International Journal of Aerospace Engineering

Papers
(The TQCC of International Journal of Aerospace Engineering 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 2022-06-01 to 2026-06-01.)
ArticleCitations
A Moving Target Online Location Algorithm Based on Factor Graph57
A Novel Nonlinear Quadrotor Attitude Regulation with Disturbances and Preassigned Convergences27
Flight Endurance Increasing Technology of New Energy UAV Based on a Strut-Braced Wing27
S2 Stream Surface Approximation Approach for Quasi Three-Dimensional Turbine Time-Marching Design Method26
Path Planning of Unmanned Helicopter in Complex Environment Based on Heuristic Deep Q-Network23
Self-Organizing Method on Mission-Level Task Allocation of Large-Scale Remote Sensing Satellite Swarm15
Quantitative Assessment of Human Factors in Civil Aircraft Flight Test Risks Based on Fuzzy Bayesian Network and Improved HFACS Model15
Heat Transfer Analysis and Structural Optimization for Spiral Channel Regenerative Cooling Thrust Chamber14
Active Flow Control of Helicopter Rotor Based on Coflow Jet14
Design of Reinforcement Learning Guidance Law for Antitorpedo Torpedoes13
Deployment Strategy and Dynamic Analysis of Large Ring Truss Antenna13
Dynamic Property Analysis of Electrically Controlled Solid Propellant13
Numerical Analysis of Ramp Angle Effects on Shock Wave Compressor Performance for Carbon Dioxide Compression12
Numerical Analysis of Free Play-Induced Aeroelastic Phenomena: A Numerical Approach With Adaptive Step Size Control12
The Computation of Quasiterminator Orbits in Asteroid Exploration Based on the Quasi‐Newton Method12
CFD Model of Turboprop Engine Nacelle Airflow for Ground Idle Condition11
A Novel Strategy for Hypersonic Vehicle With Complex Distributed No-Fly Zone Constraints11
Computational Optimal Impact Angle Control Guidance Laws Weighted by Arbitrary Functions10
Dynamic Characteristics Analysis of 3D Blade Tip Clearance for Turbine Blades with Typical Cracks10
A Fault Diagnosis Method for Avionics Equipment Based on SMOTEWB‐LGBM10
A Strong Maneuvering Target-Tracking Filtering Based on Intelligent Algorithm9
Nonlinear Predictive Control with Sliding Mode for Hypersonic Vehicle9
Experimental and Theoretical Study of Internal Pressure Loads on Boundary Walls under Gusty Wind Conditions9
Simplified Mixing Rules for Calculating Transport Coefficients of High-Temperature Air9
A New Unsteady Flow Control Technology of Centrifugal Compressor Based on Negative Circulation Concept8
Topometry Optimization of Energy Absorbing Structure through Targeting Force-Displacement Method considering Tailor Rolled Blank Process8
Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework8
Research on Autodocking Control Technology of the Propellant Umbilical Connector of Launch Vehicles8
An Improved Feedforward-Robust Algorithm for Active Vibration Control of Helicopter Maneuver Flight8
Active Control of Aerial Refueling Hose-Drogue Dynamics with the Improved Reel Take-Up System8
Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion8
A Dual-Hierarchy Synchronization Method for Signal Preambles with High Detection Rates for Satellite-Based ADS-B Receivers with Different Sensitivities8
Multiscale Feature Fusion Attention Lightweight Facial Expression Recognition8
Safety Assessment of Critical Aircraft Systems Under Multisource Uncertainty Based on Evidence Network7
Review of Root-Mean-Square Error Calculation Methods for Large Deployable Mesh Reflectors7
Query‐Based Preference Optimization for Aircraft Design: A Comparative Study of Utility‐Driven and Human‐in‐the‐Loop Approaches7
Networking Method for the Structure of a Large Modular Deployable Space Antenna7
Fill-In and Boiling Transition Characteristics during the Liquid Oxygen Chill-Down Process in a Vertical Exit-Contracted Pipe7
Formation Consensus Control Method With Time‐Varying Parameters Based on Virtual Leader7
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay7
Hierarchical Sliding‐Mode Formation Control of Quadcopters Based on Adaptive Event‐Triggered Mechanism7
Multi-UAV DMPC Cooperative Guidance with Constraints of Terminal Angle and Obstacle Avoidance7
Robust Centroid Estimation Method with the Rough and Refined Estimation for Interplanetary Optical Navigation7
Two-Loop Acceleration Autopilot Design and Analysis Based on TD3 Strategy7
L1 Adaptive Fault‐Tolerant Attitude Tracking Control of UAV Systems Subject to Faults and Input Saturation6
Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration6
Sensitivity and Consistency Analysis of BDS-3 GEO Satellite Orbit Maneuver Detection6
Aerodynamic Parameter Identification of Projectile Based on Improved Extreme Learning Machine and Ensemble Learning Theory6
Short‐Term Target Maneuvering Trajectory Prediction Using DTW–CNN–LSTM6
Predicting Flight Delays with Machine Learning: A Case Study from Saudi Arabian Airlines6
Thermal-Structural Analysis of the Support Structure for a Modular Space Deployable Antenna6
Aerodynamic Performance Comparisons of Two Kinds of Variable Nozzle Vanes for a Variable Geometry Turbine6
Adaptive Super-Twisting Cooperative Guidance Law with Fixed-Time Convergence6
Design of Adaptive Super‐Twisting Cooperative Guidance Law for Intercepting Highly Maneuvering Target6
Aircraft Trajectory Prediction Based on Bayesian Optimised Temporal Convolutional Network–Bidirectional Gated Recurrent Unit Hybrid Neural Network6
An Intelligent Trajectory Prediction Algorithm for Reentry Glide Vehicles Based on Physics‐Informed Constraints and Prediction Error Compensation6
Adaptive Distributed Fixed-Time Cooperative Three-Dimensional Guidance Law for Multimissiles against Manoeuvring Target6
Modeling and Invulnerability Analysis of Multilayer Air Traffic Network considering Altitude Layer6
Analysis of Thrust Vectoring Control for Aerospike Nozzle6
Closed-Loop Fault Diagnosis of SDR Using Gap Metric, PCA, and Kalman’s Principle5
An Exoatmospheric Homing Guidance Law Based on Deep Q Network5
Reconfiguration Control and Cost Analysis of UAV Cluster5
Vision‐Based Aircraft Localization During the End Stage of Landing Approach via Runway Mark Determination5
Effect of Aeroelastic Tailoring Design on Wing Mode5
High Precision Height Control for Wing-in-Ground Crafts5
A Novel Active Vibration Control Method for Helicopter Fuselages Based on Diffusion Cooperation5
Research on Three-Dimensional Integrated Guidance and Control Design with Multiple Constraints5
Visual Explainable Convolutional Neural Network for Aerodynamic Coefficient Prediction5
Aviation Rivet Classification and Anomaly Detection Based on Deep Learning5
Active Pointing Compensation of a HTS Multibeam Antenna5
Observer-Based Robust Finite-Time Trajectory Tracking Control for a Stratospheric Satellite Subject to External Disturbance and Actuator Saturation5
Detectable Inspection: Propeller Nick Detection Model Development Using YOLOv85
Identification of Key Factors and Mining of Association Relations in Complex Product Assembly Process5
Ontology-Based Resource Modeling and Matching Framework in Avionics Systems5
Application of Stewart Platform in the Low-Frequency Vibration Characteristic Test of Space Truss Deployable Antenna on Satellite5
A Finite‐Time Fractional‐Order Error Extended State Observer for Hypersonic Vehicle4
Prediction of Orbit Decay for Large-Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects4
Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration4
Improved F-RRT 4
Deployment Impact Experiment and Dynamic Analysis of Modular Truss Antenna4
A Modified Robust Adaptive Fault Compensation Design for Spacecraft with Guaranteed Transient Performance4
Autonomous Antidisturbance Flight Control of Tilt‐Rotor UAV in Complex Environment of Ultralow Altitude4
A Guidance Method for Impact Time and Angle Control Based on Trajectory Tracking4
Variable Structure Control and Its Ground Experimental Test for the Space Station Robot4
Design of Corrugated Airfoil for a Flapping Wing Micro Air Vehicle4
An Efficient Trajectory Negotiation and Verification Method Based on Spatiotemporal Pattern Mining4
Multiloitering Munition Cooperative Surrounding and Attack Method Based on Wolf Pack Algorithm4
Automatic Landing System Design for Unmanned Fixed-Wing Vehicles via Multivariable Active Disturbance Rejection Control4
An Intelligent Trajectory Prediction Algorithm for Hypersonic Glide Targets Based on Maneuver Mode Identification4
Influence of Different Altitudes on the Solid Rocket Contrail Formation in the Near Field4
Fatigue Reliability Analysis System for Key Components of Aero-Engine4
Multimissile Cooperative Guidance Law for Maneuvering Target Interception Based on the ICOA4
Fast Trajectory Generation Method for Midcourse Guidance Based on Convex Optimization4
Fault-Tolerant Control of Hypersonic Vehicle Using Neural Network and Sliding Mode4
Effect of Cooling Header on the Hydrocarbon Fuel Flow Distribution in a Regenerative Cooling Channel4
Dynamic Modelling and Continuous Trajectory Tracking Control of Space Robots Based on Lie Group SE(3)4
A Decision-Making Method for Distributed Unmanned Aerial Vehicle Swarm considering Attack Constraints in the Cooperative Strike Phase4
Multi-UAV Cooperative Air Combat Target Assignment Method Based on VNS-IBPSO in Complex Dynamic Environment4
Effects of Flow Coefficient on Turbine Aerodynamic Performance and Loss Characteristics4
Air-Ground Task Collaboration Safety Analysis Based on Real-Valued Differential Biclustering for Midterm Conflict in Single-Pilot Operations of Commercial Aircraft4
Reduction of the Influence of Interfering Signals on the Longitudinal Control of UAVs with Fixed Wing4
Investigation of the Effect of Axial Gap on the Mechanical Response of a Cartridge-Loaded CMDB Propellant Grain under Vibration Loads4
Influence of Geometric Parameters on Intake Performance of 3D Ramp‐Type Scramjet Inlet4
A Midcourse Guidance Method Combined with Trajectory Prediction for Antinear-Space-Gliding Vehicles4
Experimental Investigation on Flame Chemiluminescence and Flow Characteristics of a Reverse-Flow Combustor4
Prediction of the Flight Dynamics of Maneuvering Multirotor Aircraft4
Effects of Geometry of Plenum Chamber on Losses in the Bleed System of an Axial Compressor4
A Passive Vibration Control Method of Modular Space Structures Based on Band Gap Optimization4
Nonlinear Dynamic Responses of a Rotor-Bearing System with Eccentric Squeeze Film Dampers4
Separation Control for a Transonic Convex Corner Flow Using Ramp-Type Vortex Generators4
Continuous Gesture Sequences Recognition Based on Few-Shot Learning4
Commonality Benefit Analysis for Maintenance Technical Publications of Civil Aircraft Based on Learning Effect4
Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa4
A Novel Microscopic Modeling Scheme for the Shape Memory Polymer Composites with respect to the Ambient Temperature3
Coupling an Autonomous UAV With a ML Framework for Sustainable Environmental Monitoring and Remote Sensing3
Numerical Study on Effects of Arrayed Pulsed Energy Depositions on a Supersonic Combustor3
A Weight-Generating Approach of a Deep Neural Network for the Parameter Identification of Dynamic Systems3
Analysis of Single-Pilot Intention Modeling in Commercial Aviation3
On an Autonomous Pulsar Observation–Based Timekeeping Method for Deep Space3
Predetermined Performance Control of Spacecraft Formation Based on SE(3) Error Description3
A Condition Monitoring Method of Hydraulic Gear Pumps Based on Multilevel Mechanism-Data Fusion3
Nonuniform Leakage Characteristics of Straight‐Through Labyrinth Seal Under Large Driving Pressure Ratio3
Analysis of Structural Characteristics of the HALE Joined‐Wing Configuration UAV3
Nonharmonic Control of the Blade-Vortex Interaction Noise of Electrically Controlled Rotor3
Numerical and Experimental Verification of Spherically Layered Ice Model for Analysis on Hail Impacting Aviation Structures3
Finite Element Analysis to Investigate the Effects of Split Sleeve Cold Expansion Process Variables on Residual Stress Distribution and Pulling Force Progression for Al 2024‐T351 Alloy3
Computational Technique for Crack Propagation Simulation in Viscoelastic Solid Propellant3
External Excitation Effects on Combustion Instability in Dual‐Burn‐Rate Solid Rocket Motors With a Large Aspect Ratio3
Three‐Dimensional Trajectory Tracking Control for Stratospheric Airship Based on Deep Reinforcement Learning3
Three-Dimensional Guidance Approach with Obstacle Avoidance against Maneuvering Targets3
UAV Detect and Avoid from UTM-Dependent Surveillance3
An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode3
Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode3
A Spatial Clustering and Matching Game–Based Multihop Routing Algorithm for Heterogeneous UAVs3
Experimental Investigation on Flow Characteristics of a Reverse-Flow Combustor3
A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor3
Conflict Resolution Strategy Based on Flight Conflict Network Optimal Dominating Set3
Fault-Tolerant Control for Carrier-Based Aircraft Automatic Landing Subject to Multiple Disturbances and Actuator Faults3
Design and Implementation of a Tube Heat Exchanger for Turbojet Engines to Improve Operational Efficiency3
Numerical Simulation of Ice Crystal Supercooled Droplet Mixed Phase Icing Based on the Improved Messinger Model3
The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method3
Velocity-Adaptive Prescribed Performance Control for Carrier-Based Aircraft Based on Guardian Maps3
Research on SiC Speed Controller for High‐Voltage Distributed Electric Propulsion System3
Shape Adjustment of a Large Planar Phased Array Antenna With Nonlinear Cable Actuators3
Design and Reachable Domain Analysis of On‐orbit Electromagnetic Launcher for CubeSats3
The Numerical Simulation Method of the Slot Crack Groups’ Effect Analysis for Solid Rocket Motor Grain3
A Two-Level Iterative Node Importance Evaluation of Aircraft Function Modules Based on Influence Matrix3
A New Theoretical Method for Solving Forward Kinematics of the Parallel Mechanisms Based on Transfer Matrix3
Experimental Study on the Aerodynamic Characteristics of Blades at the Last Stage of a Steam Turbine at Off-Design Conditions3
3-DOF Position and Orientation Control of an Air Flotation Platform for Spacecraft Ground Microgravity Simulation by Using Double Closed-Loop Cascade PIDnn3
Control of High‐Load Compressor Stator Corner Flow by Blade Slotting3
Research on Forecasting of the Compressor Geometric Variable System Based on the MAE Model3
Eye Gaze Estimation Based on Stacked Hourglass Neural Network for Aircraft Helmet Aiming3
Detection of Aerial Vehicles Using Satellite Imagery: Comparative Analysis of U‐Net Segmentation Model and YOLO Object Detection Model3
General Modeling for Space Robot Proximity Relative Motion by Using Dual Operator With Hybrid Coordinates3
Fuel‐Saving Postcapture Detumbling by Dual‐Arm Space Robot3
Multiobjective Optimization Design of Truss Antenna3
Numerically Predicted Buckling Design Criteria for Elliptical Common Bulkhead Structures3
Automatic Task Planning and Its On-Orbit Verification of Agile Remote Sensing Satellite3
Model of Multi-Algorithmic-Based Optimization of 4D Approach Trajectory under Thunderstorm Weather3
Integrated Navigation Method of Aerospace Vehicle Based on Rank Statistics3
Height Control of Supersonic Sea‐Skimming Missiles Based on Online Parameter Identification3
Landing Reliability Assessment of Airdrop System Based on Vine-Bayesian Network3
Multiobjective Optimization of Stress-Release Boot of Solid Rocket Motor under Vertical Storage Based on RBF Model3
Nondisturbance Load Maglev Satellite Attitude Pointing Control via Path Planning3
ACP-Based Space Systems: Design, Development, and Operation3
Autonomous Landing of a Fixed‐Wing UAV With RTK GNSS and MEMS IMU3
A Pulsar Vector Observation-Based Link Acquisition Method for X-Ray Communications3
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