Aeronautical Journal

Papers
(The TQCC of Aeronautical Journal is 3. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-06-01 to 2025-06-01.)
ArticleCitations
Reinforcement learning-adaptive fault-tolerant IGC method for a class of aircraft with non-affine characteristics and multiple uncertainties – CORRIGENDUM96
Simulation framework and development of the Future Systems Simulator26
Distributed planning method for detection array of UAV formation with bearing-only sensor network25
Transit passenger-oriented optimisation of arrival aircraft sequencing23
Damper model identification using mixed physical and machine-learning-based approach22
Investigating the crumpling effect in honeycomb sandwich panels under bending loads using FEA technique22
Towards intermediate complexity modelling of contrail formation: the new dynamical framework RadMod22
Attitude maneuver planning and robust tracking control for flexible satellite21
Shock train response to pulse backpressure forcing21
Actuator fault modeling and fault-tolerant tracking control of multi-vectored propeller aerostat19
Multidisciplinary design optimisation of a fully electric regional aircraft wing with active flow control technology19
On the conditions for absolute minimum fuel burn for turbofan powered, civil transport aircraft and a simple model for wave drag16
Impact of actuation and sensor measurement delays on stability of real-time hybrid aeroelastic simulation system15
Fundamental considerations in the design and performance assessment of propulsive fuselage aircraft concepts15
An extended invariant approach to laminate failure of fibre-reinforced polymer structures15
Assessing evidence-based training in a collaborative virtual reality flight simulator15
Fixed-time anti-saturation control with concise system structure for the 6-DOF motion of spacecraft15
Frederick W. Lanchester and Aerodynamics: why an automotive engineer wrote a book for aerodynamic education12
Relative rotor phasing for multicopter vibratory load minimisation11
Elaboration and outlook for metal hydride applications in future hydrogen-powered aviation11
Estimating the required number of Harbour Pilots to support airline operations of a single pilot commercial aircraft at a UK regional airport11
Thermal management system design for a series hybrid-electric propulsion architecture11
Aerodynamic characteristics of different configurations of mechanically deployable aerodynamic decelerator in subsonic region10
Multiple unmanned aerial systems collision impacts on wing leading edge10
Output constrained neural adaptive control for a class of KKVs with non-affine inputs and unmodeled dynamics9
Effect on damage of aircraft windshield impacted by light UAV with different postures9
Base heating and stage separation of launch vehicles9
Ground collision avoidance system with multi-trajectory risk assessment and decision function9
Spacecraft attitude control based on generalised dynamic inversion with adaptive neural network9
Application of SysML for digital transformation of aircraft cabin systems8
Propeller aerodynamic optimisation to minimise energy consumption for electric fixed-wing aircraft8
Low-visibility commercial ground operations: An objective and subjective evaluation of a multimodal display8
Mitigation of flow separation in a highly bent intake duct with active and passive flow control8
Comparison of structural model reduction methods applied to a large-deformation wing box8
A deep reinforcement learning-based approach to onboard trajectory generation for hypersonic vehicles8
Tail-shake risks assessment & mitigation by wind-tunnel tests on air-intake installation on a heavy-weight H/C configuration8
A review of propeller stall flutter7
Estimation of safe flight envelope considering manoeuver overload based on cost-limited reachable set7
Optimisation analysis of reinforced cable distribution on the airship7
A multi-layer Kriging surrogate model for the reliability analysis of variable stator vanes in aero engines7
Rapid dynamic aeroelastic response analysis of the highly flexible wing with distributed propellers influence7
Genetic algorithm-based path planning of quadrotor UAVs on a 3D environment7
Improvements in learning to control perched landings6
A study on the mixing and infrared signal characteristics of a lobed mixer in a micro turbojet engine6
Small aircraft flight trajectory optimisation using a multidisciplinary approach6
Propulsive jet aerodynamics and aeroacoustics6
Periodic morphing of a NACA6409 aerofoil in ground effect, its wake mechanisms and thrust generation6
Compressibility corrections to extend a smooth local correlation-based transition model to transonic flows6
Cooperative line-of-sight guidance strategy with prescribed performance and input saturation against active defensive aircraft in two-on-two engagement6
Transit passenger-oriented optimisation of arrival aircraft sequencing – CORRIGENDUM6
Integration of CFO-based three-dimensional target manoeuver compensation guidance rate and transition region optimisation algorithm – CORRIGENDUM6
Analysis and optimisation design on damping orifice of oleo-pneumatic landing gear6
Evaluation of reduced-order models for the rapid aerodynamic analysis of supersonic and hypersonic bodies6
Predictor corrector algorithms considering multiple constraints for entry vehicles6
Impact of tank gravimetric efficiency on propulsion system integration for a first-generation hydrogen civil airliner6
Gas turbine prognostics via Temporal Fusion Transformer6
Investigation of rarefied flow over backward-facing step in different rarefaction regimes using direct simulation Monte Carlo6
Hydrogen-air lean premixed turbulent highly swirled flames stabilisation: experimental demonstration and mechanistic-kinematic description6
Battery pack technological considerations for hybrid-electric regional aircraft feasibility6
Performance of a turbojet engine with fluidic thrust vectoring6
An integrated fault-tolerant control strategy for control surface failure in a fighter aircraft5
Derivation of structural weight estimation for Unmanned Combat Aerial Vehicle (UCAV)5
Sand erosion modeling in generic compressor rig testing5
Numerical and theoretical investigation of helicopter ditching for variations in initial velocity and pitching angle5
Harmonising and standardising military airworthiness in Europe: a review of key aspects and achievements5
Experimental and numerical investigation on a supersonic inlet with large bleed window5
Aerodynamic assessment of wingtip-mounted propeller and distributed propulsion system5
Development of a design space for dissimilar materials joining in aerospace applications5
A comprehensive review and future challenges of energy-aware path planning for small unmanned aerial vehicles with hydrogen-powered hybrid propulsion5
Velocity obstacle–based conflict resolution and recovery method5
A novel stochastic matheuristic approach for the dynamic utilisation of arrival route structures: modelling of Istanbul Airport point merge system5
Collaborative navigation method based on adaptive time-varying factor graph5
Steady and unsteady aerodynamic loading of a NACA 16-616 aerofoil in a uniform flow5
Dynamic responses due to the Dryden gust of an autonomous quadrotor UAV carrying a payload5
Linear parameter-varying model order reduction and control design of FLEXOP demonstrator aircraft5
Experimental analysis of noise disturbances generated by reaction wheel4
A novel approach to runway overrun risk assessment using FRAM and flight data monitoring4
Numerical analysis of the impact of release timing on trajectory in internal store separation4
Parametric cost estimation models of civil aircraft for the preliminary aircraft design phase4
Vision geometry-based UAV flocking4
Signal corrector and decoupling estimations for UAV control4
Eye-tracking analysis to assess the mental load of unmanned aerial system operators: systematic review and future directions4
AER volume 125 issue 1289 Cover and Front matter4
Numerical investigation of the dynamic stall reduction on the UAS-S45 aerofoil using the optimised aerofoil method4
Design and dynamic analysis of landing mechanism for crew lunar vehicles4
A methodology to determine the precision uncertainty in gas turbine engine cycle models4
Control barrier function based terrain and path following control of unmanned aerial vehicle considering attitude constraint4
The RAeS 2023 written paper prizes4
Historical Development of the Coaxial Contra-Rotating Propeller – CORRIGENDUM4
Design and performance of directional rectification control system in an aircraft with a novel type of wheel-ski landing gear4
An estimation method for the fuel burn and other performance characteristics of civil transport aircraft; part 3 full flight profile when the trajectory is specified4
Lift alleviation in travelling vortical gusts4
Flow Simulation of the Flight Manoeuvres of a Large Transport Aircraft with Load Alleviation – ERRATUM4
The flight efficiency analysis on the Multi-Arrival Route Point Merge System4
Neural network-based velocity-controllable UAV flocking4
Effect of process parameters on the corrosion characteristics of friction stir welded aluminum alloy AA2014-T64
AER volume 125 issue 1291 Cover and Back matter4
Three-dimensional robust nonlinear cooperative guidance law for spatiotemporal coordination under stringent input constraint4
Design of a haptic obstacle avoidance for low-speed helicopter operations using active sidesticks4
Is deep learning superior to traditional techniques in machine health monitoring applications4
Methodology for shape prediction and conversion of a conventional aerofoil to an inflatable baffled aerofoil3
Distributed cooperative guidance law without numerical singularity with field-of-view angle constraint3
A frequency domain approach for reduced- order transonic aerodynamic modelling3
Time-dependent reliability optimisation for retraction mechanism with multiple clearance joints under wear3
Compliant mechanism design of combined aircraft wing for stable separation – CORRIGENDUM3
A human factors accident analysis framework for UAV loss of control in flight3
Landing gear ground manoeuvre statistics from automatic dependent surveillance-broadcast transponder data3
Plume flow characteristics of rectangular exhaust nozzles in a micro-jet engine3
A Monte Carlo approach for capacity and delay analyses of multiple interacting airports in Istanbul metroplex3
Vertical take-off and landing hybrid unmanned aerial vehicles: An overview3
Future aircraft concepts and design methods3
Sliding mode corrector for jet UAV control3
Attitude tracking control of hypersonic vehicle based on an improved prescribed performance dynamic surface control3
Transition flight of a concept of lifting-wing quadcopter3
Abating CO2 and non-CO2 emissions with hydrogen propulsion3
Autonomous and cooperative control of UAV cluster with multi-agent reinforcement learning3
Flight control strategy for jet transport in severe clear-air turbulence based on flight data mining3
Experimental investigation on droplet evaporation characteristics during combustion of future and current aviation fuels with range of properties3
A CSR-based visible and infrared image fusion method in low illumination conditions for sense and avoid3
Static and dynamic characteristics of supersonic cruise missile with damaged wing3
A stochastic programming model for the aircraft sequencing and scheduling problem considering flight duration uncertainties3
A dimensionality reduction approach in helicopter level flight performance testing3
AER volume 125 issue 1292 Cover and Back matter3
Impact of operator characteristics on landing gear ground manoeuvre occurrences3
Off-board aerodynamic measurements of small-UAVs in glide flight using motion tracking3
Attitude modelling and real-time robust control of a 3-DoF quadcopter UAV test bench3
Improvement of FFD parametric approach in the application of a lifting body3
Identification and classification of operating flow regimes and prediction of stall in a contra-rotating axial fan using machine learning3
The RAeS 2021 Written Paper Prizes3
Aerodynamic design of a high-efficiency two-stage axial turbine, using streamline curvature method and performance optimisation by clocking of stator blades3
In-orbit results from the attitude determination and control system of ALSAT-2B3
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