International Journal of Aeronautical and Space Sciences

Papers
(The TQCC of International Journal of Aeronautical and Space Sciences 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 2021-12-01 to 2025-12-01.)
ArticleCitations
Ramped Vane Control of a Compression Corner-Induced Flow Separation36
Measurements of the Laminar-Separated Region on the Airfoil with Actively Deflected Flap27
Correction to: Numerical Investigation of Wing–Multiple Propeller Aerodynamic Interaction Using Actuator Disk Method21
Software Safety Assurance in Non-airborne GPS-based Landing Aids18
Nonlinear Active Disturbance Rejection Controller Design for Drag-Free Satellite with Two Test Massess14
S2MSim: Cycle-Accurate and High-Performance Simulator Based on Multi-Threading for Space Multi-Core Processor13
Coking Test Using Jet A-1 and Desulfurized Kerosene in a Regenerative Cooling Channel Environment13
An Investigation on V-Notch Controlled Asymmetric Supersonic Jet13
Spacecraft Attitude Control with On-Off Thrusters via Convex Optimization Based Control Allocation13
The Influence of Strut Injection Methods on Flame Stabilization and Combustion Performance of Scramjet Engines: A Review12
A New Strategy of Visibility Conflict Optimization Between Multiple Ground Stations and Satellites12
Model-Assisted Probability of Detection Using QL-Scan GUPI for Wall-Thinning Defects12
Structural Analysis of Wing–Fuselage Lug Attachment12
A Study on the Weapon–Target Assignment Problem Considering Heading Error12
Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1: Performance and Operation)11
Vulnerability Analysis of Satellite Under the Impact Hypervelocity Projectile Considering the Formation of Behind-Plate Debris11
Small Airborne Object Recognition with Image Processing for Feature Extraction11
Effect of Jet–Wake Interaction around a Tip-Jet Rotor in Torque-Balanced States10
Airfoil Inverse Design Using a Deep Neural Net with an Explainable Attention Mechanism10
Enabling Real-Time, Modular Autonomy Flight Software for Space Robotics: Bridging Deterministic Control and Dynamic Simulation10
Optimal Guidance Law for Impact Angle and Acceleration Constraints with Time-Varying Gains10
Improved Mars Terrain Segmentation in Terms of Style Transfer and Network Architecture10
An Investigation of Internal Drag Correction Methodology for Wind Tunnel Test Data in a High-Speed Air-Breathing Vehicle Using Numerical Analysis10
Numerical Analysis of Vertical Axis Wind Turbine for Enhanced Performances10
Research on the Process of Dispersing the Bullet by a Large-Size Gasbag with Multiple Inlet Nozzles Based on the Fluid–Structure Interaction Method10
Line-of-Sight Guidance Law Based on GPC with Variable Prediction Horizon10
Task Assignment for Multiple Multi-purpose Unmanned Aerial Vehicles Using Greedy Algorithm9
Selected Papers from the 12th Asia–Pacific International Symposium on Aerospace Technology (APISAT 2021) (Jeju, Republic of Korea, Nov. 15th–17th, 2021)9
Thermally Induced Satellite Vibrations: Rigid-Flexible-Thermal Coupling in LEO, GEO, and DRO9
Thermal Design Analysis of Low Earth Orbit Optical Telescope ROKITS9
Influence of Fillers on the Post-buckling Behavior of the Hat-Stiffened Composite Panels9
Fatigue Life Prediction of Composite Laminate Based on Stress of Fiber and Matrix of UD Composite9
Energy-Based Nonlinear Scaling Methodology for Predicting Fatigue Life of PBGA Solder Balls under Cyclic Thermal Loading9
Lyapunov-Based Nonlinear Model Predictive Control for Attitude Trajectory Tracking of Unmanned Aerial Vehicles9
An Approximate Method for Buckling Analysis and Optimization of Composite Lattice Conical Panels Considering Geometric Parameters9
Reentry Risk and Safety Assessment of Spacecraft Debris Based on Machine Learning9
Adaptive Feedforward Control Method of Turboshaft Engine Based on Invariance Principle and Least Square Method9
Review on Flight Control Law Technologies of Fighter Jets for Flying Qualities9
Second-Order Sliding Mode Guidance Law of a Nonsingular Fast Terminal with a Terminal Angular Constraint8
Hybrid Adaptive Dynamic Inverse Compensation for Incipient and Time-Varying Multi-faults of Morphing Fighter8
Investigation of the Laminating Characteristics of CFRP Plates with a Thin and Wide Configuration in Production for an Effective Inspection Process8
Effects of Thermo-chemical Models on Linear Stability Analysis of Chemically Reacting Hypersonic Boundary Layers8
3-D Flight Performance Simulation of a Liquid-Filled Quadrotor8
Supersonic MLN Thrust Correction at HT with Application to The Missile Trajectory8
Event-Triggered Adaptive Fixed-Time Trajectory Tracking Control for Stratospheric Airship8
Firmware Updating Approach for FPGA-Based SDR Nanosatellite Payload8
Numerical and Experimental Analysis of Three-Dimensional Boundary-Layer Transition Induced by Isolated Cylindrical Roughness Elements7
Derivation of Buckling Knockdown Factors for Pressurized Orthogrid-Stiffened Cylinders of Launch Vehicle Structures7
Hypervelocity Impact Shielding Sandwich RAS with Miura-Ori Core Composed of NCF/PEEK Thermoplastic Composites7
Mechatronic Approaches to Synthesize Biomimetic Flapping-Wing Mechanisms: A Review7
Integrated Acoustic Analysis of Payload Fairing Using an FE-SEA Hybrid Method7
Simultaneous Vibration Reduction and Performance Improvement of Helicopter Rotor Using Individual Blade Pitch Control with Multiple Harmonic Inputs7
Comparative Analysis of Inerting Effects of Open and Closed Vent Systems Fuel Tanks7
Standard Procedure-Guided Flight Trajectory Pattern Mining for Airport Terminal Airspace7
An Investigation of Multi-rotor Drone Noise Based on the Acoustic Hemisphere in an Actual Environment7
Observation of the Development Process of Mack Second Mode Boundary-Layer Transition Using an Impulse-Type Hypersonic Shock Tunnel7
Design and Verification of Electric Pump for Small LOX/Methane Rocket Engine7
Optimizing Nanosatellite Power Generation Integrating Heat Pipes and Thermoelectric Generators for Low Earth Orbit Conditions7
FPGA-based Inference Parallelization for Onboard RL-based Routing in Dynamic LEO Satellite Networks7
Suppression of Pressure Oscillation in Supersonic Parachute Model Using a Ring6
Improvement of Heat Transfer Model Considering Heat Transfer Deterioration of Supercritical Fluid in Cooling Channel of Scramjet Propulsion System6
Orbit Control of an Earth Orbiting Solar Sail Satellite6
Extracting Flight Plans from Recorded ADS-B Trajectories6
A Comparative Study of Chemical-Kinetic Mechanisms for Combustion of Methane/Hydrogen/Air Mixtures6
Testing and Prediction of Heat Exchanger Performance for Liquid Propulsion Engine Based on Simulation Experiment6
Incorporating Airspace Constraints in Multi-phase 4D Trajectory Optimization Based on Improved Adaptive Mesh Refinement Method6
Research on Optimal Control Method for Turbofan Engine Acceleration Process with Variable Air Bleed Considering High Pressure Turbine Guide Vane Life6
Computational Fluid Dynamics Simulations of a Novel Dual-Throat Bent Nozzle6
FOPID Control of Quadrotor Based on Neural Networks Optimization and Path Planning Through Machine Learning and PSO Algorithm6
Performance Analysis of Passive Magnetic Pointing Method for Implementation of Directional Antennas on CubeSats6
Estimation Method for Pitching Moment Non-linearities of Cranked Arrow Wing at Low Speed6
Adaptive Fuzzy Logic Control Framework for Aircraft Landing Gear Automation: Optimized Design, Real-Time Response, and Enhanced Safety6
Nonlinear Dynamic Inversion Control Performance Enhancement: Aerospace Perspectives6
Aeroservoelastic Characteristics of a Corrugated Morphing Control Surface6
Vision-Based Aircraft Marshalling Recognition and UAM Control Command Generation6
Applicability of the Ti6Al4V Alloy to the Roller Arm for Aircraft Parts Made Using the DMLS Method6
Deflection Analysis of Flexible Cantilever Beam with a Drop Impact6
Simultaneous Control of Battery Charging and Load-Following for Gasoline Electric Power Systems with Output Ratio Control by a Single Parameter6
Design Factors of High-Speed Turbo-Electric Distributed Propulsion System6
Effect of Primary Holes Structure on Flow Characteristic and Combustion Performance of High Temperature Rise Combustor Based on RQL6
Relative Navigation Performance of LEO Vehicles Considering GPS–KPS Constellation and Measurement Characteristics6
Review of Machine-Learning Approaches for Object and Component Detection in Space Electro-optical Satellites6
Adaptive Controller Approach for a Three-Axis Helmholtz Magnetic Test-Bed to Test Detumbling Simulations in the GWSAT Satellite6
The Investigation of Rotating Instability Under Distortion Based on a Compressor Rotor5
Altitude-Dependent Analysis of Combustion Performance and Emissions in a Commercial Aircraft Engine Leveraging Real Engine Data5
Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 2: Core Technologies)5
Fiducial Marker-Based Autonomous Landing Using Image Filter and Kalman Filter5
Location-Based Integration of Internal Lattice Structures in a Turbine Blade for Mass Reduction and Dynamic Characteristic Comparison5
Examination of Fixed-Pitch Quadrotor Performance in a Slalom Maneuver Using Inverse Simulation5
Deep Learning Performance Comparison Using Multispectral Images and Vegetation Index for Farmland Classification5
Correction: Time-Optimal Guidance Laws Using a Frequency Domain Approach for Spacecraft Rendezvous5
Rapid Airfoil Inverse Design Method with a Deep Neural Network and Hyperparameter Selection5
Velocity Profile Optimization for Multiple UAVs Collision-Free Mission Planning5
Free Final-Time Low Thrust Trajectory Optimization Using Homotopy Approach5
Correction to: Computational Modeling of Frost Thickness on a Flat Plate Surface Considering Growth Rate with Regression Method and its Validation5
Retraction Note: Sentinel-2 Cloud Mask Classification Using Deep Learning Method5
Adaptive Attitude Scheduling and Robust Control for Hyper-agile Spacecraft with Uncertainties5
Three-Dimensional Cooperative Guidance Law Against Maneuvering Target with Time-Varying Communication Delays5
Combustion Characteristics of Shear Coaxial Injectors with Different Recess Lengths Under Wide Operating Conditions5
A Load Balance Local LEO Satellite Network AP Selection Strategy5
Trajectory Planning with Collision Avoidance for Multiple Quadrotor UAVs Using DMPC5
Design and Optimization of Winglet Shapes for Cambered Aerofoil4
Transformer Network-Aided Relative Pose Estimation for Non-cooperative Spacecraft Using Vision Sensor4
Prediction of Aircraft Departure/Spin Characteristics by Improving Kalviste Decomposing and Weak Nonlinear Analysis Method4
An Optimal Control Method for Trajectory Tracking and Swing Suppression in Helicopter-Slung Load System4
Three-Dimensional Trajectory Planning for Unmanned Aerial Vehicles Using an Enhanced Crowned Porcupine Optimization Algorithm4
Numerical Study on the Dynamic Behavior of Layered Structures under High-Velocity Impact4
Weapon-Target Assignment and Firing Scheduling for Rapid Engagement with Heterogeneous Interceptors4
An Artificial Intelligence-Based Failure Prediction Model for Three-Dimensional Woven Composite of Aircraft Wings4
Attitude Guidance for Constraining Star Tracker Elevation Angle During CubeSat-to-Ground Laser Pointing4
Aerodynamic and Aeroacoustic Effects of Variable Rotor Speed in a Coaxial Rotor System4
A Cascade Heuristic Algorithm-Based Optimized Assembly Method for Modular Micro–nano-satellite4
Development of a Machine Learning-Based Load Monitoring System for Aircraft Fatigue Life Management4
High-Fidelity Simulation and Performance Analysis of Twin-Spool Turbofan Engine Based on Multi-dynamics Approach4
Theoretical and Experimental Study on an Active–Passive Integrated Variable Stiffness Vibration Isolator4
Energy Evolution and Transfer Characteristics in Spatial Particle–Spring–Beam Model4
Research on the Integrated Modeling Method of Inlet and Engine Based on Component Level Model4
Seasonal and Segmental Variations and Peaks in Aircraft Engine Exhaust Gas Temperature4
Performance Analysis of a Ducted Rocket Under Various Flight Conditions4
Moment-Based Mass Estimation Relationship for Initial Sizing of Fixed-Wing Unmanned Aerial Vehicles4
MEMS Load Cell for Measuring μN Level Thrust of the Micro-thrusters4
Optimizing Low-Altitude Urban Airspace: Identifying Free Route Airspace and Control Points Through Spatial Analysis4
Detection of Internal Damage in CFRP-Laminated Plates Using Signal Extraction Method4
Optimization of Duct Shape for Improving Aerodynamic Performance of Ducted Tail Rotor4
Aerodynamic Analysis of High-Speed Compound Unmanned Rotorcraft Using an Unstructured Flow Solver4
Real-Time Path Planning for Unmanned Aerial Vehicles Based on Compensated Voronoi Diagram4
Numerical Study of Flow Control to Increase Vertical Tail Effectiveness of an Aircraft by Tangential Blowing4
Correction: Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow4
Study on the Viability of a Midsize Hybrid Electric Aircraft via Initial Sizing Methodology4
Experimental Investigation of Effect of Corrugations on Delta Wing for Lift Enhancement in Low Reynolds Number Flow4
A Study on Ejector Verification Using Natural Intake Method4
Numerical Investigations of Bump Effects on the Performance of Double-Ended Airfoils and ABC Rotors4
Dynamic Takeoff and Landing Control for Multi-Rotor eVTOL Aircraft4
Delayed Detached-Eddy Simulation of Subsonic Axisymmetric Base Flow4
Multi-modal Neural Adaptive Observer for Sensor and Actuator Fault Detection and Identification4
An Approximate Calculation Method for the Average Infrared Radiation Intensity in the Rear Hemisphere of Serpentine 2D Exhaust Systems Based on Limited Data3
An Immersed Boundary Method for Conjugate Heat Transfer Involving Melting/Solidification3
Aerodynamic Modeling and Verification of Quadrotor UAV Using Wind-Tunnel Test3
Trajectory Linearisation of Relative Motion to Elliptical Orbit Target Using Tschauner–Hempel Equation3
Adaptive Robust Servo LQR Control for Aircraft Under a Wide Range of Icing Conditions3
Nonsingular Predefined-Time Guidance Law with Line-of-Sight Angle Constraint for an Air-to-ground Missile3
Investigation on Lunar Landing Candidate Sites for a Future Lunar Exploration Mission3
Efficiency-Based Airport Ground Conflict Detection and Resolution: Integrating Stand Hold Strategy with Constrained Position Shifting3
Correction to: Preliminary Trajectory Design for Mitigating Debris Utilizing Solar Sailing and Conventional Propulsion3
Performance Design of a Turbofan Engine Using Multi-objective Particle Swarm Optimization (MOPSO)3
A Refined Protected Zone Model and Conflict-Aware Algorithm for Manned and Unmanned Fusion Airspace3
Finite-Time Attitude Maneuver Control for Liquid-Filled Spacecraft with Attitude and Angular Velocity Constraints Based on Barrier Lyapunov Function3
Post Flight Analysis Using Numerical Weather Prediction Data, KLAPS3
Investigation into Active and Passive Methods to Enhance Aerofoil Aerodynamic Performance3
Experimental Quantification and Computational Synergy of Dual Cross Tubular Combustion in Twin Turbojet Engines: A Mach-Regime Thermochemical Disruption3
Collaborative Covert Trajectory Planning for Spacecraft Formation Based on Configuration Transformation and Maintenance3
Spars Effect on the Stress Reduction in the Multi-box Airfoils3
Nonlinear Passivity-Based Control for Spacecraft 6-DOF Maneuver with Saturation Accommodation3
Prediction of Airfoil Lift Coefficient Based on Multilayer Perceptron3
Fine Pointing and Tracking Onboard System for CubeSat Optical Satcom3
CFD Analysis of a Missile Nozzle Performance for Three Different Fuels Under Non-premix and Partially Premix Condition3
Reconfigurable Fault-Tolerant Dynamic Control Allocation Against Multiple Effectors Impairment3
Prediction of Instantaneous Impact Point of Launch Vehicle, Including Drag Effect3
A Convex Programming-Based Approach to Trajectory Optimization for Survivability Enhancement of Homing Missiles3
Correction: Vision-Based Aircraft Marshalling Recognition and UAM Control Command Generation3
Numerical Investigations on the Influence of Ramp Locations in a Strut Injection Scramjet Combustor3
Causality-Seq2Seq Model for Battery Anomaly Detection3
Design of an Elliptical Orbit Constellation for High-Resolution Optical Observations over a Specific Area3
Integrated Optimization Design Using Improved Pigeon-inspired Algorithm for a Hypersonic Vehicle Model3
Optimization and Analysis of Key Parameters for Urban Air Mobility Vehicle3
Sliding Mode Control Method Research Based on Command Compensator for the Hypersonic Cruise Vehicle3
Study on Energy Balance at the Operating Points of Staged Combustion Cycle LRE3
Observer-Based Predefined-Time Anti-saturation Fault-Tolerant Attitude Tracking Control for Carrier-Based Aircraft with Output Constraints3
Global Trends in Airframe Research Using a Scientometric Approach3
A Study on Vibration Attenuation of Structure Applied on Eddy Current Damper3
Integrated Design of Variable Geometry Chin Inlet with Waverider Forebody3
Mode Decision Control Method for Adaptive Cycle Engine Based on Inlet and Engine Matching3
Frequencies, Modes, and Amplitudes of Supersonic Axisymmetric Nozzles Vibration3
Cooperative Global Path Planning for Multiple Unmanned Aerial Vehicles Based on Improved Fireworks Algorithm Using Differential Evolution Operation3
Third-Party Risk Assessment on the Ground for Urban Air Mobility Operations: A Case Study of Seoul Metropolitan City3
Design, Aerodynamic and Aero-acoustics Performances Based Comprehensive Investigations on Wing with and Without the Performance Enhancers of Hybrid Multirotor UAVs3
Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow3
Geometric Effects of Liquid Rocket Engine Pintle Injectors in Supercritical Combustion3
LES Study on the Ground Vortex Aerodynamics Characteristic Under Time-Varying Inlet Flow Rate and Incoming Flow Direction3
Determination of Acceptable Ranges of Asymmetric Manufacturing Tolerances based on Structural Analysis for a Drone Wing3
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