All Stories

  1. Rapid preliminary aircraft wing sizing for metallic and composite structures to support data-driven multidisciplinary design optimisation frameworks
  2. Nonlinear Model Predictive Control for Hybrid Flapping-Rotor Micro Aerial Vehicles
  3. Neural Network Observer Based LPV Fault Tolerant Control of a Flying-Wing Aircraft
  4. A review of active inceptor systems technology
  5. LPV-Based Adaptive Robust-Augmented Control for a Blended-Wing-Body Aircraft Under Icing, Faults, Disturbances, and Uncertainties
  6. Identification of Nonlinearity Sources in a Flexible Wing
  7. Enhancing Aircraft Design: Assessing Adverse Yaw and Vertical Tail Plane Reduction Using Prandtl Wing Principles in Sailplanes
  8. Early-Stage Assessment of a Flexible Aircraft Simulation Framework in a Pilot-in-the-Loop Environment
  9. Control allocation problem transformation approaches for over-actuated vectored thrust VTOLs
  10. Multidisciplinary Design Optimization of the NASA Metallic and Composite Common Research Model Wingbox: Addressing Static Strength, Stiffness, Aeroelastic, and Manufacturing Constraints
  11. Damping Identification Sensitivity in Flutter Speed Estimation
  12. Enhancing Quadrotor Resilience in Outdoor Operations with Real-time Wind Gust Measurement by using LiDAR
  13. Integration of renewable energy sources in tandem with electrolysis: A technology review for green hydrogen production
  14. Autonomous Parafoil Flaring Control System for eVTOL Aircraft
  15. An Aircraft-Manipulator System for Virtual Flight Testing of Longitudinal Flight Dynamics
  16. A Robust Adaptive PID-like Controller for Quadrotor Unmanned Aerial Vehicle Systems
  17. Full Envelope Control of Over-Actuated Fixed-Wing Vectored Thrust eVTOL
  18. Simulation framework and development of the Future Systems Simulator
  19. Disturbance Observer-Based Backstepping Terminal Sliding Mode Aeroelastic Control of Airfoils
  20. Cascaded Incremental Nonlinear Dynamic Inversion Trajectory Following for a Stratospheric Airship in Wind
  21. Disturbance Observer Based Backstepping Terminal Sliding Mode Aeroelastic Control of Airfoils
  22. Quaternion-Based Attitude Estimation of an Aircraft Model Using Computer Vision
  23. Design and Implementation of an L1 Adaptive Proportional Output Feedback Controller
  24. Aerodynamic performance of a flyable flapping wing rotor with dragonfly-like flexible wings
  25. Self-supervised learning-based two-phase flow regime identification using ultrasonic sensors in an S-shape riser
  26. Motion Estimation of an Aircraft Model Using Computer Vision
  27. Aerodynamic Analysis of Saab 340B Aircraft with Data Fusion Implementation
  28. SAAB 340B Aerodynamic Model Development Using Binary Particle Swarm Optimization
  29. A global–local meta-modelling technique for model updating
  30. Active Stall Flutter Suppression for a Revised Leishman–Beddoes Model
  31. ℒ1 Adaptive Control of Quadrotor UAVs in Case of Inversion of the Torque Direction
  32. Development of Aerodynamic and Propulsion Models Using the Iterative Equation Error Method
  33. Flight data validation of an icing accretion estimation scheme using super-twisting observers
  34. Observer based incremental backstepping terminal sliding-mode control with learning rate for a multi-vectored propeller airship
  35. The Accuracy and Computational Efficiency of the Loewner Framework for the System Identification of Mechanical Systems
  36. Analysis of Visualization Systems in Flight Simulators
  37. Fault-tolerant switched reluctance motor propulsion system for eVTOLs
  38. ℒ1 Adaptive Path-Following of Airships in Wind
  39. A Loewner-Based System Identification and Structural Health Monitoring Approach for Mechanical Systems
  40. Wind Preview-Based Model Predictive Control of Multi-Rotor UAVs Using LiDAR
  41. Development of High-Fidelity Saab 340B Aerodynamic Model
  42. Modelling, Simulation, and Verification of the Saab 340B
  43. Scheduled Flight Control System of Tilt-Rotor VTOL PAV
  44. The prospects of hydrogen in achieving net zero emissions by 2050: A critical review
  45. Control of Plane Poiseuille Flow Using the Kreiss Constant
  46. Development of Gas–Liquid Flow Regimes Identification Using a Noninvasive Ultrasonic Sensor, Belt-Shape Features, and Convolutional Neural Network in an S-Shaped Riser
  47. Autonomous Landing of an UAV Using H∞ Based Model Predictive Control
  48. Slug flow regime in a flowline with U-shape riser
  49. Effect of Rotor Tilt on the Gust Rejection Properties of Multirotor Aircraft
  50. Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study
  51. Experimental verification of an LiDAR based Gust Rejection System for a Quadrotor UAV
  52. A Kriging Approach to Model Updating for Damage Detection
  53. Control of an eVTOL using Nonlinear Dynamic Inversion
  54. Adaptive Backstepping Nonsingular Terminal Sliding-Mode Attitude Control of Flexible Airships with Actuator Faults
  55. Gas-liquid flow regimes identification using non-intrusive Doppler ultrasonic sensor and convolutional recurrent neural networks in an s-shaped riser
  56. Classification of flow regimes using a neural network and a non-invasive ultrasonic sensor in an S-shaped pipeline-riser system
  57. Slug Flow Control in an S-shape Pipeline-Riser System using an Ultrasonic Sensor
  58. Slug flow control using topside measurements: A review
  59. Observer-based incremental backstepping sliding-mode fault-tolerant control for blended-wing-body aircrafts
  60. Disturbance Observer Enhanced Neural Network LPV Control for a Blended-Wing-Body Large Aircraft
  61. Backstepping sliding-mode control of stratospheric airships using disturbance-observer
  62. Non-intrusive classification of gas-liquid flow regimes in an S-shaped pipeline riser using a Doppler ultrasonic sensor and deep neural networks
  63. An Advanced Unmanned Aerial Vehicle (UAV) Approach via Learning-Based Control for Overhead Power Line Monitoring: A Comprehensive Review
  64. Neural network adaptive backstepping fault tolerant control for unmanned airships with multi-vectored thrusters
  65. Application of Norm Optimal Iterative Learning Control to Quadrotor Unmanned Aerial Vehicle for Monitoring Overhead Power System
  66. Integrated moment-based LGMD and deep reinforcement learning for UAV obstacle avoidance
  67. Visual Flight Rules-Based Collision Avoidance Systems for UAV Flying in Civil Aerospace
  68. Adaptive sliding-mode-backstepping trajectory tracking control of underactuated airships
  69. Multirotor Sizing Methodology with Flight Time Estimation
  70. Quadrotor System Design for a 3 DOF platform based on Iterative Learning Control
  71. Severe slug mitigation in an S-shape pipeline-riser system by an injectable venturi
  72. Venturi Multiphase Flow Measurement based Active Slug Control
  73. A benchtop flight control demonstrator
  74. Degraded Planary Tracking Control of an Omnidirectional Vectored-Thruster Aerostat
  75. Modelling and control of the roll-stabilised control unit of a rotary steerable system directional drilling tool
  76. High Aspect Ratio Wing Design Using the Minimum Exergy Destruction Principle
  77. Bilinear modelling, control and stability of directional drilling
  78. Quasi-bilinear modelling and control of directional drilling
  79. Application of LQG and H∞ Gain Scheduling Techniques to Active Suppression of Flutter
  80. Extremum Seeking Control for Truck Drag Reduction
  81. Multi-Objective Optimal Longitudinal Flight Control System Design for Large Flexible Transport Aircraft
  82. Multiobjective Environmental Departure Procedure Optimization
  83. Application of an Efficient Gradient-Based Optimization Strategy for Aircraft Wing Structures
  84. A Furcated Visual Collision Avoidance System for an Autonomous Micro Robot
  85. Applying a Modified Smith Predictor-Bilinear Proportional Plus Integral Control for Directional Drilling ⁎ ⁎This work was supported by Schlumberger
  86. Bilinear Modelling and Attitude Control of a Quadrotor
  87. Gust Rejection Properties of VTOL Multirotor Aircraft
  88. Adopting exergy analysis for use in aerospace
  89. Directional Drilling Attitude Control With Input Disturbances and Feedback Delay * *This work was supported by Schlumberger
  90. Application of Lyapunov matrix inequality based unsymmetrical saturated control to a multi-vectored propeller airship
  91. Evaluating the Rationale for Folding Wing Tips Comparing the Exergy and Breguet Approaches
  92. Decision-making for unmanned aerial vehicle operation in icing conditions
  93. Bilinear modelling and bilinear PI control of directional drilling
  94. Robust sliding mode control of a quadrotor
  95. Solving optimal control problems using chebfun
  96. Fault tolerant control of a quadrotor using ℒ1adaptive control
  97. Entropy Generation Minimisation and Exergy analysis approaches for aerospace applications - A review
  98. Mixed Uncertainty Analysis of Pole Placement and H∞Controllers for Directional Drilling Attitude Tracking
  99. Collaborative Control in a Flying-Boom Aerial Refueling Simulation
  100. State space modelling of a Class E2 converter for inductive links
  101. High-Input-Voltage High-Frequency Class E Rectifiers for Resonant Inductive Links
  102. Electronic Tuning of Misaligned Coils in Wireless Power Transfer Systems
  103. One-comparator counter-based controller for synchronous DC/DC converters
  104. A study on a multi-controller design of the drawtube for aerial boom refueling
  105. Alternative approach to the design of a gain‐scheduled output feedback controllers
  106. Wireless Power Transfer Using Class E Inverter With Saturable DC-Feed Inductor
  107. Research and design on a control system for a disk-type flying robot with multiple rotors
  108. Real-time obstacle collision avoidance for fixed wing aircraft using B-splines
  109. Tuning Class E Inverters Applied in Inductive Links Using Saturable Reactors
  110. Framework for Flight Loads Analysis of Trajectory-Based Manoeuvres with Pilot Models
  111. Intelligent Collision Avoidance for Multi Agent Mobile Robots
  112. Electronic tuning of a high frequency DC/AC inverter for inductive power transfer
  113. Wireless power transfer using Class E inverter with saturable DC-feed inductor
  114. Modelling and Control of a Star-Shaped Octorotor
  115. Gain-scheduledH∞control via parameter-dependent Lyapunov functions
  116. Application of L1 Adaptive Controller to Longitudinal Dynamics of a High Manoeuvrability Aircraft
  117. Optimised configuration of sensors for fault tolerant control of an electro-magnetic suspension system
  118. Automated return-to-route manoeuvres for Unmanned Aircraft systems
  119. Automated return-to-route maneuvers for unmanned aircraft systems
  120. Fault-tolerance for quadrotor-type UAVs
  121. A multiobjective trajectory optimisation method for planning environmentally efficient trajectories
  122. Application of pilot models to study trajectory based manoeuvres
  123. Multi-objective Control Allocation with Conflict Resolution
  124. Positioning Algorithm for Autonomous Thermal Soaring
  125. Vector Based Kinematic Closed-Loop Attitude Control-System for Directional Drilling
  126. Rotary Steerable Directional Drilling Stick/Slip Mitigation Control
  127. Attitude control system for directional drilling bottom hole assemblies
  128. Real-time optimal techniques for unmanned air vehicles fuel saving
  129. Computational Air Traffic Management
  130. Minimum strain energy waypoint-following controller for directional drilling using OGH curves
  131. Real-time Trajectory Generation for Collision Avoidance with Obstacle Uncertainty
  132. Road vehicle state estimation using low-cost GPS/INS
  133. Linear Parameter Varying control of a quadrotor
  134. A comparison of neural networks for FDI of rolling element bearings – demonstrated on experimental rig data
  135. Computing the maximum transient energy growth
  136. On-board trajectory generation for collision avoidance in unmanned aerial vehicles
  137. A review of ground vehicle dynamic state estimations utilising GPS/INS
  138. Linear feedback control of transient energy growth and control performance limitations in subcritical plane Poiseuille flow
  139. Recursive Variable Horizon Trajectory Control for Directional Drilling Using Elliptical Helixes
  140. Recovery from rotor failure for quadrotor-type UAVs
  141. LMI Formulations for Minimal Sensitivity Finite Word Length Controller Realizations
  142. Unmanned aerial vehicle aerodynamic model identification from a racetrack manoeuvre
  143. Propulsion and Flight Controls Integration for a Blended-Wing-Body Transport Aircraft
  144. Direct Method Based Control System for an Autonomous Quadrotor
  145. Finite wordlength controller realisations using the specialised implicit form
  146. Robust Linear Feedback Control of Attitude for Directional Drilling Tools (13th IFAC Symposium on Automation in Mining, Mineral and Metal Processing)
  147. Effector Failure Mitigation by Control Allocation for a UAV with Integrated Fluidic Control Devices
  148. Aircraft Route Re-planning for a Pop-up Obstacle using a Direct Method
  149. Feedback control of transient energy growth in subcritical plane Poiseuille flow
  150. Simulation of wake vortex effects for UAVs in close formation flight
  151. A Quaternion-Based Inverse Dynamics Model for Real-Time UAV Trajectory Generation
  152. LPV Autopilot Design of a Jindivik UAV
  153. Modeling of Wake Vortex Effects for Unmanned Air Vehicle Simulations
  154. Quaternion-Based Inverse Dynamics Model for Expressing Aerobatic Aircraft Trajectories
  155. Ideal Vehicle Sideslip Estimation Using Consumer Grade GPS and INS
  156. Diesel engine indicated and load torque estimation using a non-linear observer
  157. Linear and non-linear simulations of feedback control in plane Poiseuille flow
  158. Design of poiseuille flow controllers using the method of inequalities
  159. Real-Time Transient Three Spool Turbofan Engine Simulation: A Hybrid Approach
  160. Minimizing transient energy growth in plane Poiseuille flow
  161. A numerical investigation into the effect of engine bleed on performance of a single-spool turbojet engine
  162. Simulations of Feedback Control of Early Transition in Poiseuille Flow
  163. Optimal Finite-precision Implementations of Linear Parameter Varying Controllers
  164. Linear quadratic control of plane Poiseuille flow–the transient behaviour
  165. On the Minimization of Maximum Transient Energy Growth
  166. A Unifying Framework for Finite Wordlength Realizations
  167. INTEGRATION OF H∞ AND TIME DOMAIN SPECIFICATIONS USING THE CONVEX COMBINATION METHOD
  168. Complexity of controllers (cyber-physical systems)
  169. A linear state-space representation of plane Poiseuille flow for control design: a tutorial
  170. Optimal controller and filter realizations using finite-precision, floating-point arithmetic
  171. MINIMISATION OF TRANSIENT PERTURBATION GROWTH IN LINEARISED LORENZ EQUATIONS
  172. Optimal realizations of floating-point implemented digital controllers with finite word length considerations
  173. A unified closed-loop stability measure for finite-precision digital controller realizations implemented in different representation schemes
  174. A three-term backpropagation algorithm
  175. A Comparison of Dynamic Models of Various Complexity for Diesel Engines
  176. Detailed analytical model of a single-cylinder diesel engine in the crank angle domain
  177. Genetic algorithm approach to designing finite-precision controller structures
  178. Controller realizations of a teleoperated dual-wrist assembly system with finite word length considerations
  179. Reduction of controller fragility by pole sensitivity minimization
  180. Digital Controller Implementation and Fragility
  181. Instantaneous friction components model for transient engine operation
  182. Comments on "On the structure of digital controllers with finite word length consideration"
  183. Finite word length stability issues in an l1framework
  184. Optimal finite-precision controller realization of sampled-data systems
  185. Stability issues of finite precision state estimate feedback controller realizations for discrete time systems
  186. Optimal FWL controller structures in the delta-operator domain
  187. Dynamic simulation of a single-cylinder diesel engine including dynamometer modelling and friction
  188. A genetic algorithm approach to designing finite-precision PID controller structures
  189. Maximizing lower bound stability measure of finite precision PID controller realizations by nonlinear programming
  190. Adaptive simulated annealing for designing finite-precision PID controller structures
  191. Optimal digital controller structure for a fluid power system subject to wordlength constraints
  192. A mathematical transient model for the dynamics of a single cylinder Diesel engine
  193. Simulated annealing for multiobjective control system design
  194. Evolutionary Hinfin; design of an electromagnetic suspension control system for a maglev vehicle
  195. Simulated annealing for multi-objective control system design
  196. Robust control of a paper machine
  197. Robust control of an unknown plant - the IFAC 93 benchmark
  198. MODCONS - a MATLAB toolbox for multi-objective control system design
  199. Robust control of the benchmark problem using H∞ methods and numerical optimization techniques
  200. Robust controller design using H/sub ∞/ loop-shaping and the method of inequalities
  201. EMS control system design for a maglev vehicle—A critical system
  202. Critical Control of the Suspension for a Maglev Transport System
  203. A Simulated Annealing Inequalities Solver
  204. A MoI Based on ℌ∞ Theory — with a Case Study
  205. Multi-objective design of finite word-length controller structures
  206. Multiobjective design of low complexity digital controllers
  207. Multiobjective design using various control techniques
  208. Fuzzy sliding mode control for a robot manipulator
  209. Robust adaptive control for robot manipulators
  210. Multiobjective robust control using evolutionary algorithms
  211. A mixed optimization approach to multiobjective computer-aided control system design
  212. Algorithms for the method of inequalities-a comparative study