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 2021-05-01 to 2025-05-01.)
ArticleCitations
S2 Stream Surface Approximation Approach for Quasi Three-Dimensional Turbine Time-Marching Design Method61
Satellite In-Orbit Secondary Collision Risk Assessment43
Low-Orbit Large-Scale Communication Satellite Constellation Configuration Performance Assessment30
Passive Sonar Multiple-Target Tracking with Nonlinear Doppler and Bearing Measurements Using Multiple Sensors24
Deployment Strategy and Dynamic Analysis of Large Ring Truss Antenna19
Path Planning of Unmanned Helicopter in Complex Environment Based on Heuristic Deep Q-Network17
Active Flow Control of Helicopter Rotor Based on Coflow Jet16
A Novel Nonlinear Quadrotor Attitude Regulation with Disturbances and Preassigned Convergences14
A Moving Target Online Location Algorithm Based on Factor Graph14
Structural Feature-Preserving Point Cloud Denoising Method for Aero-Engine Profile13
CFD Model of Turboprop Engine Nacelle Airflow for Ground Idle Condition12
Flight Endurance Increasing Technology of New Energy UAV Based on a Strut-Braced Wing12
Heat Transfer Analysis and Structural Optimization for Spiral Channel Regenerative Cooling Thrust Chamber12
Self-Organizing Method on Mission-Level Task Allocation of Large-Scale Remote Sensing Satellite Swarm12
Experimental and Theoretical Study of Internal Pressure Loads on Boundary Walls under Gusty Wind Conditions11
A Fault Diagnosis Method for Avionics Equipment Based on SMOTEWB‐LGBM11
Nonlinear Predictive Control with Sliding Mode for Hypersonic Vehicle11
Simplified Mixing Rules for Calculating Transport Coefficients of High-Temperature Air9
Estimation-Based and Dropout-Dependent Control Design for Aeroengine Distributed Control System with Packet Dropout9
Numerical Analysis of Free Play-Induced Aeroelastic Phenomena: A Numerical Approach With Adaptive Step Size Control9
Dynamic Characteristics Analysis of 3D Blade Tip Clearance for Turbine Blades with Typical Cracks9
Numerical Study on Rod Thrust Vector Control for Physical Applications9
Computational Optimal Impact Angle Control Guidance Laws Weighted by Arbitrary Functions9
Multiple Spacecraft Formation Flying Control around Artificial Equilibrium Point Using Propellantless Approach9
Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event9
A Novel Strategy for Hypersonic Vehicle With Complex Distributed No-Fly Zone Constraints8
Active Control of Aerial Refueling Hose-Drogue Dynamics with the Improved Reel Take-Up System8
Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System8
Trajectory Optimization of Hypersonic Periodic Cruise Using an Improved PSO Algorithm8
A Strong Maneuvering Target-Tracking Filtering Based on Intelligent Algorithm8
Fill-In and Boiling Transition Characteristics during the Liquid Oxygen Chill-Down Process in a Vertical Exit-Contracted Pipe8
A New Unsteady Flow Control Technology of Centrifugal Compressor Based on Negative Circulation Concept7
Topometry Optimization of Energy Absorbing Structure through Targeting Force-Displacement Method considering Tailor Rolled Blank Process7
Multiscale Feature Fusion Attention Lightweight Facial Expression Recognition7
Networking Method for the Structure of a Large Modular Deployable Space Antenna7
Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework7
A UAV Pursuit-Evasion Strategy Based on DDPG and Imitation Learning7
Multi-UAV DMPC Cooperative Guidance with Constraints of Terminal Angle and Obstacle Avoidance7
An Improved Feedforward-Robust Algorithm for Active Vibration Control of Helicopter Maneuver Flight7
Research on Autodocking Control Technology of the Propellant Umbilical Connector of Launch Vehicles7
Review of Root-Mean-Square Error Calculation Methods for Large Deployable Mesh Reflectors7
Robust Crater Detection Algorithm Based on Maximum Entropy Threshold Segmentation7
Influence of Three-Body Gravitational Perturbation for Drag-Free Spacecraft6
Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion6
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay6
An Efficient Dynamic Modeling Technique for a Central Tie Rod Rotor6
Transportation of Payload Using Multiple Quadrotors via Rigid Connection6
Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet6
A Dual-Hierarchy Synchronization Method for Signal Preambles with High Detection Rates for Satellite-Based ADS-B Receivers with Different Sensitivities6
Calculation of the Influence Zone for Planetary Sampling Based on DEM Simulation6
Thermal-Structural Analysis of the Support Structure for a Modular Space Deployable Antenna6
Model Predictive Control for Automatic Carrier Landing with Time Delay5
Aerodynamic Parameter Identification of Projectile Based on Improved Extreme Learning Machine and Ensemble Learning Theory5
Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration5
Sensitivity and Consistency Analysis of BDS-3 GEO Satellite Orbit Maneuver Detection5
Short‐Term Target Maneuvering Trajectory Prediction Using DTW–CNN–LSTM5
Engineering Application of an Identification Method to Shock-Induced Vortex Stability in the Transonic Axial Fan Rotor5
Aircraft Trajectory Prediction Based on Bayesian Optimised Temporal Convolutional Network–Bidirectional Gated Recurrent Unit Hybrid Neural Network5
Adaptive Trajectory Tracking Control for Rotorcraft Using Incremental Backstepping Sliding Mode Control Strategy5
Adaptive Super-Twisting Cooperative Guidance Law with Fixed-Time Convergence5
Modeling and Invulnerability Analysis of Multilayer Air Traffic Network considering Altitude Layer5
Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure5
Two-Loop Acceleration Autopilot Design and Analysis Based on TD3 Strategy5
L1 Adaptive Fault‐Tolerant Attitude Tracking Control of UAV Systems Subject to Faults and Input Saturation5
Predicting Flight Delays with Machine Learning: A Case Study from Saudi Arabian Airlines5
Spacecraft Intelligent Fault Diagnosis under Variable Working Conditions via Wasserstein Distance-Based Deep Adversarial Transfer Learning5
Research on Three-Dimensional Integrated Guidance and Control Design with Multiple Constraints5
Aerodynamic Performance Comparisons of Two Kinds of Variable Nozzle Vanes for a Variable Geometry Turbine5
Robust Centroid Estimation Method with the Rough and Refined Estimation for Interplanetary Optical Navigation5
Aviation Rivet Classification and Anomaly Detection Based on Deep Learning4
Ontology-Based Resource Modeling and Matching Framework in Avionics Systems4
Evaluation of Ion Beam Behavior in 50 W Class RF Ion Thruster4
Closed-Loop Fault Diagnosis of SDR Using Gap Metric, PCA, and Kalman’s Principle4
Cell Area-Based Method for Analyzing the Coverage Capacity of Satellite Constellations4
Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine4
Free Vibration of Annular Circular Plates Based on Higher-Order Shear Deformation Theory: A Spline Approximation Technique4
Observer-Based Robust Finite-Time Trajectory Tracking Control for a Stratospheric Satellite Subject to External Disturbance and Actuator Saturation4
Application of Stewart Platform in the Low-Frequency Vibration Characteristic Test of Space Truss Deployable Antenna on Satellite4
Lightweight Design of Solar UAV Wing Structures Based on Sandwich Equivalent Theory4
Dynamic Drag Reduction Effects of Aerospikes and Aerodisks4
A User-Priority-Driven Multi-UAV Cooperative Reconnaissance Strategy4
Visual Explainable Convolutional Neural Network for Aerodynamic Coefficient Prediction4
Evolutionary Optimization of Multirendezvous Impulsive Trajectories4
Application of the Improved Grey Wolf Algorithm in Spacecraft Maneuvering Path Planning4
A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage4
Active Pointing Compensation of a HTS Multibeam Antenna4
A Novel Active Vibration Control Method for Helicopter Fuselages Based on Diffusion Cooperation4
Identification of Key Factors and Mining of Association Relations in Complex Product Assembly Process4
Adaptive Distributed Fixed-Time Cooperative Three-Dimensional Guidance Law for Multimissiles against Manoeuvring Target4
Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm4
Numerical Study on Combustion and Atomization Characteristics of Coaxial Injectors for LOX/Methane Engine4
Sizing and Mission Profile Analysis of the Hybrid-Electric Propulsion System for Retrofitting a Fixed Wing VTOL Aircraft4
Deployment Impact Experiment and Dynamic Analysis of Modular Truss Antenna4
An Exoatmospheric Homing Guidance Law Based on Deep Q Network4
Research on Aluminum Honeycomb Buffer Device for Soft Landing on the Lunar Surface4
Effect of Aeroelastic Tailoring Design on Wing Mode4
High Precision Height Control for Wing-in-Ground Crafts4
Experimental Investigation on Flame Chemiluminescence and Flow Characteristics of a Reverse-Flow Combustor4
Finite Element Simulations of Dynamic Shear Fracture of Hollow Shear Pins4
Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions4
A Deep Learning Anomaly Detection Framework for Satellite Telemetry with Fake Anomalies4
Integrated Optimization of Pipe Routing and Clamp Layout for Aeroengine Using Improved MOALO3
Numerical Simulation of Ice Crystal Supercooled Droplet Mixed Phase Icing Based on the Improved Messinger Model3
Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa3
Effect of Cooling Header on the Hydrocarbon Fuel Flow Distribution in a Regenerative Cooling Channel3
Experimental and Numerical Investigations on the Ignition of RBCC Gas-Oxygen/Kerosene Rocket Ejector3
Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy3
A Modified Robust Adaptive Fault Compensation Design for Spacecraft with Guaranteed Transient Performance3
Investigation on Viscoelastic Poisson’s Ratio of Composite Materials considering the Effects of Dewetting3
Investigation of the Effect of Axial Gap on the Mechanical Response of a Cartridge-Loaded CMDB Propellant Grain under Vibration Loads3
Effects of Flow Coefficient on Turbine Aerodynamic Performance and Loss Characteristics3
Influence of Different Altitudes on the Solid Rocket Contrail Formation in the Near Field3
Multi-UAV Cooperative Air Combat Target Assignment Method Based on VNS-IBPSO in Complex Dynamic Environment3
Fatigue Reliability Analysis System for Key Components of Aero-Engine3
Influence of Propeller Slipstream on the Flow Field of S-Shaped Intake3
UAV Detect and Avoid from UTM-Dependent Surveillance3
Variable Structure Control and Its Ground Experimental Test for the Space Station Robot3
Nonlinear Dynamic Responses of a Rotor-Bearing System with Eccentric Squeeze Film Dampers3
A New Theoretical Method for Solving Forward Kinematics of the Parallel Mechanisms Based on Transfer Matrix3
An Intelligent Trajectory Prediction Algorithm for Hypersonic Glide Targets Based on Maneuver Mode Identification3
Integrated Navigation Method of Aerospace Vehicle Based on Rank Statistics3
Two-Stage Degradation Assessment and Prediction Method for Aircraft Engine Based on Data Fusion3
Design of Corrugated Airfoil for a Flapping Wing Micro Air Vehicle3
Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration3
A Decision-Making Method for Distributed Unmanned Aerial Vehicle Swarm considering Attack Constraints in the Cooperative Strike Phase3
Improved F-RRT 3
Research on Flow Characteristics of a Variable Mach Number Aerodynamic Test Device by a Rotating Profile3
Influence of Geometric Parameters on Intake Performance of 3D Ramp‐Type Scramjet Inlet3
Robust Integrated Guidance and Control Design for Angle Penetration Attack of Multimissiles3
Application of Principal Component Analysis-Assisted Neural Networks for the Rotor Blade Load Prediction3
Commonality Benefit Analysis for Maintenance Technical Publications of Civil Aircraft Based on Learning Effect3
Fast Trajectory Generation Method for Midcourse Guidance Based on Convex Optimization3
Prediction of Orbit Decay for Large-Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects3
Investigation on the Horizontal Landing Velocity and Pitch Angle Impact on the Soft-Landing Dynamic Characteristics3
Global Sensitivity Analysis of Earth-Moon Transfer Orbit Parameters Based on Sobol Method3
Reduction of the Influence of Interfering Signals on the Longitudinal Control of UAVs with Fixed Wing3
High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument3
Fault-Tolerant Control of Hypersonic Vehicle Using Neural Network and Sliding Mode3
Landing Reliability Assessment of Airdrop System Based on Vine-Bayesian Network3
A Midcourse Guidance Method Combined with Trajectory Prediction for Antinear-Space-Gliding Vehicles3
Air-Ground Task Collaboration Safety Analysis Based on Real-Valued Differential Biclustering for Midterm Conflict in Single-Pilot Operations of Commercial Aircraft3
Automatic Landing System Design for Unmanned Fixed-Wing Vehicles via Multivariable Active Disturbance Rejection Control3
A Passive Vibration Control Method of Modular Space Structures Based on Band Gap Optimization3
Effects of Geometry of Plenum Chamber on Losses in the Bleed System of an Axial Compressor3
Continuous Gesture Sequences Recognition Based on Few-Shot Learning3
A Robust Adaptive Control Algorithm for Multimissile Cooperative Formation3
An Efficient Trajectory Negotiation and Verification Method Based on Spatiotemporal Pattern Mining3
A Finite‐Time Fractional‐Order Error Extended State Observer for Hypersonic Vehicle3
Target Tactical Intention Recognition in Multiaircraft Cooperative Air Combat3
Prediction of the Flight Dynamics of Maneuvering Multirotor Aircraft3
Multiobjective Optimization of Turbine Coolant Collection/Distribution Plenum Based on the Surrogate Model3
Separation Control for a Transonic Convex Corner Flow Using Ramp-Type Vortex Generators3
Backstepping Control Based on Constrained Command Filter for Hypersonic Flight Vehicles with AOA and Actuator Constraints3
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