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 2021-06-01 to 2025-06-01.)
ArticleCitations
Passive Sonar Multiple-Target Tracking with Nonlinear Doppler and Bearing Measurements Using Multiple Sensors64
Deployment Strategy and Dynamic Analysis of Large Ring Truss Antenna43
Path Planning of Unmanned Helicopter in Complex Environment Based on Heuristic Deep Q-Network32
Active Flow Control of Helicopter Rotor Based on Coflow Jet25
A Moving Target Online Location Algorithm Based on Factor Graph20
Low-Orbit Large-Scale Communication Satellite Constellation Configuration Performance Assessment17
A Novel Nonlinear Quadrotor Attitude Regulation with Disturbances and Preassigned Convergences17
S2 Stream Surface Approximation Approach for Quasi Three-Dimensional Turbine Time-Marching Design Method15
Satellite In-Orbit Secondary Collision Risk Assessment14
Flight Endurance Increasing Technology of New Energy UAV Based on a Strut-Braced Wing14
Structural Feature-Preserving Point Cloud Denoising Method for Aero-Engine Profile14
Self-Organizing Method on Mission-Level Task Allocation of Large-Scale Remote Sensing Satellite Swarm12
Heat Transfer Analysis and Structural Optimization for Spiral Channel Regenerative Cooling Thrust Chamber12
Nonlinear Predictive Control with Sliding Mode for Hypersonic Vehicle12
Estimation-Based and Dropout-Dependent Control Design for Aeroengine Distributed Control System with Packet Dropout10
Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event10
Computational Optimal Impact Angle Control Guidance Laws Weighted by Arbitrary Functions9
Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System9
Multiple Spacecraft Formation Flying Control around Artificial Equilibrium Point Using Propellantless Approach9
A Strong Maneuvering Target-Tracking Filtering Based on Intelligent Algorithm9
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
Dynamic Characteristics Analysis of 3D Blade Tip Clearance for Turbine Blades with Typical Cracks9
A Novel Strategy for Hypersonic Vehicle With Complex Distributed No-Fly Zone Constraints9
A Fault Diagnosis Method for Avionics Equipment Based on SMOTEWB‐LGBM8
Numerical Analysis of Free Play-Induced Aeroelastic Phenomena: A Numerical Approach With Adaptive Step Size Control8
CFD Model of Turboprop Engine Nacelle Airflow for Ground Idle Condition8
Numerical Study on Rod Thrust Vector Control for Physical Applications8
Trajectory Optimization of Hypersonic Periodic Cruise Using an Improved PSO Algorithm8
Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework7
A Dual-Hierarchy Synchronization Method for Signal Preambles with High Detection Rates for Satellite-Based ADS-B Receivers with Different Sensitivities7
Topometry Optimization of Energy Absorbing Structure through Targeting Force-Displacement Method considering Tailor Rolled Blank Process7
Networking Method for the Structure of a Large Modular Deployable Space Antenna7
Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion7
Multi-UAV DMPC Cooperative Guidance with Constraints of Terminal Angle and Obstacle Avoidance7
A UAV Pursuit-Evasion Strategy Based on DDPG and Imitation Learning7
A New Unsteady Flow Control Technology of Centrifugal Compressor Based on Negative Circulation Concept7
Fill-In and Boiling Transition Characteristics during the Liquid Oxygen Chill-Down Process in a Vertical Exit-Contracted Pipe7
Multiscale Feature Fusion Attention Lightweight Facial Expression Recognition7
Research on Autodocking Control Technology of the Propellant Umbilical Connector of Launch Vehicles7
Robust Crater Detection Algorithm Based on Maximum Entropy Threshold Segmentation7
Active Control of Aerial Refueling Hose-Drogue Dynamics with the Improved Reel Take-Up System6
An Efficient Dynamic Modeling Technique for a Central Tie Rod Rotor6
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay6
Thermal-Structural Analysis of the Support Structure for a Modular Space Deployable Antenna6
An Improved Feedforward-Robust Algorithm for Active Vibration Control of Helicopter Maneuver Flight6
Transportation of Payload Using Multiple Quadrotors via Rigid Connection6
Predicting Flight Delays with Machine Learning: A Case Study from Saudi Arabian Airlines6
Review of Root-Mean-Square Error Calculation Methods for Large Deployable Mesh Reflectors6
Two-Loop Acceleration Autopilot Design and Analysis Based on TD3 Strategy6
Model Predictive Control for Automatic Carrier Landing with Time Delay6
Aircraft Trajectory Prediction Based on Bayesian Optimised Temporal Convolutional Network–Bidirectional Gated Recurrent Unit Hybrid Neural Network5
Modeling and Invulnerability Analysis of Multilayer Air Traffic Network considering Altitude Layer5
A User-Priority-Driven Multi-UAV Cooperative Reconnaissance Strategy5
Spacecraft Intelligent Fault Diagnosis under Variable Working Conditions via Wasserstein Distance-Based Deep Adversarial Transfer Learning5
Adaptive Super-Twisting Cooperative Guidance Law with Fixed-Time Convergence5
Closed-Loop Fault Diagnosis of SDR Using Gap Metric, PCA, and Kalman’s Principle5
Engineering Application of an Identification Method to Shock-Induced Vortex Stability in the Transonic Axial Fan Rotor5
Adaptive Trajectory Tracking Control for Rotorcraft Using Incremental Backstepping Sliding Mode Control Strategy5
Influence of Three-Body Gravitational Perturbation for Drag-Free Spacecraft5
Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet5
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
Visual Explainable Convolutional Neural Network for Aerodynamic Coefficient Prediction5
A Novel Active Vibration Control Method for Helicopter Fuselages Based on Diffusion Cooperation5
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
Robust Centroid Estimation Method with the Rough and Refined Estimation for Interplanetary Optical Navigation5
L1 Adaptive Fault‐Tolerant Attitude Tracking Control of UAV Systems Subject to Faults and Input Saturation5
Short‐Term Target Maneuvering Trajectory Prediction Using DTW–CNN–LSTM5
Aerodynamic Parameter Identification of Projectile Based on Improved Extreme Learning Machine and Ensemble Learning Theory5
Adaptive Distributed Fixed-Time Cooperative Three-Dimensional Guidance Law for Multimissiles against Manoeuvring Target5
Observer-Based Robust Finite-Time Trajectory Tracking Control for a Stratospheric Satellite Subject to External Disturbance and Actuator Saturation5
A Deep Learning Anomaly Detection Framework for Satellite Telemetry with Fake Anomalies5
Sensitivity and Consistency Analysis of BDS-3 GEO Satellite Orbit Maneuver Detection5
Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure5
Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine4
Cell Area-Based Method for Analyzing the Coverage Capacity of Satellite Constellations4
Integrated Optimization of Pipe Routing and Clamp Layout for Aeroengine Using Improved MOALO4
Prediction of Orbit Decay for Large-Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects4
Effect of Aeroelastic Tailoring Design on Wing Mode4
Nonlinear Dynamic Responses of a Rotor-Bearing System with Eccentric Squeeze Film Dampers4
Identification of Key Factors and Mining of Association Relations in Complex Product Assembly Process4
Fatigue Reliability Analysis System for Key Components of Aero-Engine4
Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm4
Evaluation of Ion Beam Behavior in 50 W Class RF Ion Thruster4
Sizing and Mission Profile Analysis of the Hybrid-Electric Propulsion System for Retrofitting a Fixed Wing VTOL Aircraft4
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
Deployment Impact Experiment and Dynamic Analysis of Modular Truss Antenna4
Reduction of the Influence of Interfering Signals on the Longitudinal Control of UAVs with Fixed Wing4
Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration4
Effects of Geometry of Plenum Chamber on Losses in the Bleed System of an Axial Compressor4
Detectable Inspection: Propeller Nick Detection Model Development Using YOLOv84
Dynamic Drag Reduction Effects of Aerospikes and Aerodisks4
Experimental Investigation on Flame Chemiluminescence and Flow Characteristics of a Reverse-Flow Combustor4
Improved F-RRT 4
Lightweight Design of Solar UAV Wing Structures Based on Sandwich Equivalent Theory4
Prediction of the Flight Dynamics of Maneuvering Multirotor Aircraft4
Finite Element Simulations of Dynamic Shear Fracture of Hollow Shear Pins4
Research on Aluminum Honeycomb Buffer Device for Soft Landing on the Lunar Surface4
Aviation Rivet Classification and Anomaly Detection Based on Deep Learning4
Application of the Improved Grey Wolf Algorithm in Spacecraft Maneuvering Path Planning4
Free Vibration of Annular Circular Plates Based on Higher-Order Shear Deformation Theory: A Spline Approximation Technique4
A Modified Robust Adaptive Fault Compensation Design for Spacecraft with Guaranteed Transient Performance4
Influence of Geometric Parameters on Intake Performance of 3D Ramp‐Type Scramjet Inlet4
Ontology-Based Resource Modeling and Matching Framework in Avionics Systems4
Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions4
Application of Stewart Platform in the Low-Frequency Vibration Characteristic Test of Space Truss Deployable Antenna on Satellite4
Fast Trajectory Generation Method for Midcourse Guidance Based on Convex Optimization4
High Precision Height Control for Wing-in-Ground Crafts4
An Exoatmospheric Homing Guidance Law Based on Deep Q Network4
The Numerical Simulation Method of the Slot Crack Groups’ Effect Analysis for Solid Rocket Motor Grain3
Computational Technique for Crack Propagation Simulation in Viscoelastic Solid Propellant3
Multi-UAV Cooperative Air Combat Target Assignment Method Based on VNS-IBPSO in Complex Dynamic Environment3
Global Sensitivity Analysis of Earth-Moon Transfer Orbit Parameters Based on Sobol Method3
Continuous Gesture Sequences Recognition Based on Few-Shot Learning3
Backstepping Control Based on Constrained Command Filter for Hypersonic Flight Vehicles with AOA and Actuator Constraints3
Investigation on Viscoelastic Poisson’s Ratio of Composite Materials considering the Effects of Dewetting3
Effect of Cooling Header on the Hydrocarbon Fuel Flow Distribution in a Regenerative Cooling Channel3
Automatic Landing System Design for Unmanned Fixed-Wing Vehicles via Multivariable Active Disturbance Rejection Control3
UAV Detect and Avoid from UTM-Dependent Surveillance3
Influence of Different Altitudes on the Solid Rocket Contrail Formation in the Near Field3
Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa3
Commonality Benefit Analysis for Maintenance Technical Publications of Civil Aircraft Based on Learning Effect3
Dynamic Modelling and Continuous Trajectory Tracking Control of Space Robots Based on Lie Group SE(3)3
Robust Controller Designing for an Air-Breathing Hypersonic Vehicle with an HOSVD-Based LPV Model3
Autonomous Landing of a Fixed‐Wing UAV With RTK GNSS and MEMS IMU3
Separation Control for a Transonic Convex Corner Flow Using Ramp-Type Vortex Generators3
Investigation on the Horizontal Landing Velocity and Pitch Angle Impact on the Soft-Landing Dynamic Characteristics3
An Efficient Trajectory Negotiation and Verification Method Based on Spatiotemporal Pattern Mining3
Mission Planning Issues of Imaging Satellites: Summary, Discussion, and Prospects3
Robust Integrated Guidance and Control Design for Angle Penetration Attack of Multimissiles3
Influence of Propeller Slipstream on the Flow Field of S-Shaped Intake3
A Passive Vibration Control Method of Modular Space Structures Based on Band Gap Optimization3
Air-Ground Task Collaboration Safety Analysis Based on Real-Valued Differential Biclustering for Midterm Conflict in Single-Pilot Operations of Commercial Aircraft3
A Robust Adaptive Control Algorithm for Multimissile Cooperative Formation3
A New Theoretical Method for Solving Forward Kinematics of the Parallel Mechanisms Based on Transfer Matrix3
Investigation of the Effect of Axial Gap on the Mechanical Response of a Cartridge-Loaded CMDB Propellant Grain under Vibration Loads3
A Midcourse Guidance Method Combined with Trajectory Prediction for Antinear-Space-Gliding Vehicles3
A Finite‐Time Fractional‐Order Error Extended State Observer for Hypersonic Vehicle3
Multiobjective Optimization of Turbine Coolant Collection/Distribution Plenum Based on the Surrogate Model3
Landing Reliability Assessment of Airdrop System Based on Vine-Bayesian Network3
Shape Adjustment of a Large Planar Phased Array Antenna With Nonlinear Cable Actuators3
Variable Structure Control and Its Ground Experimental Test for the Space Station Robot3
Target Tactical Intention Recognition in Multiaircraft Cooperative Air Combat3
Effects of Flow Coefficient on Turbine Aerodynamic Performance and Loss Characteristics3
Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy3
Research on Flow Characteristics of a Variable Mach Number Aerodynamic Test Device by a Rotating Profile3
Design of Corrugated Airfoil for a Flapping Wing Micro Air Vehicle3
High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument3
Numerical Simulation of Ice Crystal Supercooled Droplet Mixed Phase Icing Based on the Improved Messinger Model3
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
Fault-Tolerant Control of Hypersonic Vehicle Using Neural Network and Sliding Mode3
A Decision-Making Method for Distributed Unmanned Aerial Vehicle Swarm considering Attack Constraints in the Cooperative Strike Phase3
Experimental and Numerical Investigations on the Ignition of RBCC Gas-Oxygen/Kerosene Rocket Ejector3
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