Aerospace

Papers
(The H4-Index of Aerospace is 36. 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 Parameter Self-Tuning Rule Based on Spatial–Temporal Scale for Active Disturbance Rejection Control and Its Application in Flight Test Chamber Systems93
Simulation and Design of a CubeSat-Compatible X-Ray Photovoltaic Payload Using Timepix3 Sensors92
Conceptual Design and Aerostructural Trade-Offs in Hydrogen- Powered Strut-Braced Wing Aircraft: Insights into Dry and Wet Ultra-High Aspect Ratio Wings78
Impact of Groove Manufacturing Errors on Aircraft Skin-Friction Reduction71
The Low Fuel Consumption Keeping Method of Eccentricity under Integrated Keeping of Inclination-Longitude71
Playful Probing: Towards Understanding the Interaction with Machine Learning in the Design of Maintenance Planning Tools69
Three-Dimensional Flutter Numerical Simulation of Wings in Heavy Gas and Transonic Flutter Similarity Law Correction Method68
Path Planning with Multiple UAVs Considering the Sensing Range and Improved K-Means Clustering in WSNs66
Combustion Characteristics of HTPB-Based Hybrid Rocket Fuels: Using Nickel Oxide as the Polymer Matrix Pyrolysis Catalyst63
Hugoniot Relation for a Bow-Shaped Detonation Wave Generated in RP Laser Propulsion62
Pressure Characteristics and Vortex Observation in Chiral-Symmetric Space Orthogonal Bifurcation58
Effect of Quasi-Static Door Operation on Shear Layer Bifurcations in Supersonic Cavities57
Experimental Study on the Ignition/Extinction Performances of a Central Staged Direct Mixing Combustor and the Construction of an Engineering Prediction Model56
Study on Plasma-Chemical Mode of Pulsed Coaxial Dielectric Barrier Discharge Plasma Based on Mass Spectrometry53
A Generic Actuator Management Solution for Space Applications Based on Convex Optimization49
Learning Aircraft Spin Dynamics from Measurement Data Using Hankel DMDc with Error in Variables49
Investigation of Fluid–Structure Interactions of an Uncontrolled Flexible Hemisphere Utilising Non-Simultaneous Stereo Particle Image Velocimetry and Digital Image Correlation47
Combustion of Date Stone and Jojoba Solid Waste in a Hybrid Rocket-like Combustion Chamber47
Study on Flow Structure Characteristics Along the Latticework Duct Subchannels and Classification Boundary Prediction46
HCF and LCF Analysis of a Generic Full Admission Turbine Blade46
Development and Evaluation of Regolith Mass Estimation Sensor Based on Photoresist Effect46
A Multisubstructure-Based Method for the Assessment of Displacement and Stress in a Fluid–Structure Interaction Framework45
Special Issue “Gust Influences on Aerospace”44
UAV Control Based on Pattern Recognition in Aquaculture Application42
The Communicative Behavior of Russian Cosmonauts: “Content” Space Experiment Result Generalization41
Effects of Aeroelastic Walls on the Aeroacoustics in Transonic Cavity Flow41
Numerical Modeling of the Walls Perforation Influence on the Accuracy of Wind Tunnel Experiments Using Two-Dimensional Computational Fluid Dynamics Model41
Assessing an Image-to-Image Approach to Global Path Planning for a Planetary Exploration40
Finite-Time Tracking Control Based on Immersion and Invariance with Dynamically Scaling Factor for Agile Missiles40
An Improved Fault Identification Method for Electromechanical Actuators39
Integrated Hardware and Algorithmic Decoupling of Light-Noise-Attenuation Coupled Errors: A Path to 50 Pa Precision in Micro-Pressure PSP Measurements39
Implementing a Multi-Attribute Decision-Making-Based Approach to Evaluate Small Electric Vertical Takeoff and Landing Fixed-Wing Drones with Mission Efficiency39
Mission Design and Orbit-Attitude Control Algorithms Development of Multistatic SAR Satellites for Very-High-Resolution Stripmap Imaging37
Attitude Maneuver and Stability Control of Hyper-Agile Satellite Using Reconfigurable Control Moment Gyros37
Numerical Investigation on the Mechanism of Solid Rocket Motor Instability Induced by Differences between On-Ground and In-Flight Conditions37
A Prognostic and Health Management Framework for Aero-Engines Based on a Dynamic Probability Model and LSTM Network37
Design and Mechanical Properties of Maximum Bulk Modulus Microstructures Based on a Smooth Topology with Grid Point Density36
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