International Journal of Aeronautical and Space Sciences

Papers
(The median citation count of International Journal of Aeronautical and Space Sciences is 0. 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 2021-04-01 to 2025-04-01.)
ArticleCitations
Investigation into Active and Passive Methods to Enhance Aerofoil Aerodynamic Performance28
S2MSim: Cycle-Accurate and High-Performance Simulator Based on Multi-Threading for Space Multi-Core Processor28
Study on Characteristic Modeling and Command Tracking Control Method for Variable Configuration Aircraft25
An Investigation on V-Notch Controlled Asymmetric Supersonic Jet19
A Semi-Supervised Object Detection Method for Close Range Detection of Spacecraft and Space Debris17
Monte-Carlo Simulation for Analyzing the Performance Variation of a Liquid Rocket Engine Using Gas-Generator Cycle16
Numerical Study of Flow Control to Increase Vertical Tail Effectiveness of an Aircraft by Tangential Blowing16
Attitude Guidance for Constraining Star Tracker Elevation Angle During CubeSat-to-Ground Laser Pointing15
Performance Analysis of a Ducted Rocket Under Various Flight Conditions14
Three-Dimensional Trajectory Planning for Unmanned Aerial Vehicles Using an Enhanced Crowned Porcupine Optimization Algorithm13
MEMS Load Cell for Measuring μN Level Thrust of the Micro-thrusters12
Structural Soundness Verification of a Composite Oxidant Propulsion Tank for Space Launch Vehicles Through a Structural Static Test11
A Robust Subpixel-Level Celestial Edge Localization Algorithm for Optical Navigation11
Spacecraft Attitude Control with On-Off Thrusters via Convex Optimization Based Control Allocation10
Design, Aerodynamic and Aero-acoustics Performances Based Comprehensive Investigations on Wing with and Without the Performance Enhancers of Hybrid Multirotor UAVs10
Control-Oriented Modeling of a Three-Dimensional Hypersonic Vehicle with Rigid/Flexible Coupling9
Parallel Multiscale Numerical Framework of the Non-linear Failure Analysis for Three-Dimension Composite Structures9
Indirect Estimation Based Active Disturbance Rejection Control for Solar Sail Station-Keeping9
Geometric Effects of Liquid Rocket Engine Pintle Injectors in Supercritical Combustion9
Numerical Investigation on Aerodynamic Performance and Interaction of a Lift-Offset Coaxial Rotor in Forward Flight9
Coking Test Using Jet A-1 and Desulfurized Kerosene in a Regenerative Cooling Channel Environment9
Estimation of Effective Mechanical Properties of Plain Woven Composites Using Direction-Selective Micromechanical Models8
Correction: Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow8
Moment-Based Mass Estimation Relationship for Initial Sizing of Fixed-Wing Unmanned Aerial Vehicles8
A Study on Ejector Verification Using Natural Intake Method8
A New Strategy of Visibility Conflict Optimization Between Multiple Ground Stations and Satellites8
A Method of Metallisation of Carbon Fibre-Reinforced Plastic (CFRP) Sandwich Antenna Reflector Dish for High-Frequency Applications8
Measurements of the Laminar-Separated Region on the Airfoil with Actively Deflected Flap8
A Novel Fixed-Time Convergence Three-Dimensional Guidance Law for Intercepting Highly Maneuvering Targets8
Integrated Optimization Design Using Improved Pigeon-inspired Algorithm for a Hypersonic Vehicle Model7
Regenerative-Cooling Heat-Transfer Performance of Mg/CO2 Powder Rocket Engines for Mars Missions7
A Study on a Terrain Scan Data Generation Algorithm Using Digital Terrain Elevation Data (DTED)7
Relationship between Magnetic Field Interference and Electromagnetic Drag in Multicoil Magnetic Sails7
MPPI-Based Computational Guidance for Impact Time Control with Practical Constraints7
Dynamic Simulation and Aircraft Level Assessment of CMC Implementation on GTF Engine7
Weapon-Target Assignment and Firing Scheduling for Rapid Engagement with Heterogeneous Interceptors7
Structural Analysis of Wing–Fuselage Lug Attachment7
Characteristics of Injection Scheme in Linearized RDE7
A Through-Flow Analysis for Application to Off-Design of Axial Gas Turbines7
Aerodynamic Analysis of High-Speed Compound Unmanned Rotorcraft Using an Unstructured Flow Solver7
Energy Evolution and Transfer Characteristics in Spatial Particle–Spring–Beam Model6
Theoretical and Experimental Study on an Active–Passive Integrated Variable Stiffness Vibration Isolator6
Direct-Numerical Simulation with the Stability Theory for Turbulent Transition in Hypersonic Boundary Layer6
Software Safety Assurance in Non-airborne GPS-based Landing Aids6
Design of a Helicopter System Recovery for a Sounding Rocket6
Closed-Form Solutions for Single-Axis Slew Maneuvers Under a Fixed Final Time Constraint6
Level and Program Analytics of MUM-T System6
Effect of the Flow Passage Area Ratio on a Double Slit-Type Pintle Injector6
Numerical Investigations of Bump Effects on the Performance of Double-Ended Airfoils and ABC Rotors5
Development of Power Plant Trio CanSat Platform Powered by Solar, Wind and Piezo Energy Harvesting Systems5
Simulation and Experimental Research on Shape Adjustment of Membrane Reflector Antenna (MRA) Combined with Electrostatic Forces and Boundary Cable Forces5
A Comparative Study of Hypervelocity Impact Characteristics in Aluminum Whipple Shielding Through 3D Measurement and Numerical Analysis5
Cable Suspension and Balance System with Low Support Interference and Vibration for Effective Wind Tunnel Tests5
Ramped Vane Control of a Compression Corner-Induced Flow Separation5
Efficient Aerodynamic Analysis of Air-Breathing Hypersonic Vehicle using Local Surface Inclination Method based on Unstructured Meshes5
A Study on the Weapon–Target Assignment Problem Considering Heading Error5
UAV Head-On Situation Maneuver Generation Using Transfer-Learning-Based Deep Reinforcement Learning5
Deployment and Blossoming Analysis of a Fiber Reinforced Polymer (FRP) Collapsible Tubular Mast (CTM) Boom for Aerospace Applications5
Numerical Study of Effects of Fuselage and Facility Wall on PSP Rotor Performance in Hover5
Coupled Kernel Extreme Learning Machine and Cuckoo Search for Aerodynamic Modeling and Stability Analysis of Spinning Projectiles5
Correction to: Numerical Investigation of Wing–Multiple Propeller Aerodynamic Interaction Using Actuator Disk Method4
Theoretical Modeling on Three Operation Modes of a Scramjet Isolator4
Nonlinear Active Disturbance Rejection Controller Design for Drag-Free Satellite with Two Test Massess4
Numerical Study on the Dynamic Behavior of Layered Structures under High-Velocity Impact4
Experimental Investigation of Effect of Corrugations on Delta Wing for Lift Enhancement in Low Reynolds Number Flow4
Correction: Thermal Analysis and Control Design for Space Optical Telescope ROKITS4
Development of a Lunar Vehicle with a Hybrid Rocket Engine Produced Using Lunar Resources4
Satellite Imagery Super-Resolution Using Squeeze-and-Excitation-Based GAN4
Soft Landing of a Hybrid Rocket Thruster Powered Platform: Hardware-in-the-Loop Simulation4
Comparison of Test Results and Finite-Element Analysis Using Elastoplastic Modeling of 2.5D C/SiC Composites4
Prediction of Aircraft Departure/Spin Characteristics by Improving Kalviste Decomposing and Weak Nonlinear Analysis Method4
Multidisciplinary Design Optimization Processes for Efficiency Improvement of Aircraft: State-of-the-Art Review4
SIS Error Estimation for Fault Detection of IRNSS Using Beeline Method4
Correction: Thermal Design Analysis of Low Earth Orbit Optical Telescope ROKITS4
Ice Accretion Prediction on Turbofan Engine Nacelle Under Takeoff Conditions Based on Finite-Area Method4
Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1: Performance and Operation)4
Small Airborne Object Recognition with Image Processing for Feature Extraction4
Regulation Scheme of Turbofan Engine Nozzle for Infrared Signature Management4
Study on the Viability of a Midsize Hybrid Electric Aircraft via Initial Sizing Methodology4
Research on the Integrated Modeling Method of Inlet and Engine Based on Component Level Model4
Precise Relative Positioning Using Doppler Measurements of Android Smartphones4
An Assessment of Explosive and Fire Risks from Fighter Jet Collision with Aircraft Carrier4
Prediction and Evaluation of Frosting Surface on Cylindrical Structure Using Growth Rate Model4
Fatigue Life Prediction of Composite Laminate Based on Stress of Fiber and Matrix of UD Composite3
Frequencies, Modes, and Amplitudes of Supersonic Axisymmetric Nozzles Vibration3
Surrogate Model Considering Trim Condition for Design Optimization of High-Aspect-Ratio Flexible Wing3
Modeling and Attitude Disturbance Rejection Control of a Compound High-Speed Helicopter with a New Configuration3
Star Tracker Geometric Calibration Through Full-State Estimation Including Attitude3
Hydrodynamic Ram Test of Composite T-Joint Structure3
The Optimization Process of Aircraft Side Panel’s Weight Reduction Based on Orthogonal Experiment3
Effect of Jet–Wake Interaction around a Tip-Jet Rotor in Torque-Balanced States3
Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow3
A Performance Calculation Method of Coaxial High-Speed Helicopter Engine Based on Power Matching3
A Refined Protected Zone Model and Conflict-Aware Algorithm for Manned and Unmanned Fusion Airspace3
Task Assignment for Multiple Multi-purpose Unmanned Aerial Vehicles Using Greedy Algorithm3
Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed3
Finite-Time Attitude Maneuver Control for Liquid-Filled Spacecraft with Attitude and Angular Velocity Constraints Based on Barrier Lyapunov Function3
Correction: A Survey on Structural Coupling Design and Testing of the Flexible Military Aircraft3
Three-Dimensional Prescribed-Time Impulsive Pinning Cooperative Guidance3
Support Vector Regression-Based Performance Prediction for Unmanned Aerial Vehicles3
Optimal Guidance Law for Impact Angle and Acceleration Constraints with Time-Varying Gains3
A Design Feasibility Study of a Turbine Blade Disc Interface (Dovetail) Made By Four-Directional Braided Ceramic Matrix Composite (Sic/Sic)3
Efficiency-Based Airport Ground Conflict Detection and Resolution: Integrating Stand Hold Strategy with Constrained Position Shifting3
Application of Ground Flutter Emulation Test Technique for the Passive Flutter Suppression Effect Validation3
Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements3
Post Flight Analysis Using Numerical Weather Prediction Data, KLAPS3
Lyapunov-Based Nonlinear Model Predictive Control for Attitude Trajectory Tracking of Unmanned Aerial Vehicles3
Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model3
Study on Performance of Closed Air Circulation System Driven by Electric Compressor3
Rotorcraft Flight Regime Recognition in Complex Maneuvers Using Adaptive Extended Kalman Filter3
Impact of Additive Manufacturing Surface Roughness on the Aerodynamic Performance of Axial Compressor Blades3
Fault-Tolerant Control for Aircraft with Structural Damage Using Sparse Online Gaussian Process Regression3
The Effect of Ambient Pressure and Gas–Liquid Ratio on the Spray Characteristics of an Effervescent Atomizer3
Improved Mars Terrain Segmentation in Terms of Style Transfer and Network Architecture3
Simultaneous Search and Tracking of Non-cooperative Mobile Targets Using Multiple UAVs in Uneven Environments3
Cost Estimation of Earth Observation Satellites Based on Technology-Aware Complexity and Cost Adjustment3
A Climb-and-dive Guidance Law with the Altitude Constraint3
Passive Reduction of Pressure Fluctuation by Using Cylindrical Rod on Open Cavity3
Three-Dimensional Prescribed Performance Guidance Law with Field-of-View Constraint and Feasibility Analysis3
Fluid–Structure Interaction Analysis of a Fabric Skin for Fabric-Covered Wind Turbine Blades3
An Investigation on Constant Convection Coefficient Assumption in Decoupled Conjugate Heat Transfer3
Multi-disciplinary Optimization of Wing Sandwich Structure using Proper Orthogonal Decomposition and Automatic Machine Learning3
Optimum Design of Liquid Fuel Launch Vehicle Based on Design of Missile Under Uncertainty with Latin Hyper-cube Method (LHS)3
Correction: Vision-Based Aircraft Marshalling Recognition and UAM Control Command Generation3
Theoretical and Experimental Analysis of the Group Velocity for Lamb Wave on Unidirectional Composite Plates3
Cooperative Guidance for Maneuvering Penetration with Attack Time Consensus and Bounded Input3
The Continuous Thrust Long-Orbit Satellite Pursuit-Evasion Game Control Using Feedback Genetic Shooting Method3
Research on the Process of Dispersing the Bullet by a Large-Size Gasbag with Multiple Inlet Nozzles Based on the Fluid–Structure Interaction Method3
Surrogate Model Based on Data-Driven Model Reduction for Inelastic Behavior of Composite Microstructure3
Improved Conceptual Design of eVTOL Aircraft: Considering Rotor–Rotor Interactional Effects2
Bézier Curves for Smooth Entry into Elliptic Orbits2
Thermal Design Analysis of Low Earth Orbit Optical Telescope ROKITS2
Functional Analysis and Validation of a UAM Integrated Flight Management (UIFM) System2
Vulnerability Analysis of Satellite Under the Impact Hypervelocity Projectile Considering the Formation of Behind-Plate Debris2
Manifold-Based Space Mission Design with Poincaré Filtering Algorithm2
Causality-Seq2Seq Model for Battery Anomaly Detection2
HQP-Based Obstacle Avoidance Motion Planning and Control of On-Orbit Redundant Manipulators2
Flush Air Data System Modeling Using DOE-Based Wind-Tunnel Test2
Integrated Design of Variable Geometry Chin Inlet with Waverider Forebody2
Airfoil Inverse Design Using a Deep Neural Net with an Explainable Attention Mechanism2
Physics-Based Airframe Design Approach Expanded from the Conceptual Design of Coaxial Rotorcraft2
A New Trust-Region Constraint Method for Sequential Convex Programming Framework for Entry Guidance2
Simulations of Hypervelocity Impact Between Space Objects with Various Shapes and Space Lattice Core Sandwich Panel Structures2
Model-based Fault Detection and Identification of a Quadrotor with Rotor Fault2
Reduced-Order Sliding Mode Observer-Based Backstepping Integral Logarithmic Sliding Mode Control: Application to Wing Aeroelastic System2
Design of an Elliptical Orbit Constellation for High-Resolution Optical Observations over a Specific Area2
Investigation of the Characteristic Length Scale and Influencing Factors for Supersonic Gas Jets2
Nonlinear Model Predictive Control of Thermal Vacuum Chamber Temperature2
Comparative Analysis of Improved Aerodynamic Performance: Computational Fluid Dynamics Study of the Trailing Edge Morphing Concept Parameters2
Numerical Prediction of the Impact Fracture of a Projectile Through Oblique Target2
Fundamental Theories of Aeronautics/Mechanical Structures: Past and Present Reddy’s Work, Developments, and Future Scopes2
Key Mechanisms of the Effect of Atomization on Lean Blow-Out Limits of Aero Engines2
Effect of Supply Air Failure on Cabin Pressure Control System of a Fighter Aircraft2
Correction Technique of Inertial Force and Moment in Direct Force Measuring Test of Dynamic Aerodynamic Performance of Airfoils2
Tracking of Maneuvering Extended Object Using High-Resolution Radar Based on Improved Gaussian Processes with Adaptive Contouring2
Optimization of RAIM Based on Dual-Frequency Dual-Constellation INS Integrated Navigation System2
A Novel Engine Fault-Tolerant Control Method Based on Input Scheduling for Tiltrotor Aircraft2
Coarray Fortran Parallel Implementation of a Finite Volume Method-Based Aircraft Ice Accretion Simulation Code2
Influence of Fillers on the Post-buckling Behavior of the Hat-Stiffened Composite Panels2
Numerical Simulation of the Backward Dispensing of a Missile from the Guide Rail Inside the Carrier at Supersonic Flow2
Reentry Risk and Safety Assessment of Spacecraft Debris Based on Machine Learning2
Assessment of the Wave-Shaped Surface of Wingsuit on Aerodynamic Performance2
Design and Co-simulation of an Antiskid Brake System for a Civil Aircraft2
Multi-objective Optimization of Aerodynamic Blade Shapes for Quadcopter System to Enhance Hovering Thrust and Power Consumption Efficiency2
Numerical Study on Tube Shape Influence on Aerodynamic Drag in an Evacuated Tube Transport System2
Review on Flight Control Law Technologies of Fighter Jets for Flying Qualities2
Correction to: Vertiport Performance Analysis for On-Demand Urban Air Mobility Operation in Seoul Metropolitan Area2
Reentry Attitude Fault Tolerant Control for RLV Based on Adaptive Second-Order Nonsingular Fast Terminal Sliding Mode2
Guidance Law for Maneuvering Targets with Impact Time Constraint and Field-of-View Range Analysis2
Selected Papers from the 13th Asian Computational Fluid Dynamics Conference (ACFD 2022) (Jeju, Republic of Korea, Oct. 16th–19th, 2022)2
Nozzle Flow Characterization of the SNU Hypersonic Shock Tunnel2
Ballistic Penetration Test and Simulation of Metallic Aircraft Wing Fuel Tank2
Flight Regimes and Environmental Impact: A Linear Regression Analysis of co2 Emissions for En-Route Air Traffic Operations1
Determination of Acceptable Ranges of Asymmetric Manufacturing Tolerances based on Structural Analysis for a Drone Wing1
Analysis of the Effects of Warm Weather Conditions on Fuel Tank Flammability1
Effects of Cesium Salts on the Electrical Conductivity of the Weakly Ionized Gas in a Hypersonic MHD Channel1
Optimization of Permeability Distribution of Canopy Based on Parachute Performance1
Optimal Policy of Pitch-Hold Phase for Mine Detection of UAV Based on Mixed-Integer Linear Programming1
Correction: Flight Regimes and Environmental Impact: A Linear Regression Analysis of co2 Emissions for En-Route Air Traffic Operations1
Integrated Acoustic Analysis of Payload Fairing Using an FE-SEA Hybrid Method1
Static Mechanical Characteristics Analysis of Aircraft Tire Under Extreme Weather Conditions1
Numerical Study on Ejection and Deployment of Space Net1
Real-Time Prediction Model for Infrared Characteristics of Turbofan Engine1
Reliability Analysis with Proportional Hazard Model in Aeronautics1
Effects of Thermo-chemical Models on Linear Stability Analysis of Chemically Reacting Hypersonic Boundary Layers1
Correction to: Geometric Effects of Liquid Rocket Engine Pintle Injectors in Supercritical Combustion1
Performance Analysis of X-Band Satellite Links Using Receive Combining in a Dual-Contact Scenario1
RETRACTED ARTICLE: Sentinel-2 Cloud Mask Classification Using Deep Learning Method1
Fuzzy Adaptive Compensation Control for Space Manipulator with Joint Flexibility and Dead Zone Based on Neural Network1
An Investigation of Multi-rotor Drone Noise Based on the Acoustic Hemisphere in an Actual Environment1
Prediction of Instantaneous Impact Point of Launch Vehicle, Including Drag Effect1
Structural Safety Evaluation of Test Fixture for Static Load Test of External Fuel Tank for Fixed-Wing Aircraft1
An Investigation of Internal Drag Correction Methodology for Wind Tunnel Test Data in a High-Speed Air-Breathing Vehicle Using Numerical Analysis1
The Application of a Modified Adaptive CS Model in Tracking and Predicting Maneuvering Targets on the Airport Surface1
An Approximate Method for Buckling Analysis and Optimization of Composite Lattice Conical Panels Considering Geometric Parameters1
Active Vibration Suppression of the Wind Tunnel Model Support Structure by Positive Position Feedback Controller with Robust Phase Compensator1
Study on Absorption Characteristics of Electromagnetic Wave in Thin Plasma Slab1
International Civil Aviation Organization (ICAO) Based Noise Exposure Levels at Kuwait International Airport (KIA): Assessment and Mitigation Strategies1
Adaptive Robust Servo LQR Control for Aircraft Under a Wide Range of Icing Conditions1
A Study on Vibration Attenuation of Structure Applied on Eddy Current Damper1
Flight Test Design and Nonlinear Model Identification for Landing Gear Aerodynamics1
Efficient Correlation Method for Satellite Thermal Analysis Model Using Multiple Linear Regression and Optimization Algorithms1
Light-Weight Design of Aerospace Components Using Genetic Algorithm and Dandelion Optimization Algorithm1
A Study on Particle Collisions in Hall Thruster Plasma Using a Hybrid PIC-DSMC Model1
Numerical Analysis of the Thermal Performance of a PCM-Based Heat Sink Under Flight Random Vibration1
Magnus Effect over Aerodynamic Components of Spinning Missile1
Neural Adaptive Sliding Mode Control for Camera Positioner Quadrotor UAV1
A Convex Programming-Based Approach to Trajectory Optimization for Survivability Enhancement of Homing Missiles1
Stability Margin and Structural Coupling Analysis of a Hybrid INDI Control for the Fighter Aircraft1
The Design Improvement of a Rotary-Wing Aircraft Frame Considering Fatigue Life and Fracture Characteristics1
Active Airframe Vibration Control Study Using a Small-Scale Model for Lift-Offset Compound Helicopter1
An Experimental Investigation to Enhance the Aerodynamic Efficiency of Micro Aerial Vehicle Wing Using Bio-inspired Serrations1
Assessment of Drag Prediction Techniques for a Flying Vehicle Based on Radar-Tracked Data1
Linkage Learning Optimization of Aeroelastic and Structural Behavior of Composite Wings1
Numerical Investigation of a Ballistic Range Free Flight Model1
A Dynamic Power Consumption Estimation Method of Electro-mechanical Actuator for UAV Modeling and Simulation1
Multi-agent Reinforcement Learning with Attention Mechanism for Collaborative Management of Airspace Users in the Pre-flight Phase1
Numerical and Experimental Analysis of Three-Dimensional Boundary-Layer Transition Induced by Isolated Cylindrical Roughness Elements1
Fine Pointing and Tracking Onboard System for CubeSat Optical Satcom1
Multi-disciplinary and Multi-objective Design Optimization of a Lunar Rover System with Operational Considerations1
Comparative Analysis of Inerting Effects of Open and Closed Vent Systems Fuel Tanks1
Selected Papers from the 12th Asia–Pacific International Symposium on Aerospace Technology (APISAT 2021) (Jeju, Republic of Korea, Nov. 15th–17th, 2021)1
Event-Triggered Adaptive Fixed-Time Trajectory Tracking Control for Stratospheric Airship1
Cooperative Global Path Planning for Multiple Unmanned Aerial Vehicles Based on Improved Fireworks Algorithm Using Differential Evolution Operation1
Study on the Relationship Between Migration of Desensitizer and Combustion Performance of a Double-Base Propellant1
Investigation on Lunar Landing Candidate Sites for a Future Lunar Exploration Mission1
CFD Analysis of a Missile Nozzle Performance for Three Different Fuels Under Non-premix and Partially Premix Condition1
Experimental Study on the Wing Parameter Optimization of Flapping-Wing Aircraft Based on the Clap-and-Fling Mechanism1
Performance Design of a Turbofan Engine Using Multi-objective Particle Swarm Optimization (MOPSO)1
Super-resolution Reconstruction of Transitional Boundary Layers Using a Deep Neural Network1
Numerical Investigations on the Influence of Ramp Locations in a Strut Injection Scramjet Combustor1
An Angular Discretization Method Using Repulsive Particles for the Three-Dimensional Radiative Transfer Equation1
Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System1
Second-Order Sliding Mode Guidance Law of a Nonsingular Fast Terminal with a Terminal Angular Constraint1
Aerodynamic Characteristics and Flow Structure of Hawkmoth-Like Wing with LE Vein1
Routing Prediction Strategy for UAV Swarm Network Using Pigeon-Inspired Optimization-Based Neural Network1
Review of More Electric Engines for Civil Aircraft1
Multi-Matching-Based Vision Navigation Referencing Map Tile1
Derivation of Buckling Knockdown Factors for Pressurized Orthogrid-Stiffened Cylinders of Launch Vehicle Structures1
Design and Verification of Electric Pump for Small LOX/Methane Rocket Engine1
A Probabilistic Approach for Three-Dimensional Variation Analysis in Aero-engine Rotors Assembly1
Study on the Influence of Flight Altitude on the Rocket Plume Radiation Enhancement Effect Caused by Afterburning1
Characterization of Spacecraft Tank Sloshing Based on a Smooth Particle Hydrodynamics Approach1
Prediction of Airfoil Lift Coefficient Based on Multilayer Perceptron1
Monocular SLAM with Point and Line Features Applied to Spacecraft Relative Navigation1
Third-Party Risk Assessment on the Ground for Urban Air Mobility Operations: A Case Study of Seoul Metropolitan City1
Supersonic MLN Thrust Correction at HT with Application to The Missile Trajectory1
Improved Modeling Method for 3-Dimensional Woven Composites Using Weaving Parameters1
Experimental and Numerical Investigation on Attitude Adjustment Characteristics of Spacecraft with Impulse Thruster1
Numerical Prediction of Failure Load of Scarf-Patch-Repaired CFRP Composite Using Damage Zone Model and Cohesive Zone Model1
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