142. Experimental Evaluation of Numerical Continuation and Bifurcation Methods Applied to Autogyro Rotor Blade Aeromechanical Stability

    Article • January 2009, ASME International

    Professor Mark Lowenberg

  143. Interaction of torsion and lateral bending in aircraft nose landing gear shimmy

    Article • Nonlinear Dynamics, December 2008, Springer Science + Business Media

    Professor Mark Lowenberg

  144. Dynamic Gain Scheduled Control of an F16 Model

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  145. Dynamic Wind Tunnel Rig Implementation of Nonlinear Dynamic Inversion-Based Anti-Windup Scheme

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  146. Modelling Continuously Morphing Aircraft for Flight Control

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  147. Nonlinear Ground Dynamics of Aircraft: Bifurcation Analysis of Turning Solutions

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  148. Modeling of Nose Landing Gear Shimmy with Lateral and Longitudinal Bending and a Non-Zero Rake Angle

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  149. Nonlinear Dynamic Inversion Based Anti-windup - An Aerospace Application

    Article • IFAC Proceedings Volumes, January 2008, Elsevier

    Professor Mark Lowenberg

  150. An Analysable Nonlinear Criterion for Clearance of Flight Control Laws

    Article • August 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  151. Modelling the Dynamic Response of a Morphing Wing with Active Winglets

    Article • August 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  152. Evaluation of a Three Degree of Freedom Test Rig for Stability Derivative Estimation

    Article • Journal of Aircraft, November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  153. Tailored Dynamic Gain-Scheduled Control

    Article • Journal of Guidance Control and Dynamics, November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  154. Flight Dynamics Analysis of Periodically Forced Rotorcraft Model

    Article • August 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  155. Integration of Control Allocation Methods in Bifurcation Analysis Framework

    Article • August 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  156. Design of a Gain-Scheduled Flight Control System Using Bifurcation Analysis

    Article • Journal of Guidance Control and Dynamics, March 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  157. Fuzzy Decision Tree Cloning of Flight Trajectory Optimisation for Rapid Path Planning

    Article • January 2006, Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg

  158. Stability and Control Assessment of a Blended-Wing-Body Airliner Configuration

    Article • August 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  159. Tailored dynamic gain-scheduled control of a nonlinear UCAV model

    Article • August 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  160. Wind-Tunnel Testing of a Dynamic State-Feedback Gain Scheduled Control System

    Article • August 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  161. Non-Linear Vehicle Dynamics Using Bifurcation Methods

    Article • November 2004, SAE International

    Professor Mark Lowenberg

  162. Comparative Evaluation of Unsteady Aerodynamic Modelling Approaches

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  163. Bifurcation Analysis of Rotorcraft Dynamics with an Underslung Load

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  164. Dynamic State-Feedback Gain Scheduled Control of the ICE 101-TV

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  165. Continuation Methods for Aircraft Models Subject to Integrator Wind-Up

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  166. Modelling Non-linear Behaviour in a Single Degree-of-Freedom Dynamic Wind Tunnel Rig

    Article • August 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  167. Control of Nonlinear Aircraft Models Using Dynamic State-Feedback Gain Scheduling

    Article • August 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  168. Aircraft Control Law Clearance Analysis Using Bifurcation and Continuation Methods

    Article • August 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  169. Experimental Analysis and Modeling of Limit Cycles in a Dynamic Wind-Tunnel Rig

    Article • Journal of Aircraft, July 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  170. BIFURCATION TAILORING VIA NEWTON FLOW-AIDED ADAPTIVE CONTROL

    Article • International Journal of Bifurcation and Chaos, March 2003, World Scientific Pub Co Pte Lt

    Professor Mark Lowenberg

  171. Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus

    Article • August 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  172. Aircraft Flight Dynamics Analysis and Controller Design Using Bifurcation Tailoring

    Article • August 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  173. The continuation design framework for nonlinear aircraft control

    Article • August 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  174. MEASURING AND IMPROVING NEURAL NETWORK GENERALIZATION FOR MODEL UPDATING

    Article • Journal of Sound and Vibration, November 2000, Elsevier

    Professor Mark Lowenberg

  175. Nonlinear sensitivity studies for flight mechanics design

    Article • August 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  176. Derivation of non-linear control strategies via numerical continuation

    Article • August 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  177. Bifurcation analysis of multiple–attractor flight dynamics

    Article • Philosophical Transactions of the Royal Society A Mathematical Physical and Engineering Sciences, October 1998, Royal Society Publishing

    Professor Mark Lowenberg

  178. Development of control schedules to modify spin behaviour

    Article • August 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  179. Bifurcation analysis as a tool for post-departure stability enhancement

    Article • August 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  180. Stability and controllability evaluation of sustained flight manoeuvres

    Article • July 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  181. Model selection for high incidence flight mechanics analysis

    Article • August 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Mark Lowenberg

  182. Bifurcation-Based Clearance of Linear Stability Criteria

    Article • Springer Science + Business Media

    Professor Mark Lowenberg

  183. Bifurcation and Continuation Method

    Article • Springer Science + Business Media

    Professor Mark Lowenberg

  184. Continuation based control of aircraft dynamics

    Article • Institute of Electrical & Electronics Engineers (IEEE)

    Professor Mark Lowenberg