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ABSTRACT
- Hierarchical conflict resolution for orbital transfer scheduling in LEO constellations under partial satellite failures
- A multi-modal deep learning method for SGP4 orbit propagation accuracy enhancement
- RoverDevKit: An open, physics-grounded tradespace toolkit for conceptual design of lunar micro-rovers
- Online all-azimuth return guidance with specified terminal heading for a winged reusable launch vehicle demonstrator
- All-directional optimal Glideslope approach for rendezvous of satellites in proximity
- A virtual blueprint-based guidance framework for autonomous lunar construction
- Simulating ionic liquid fragmentation in electrospray thrusters with foundation models
- Projections of Earth’s technosphere: Civilization collapse–recovery dynamics and detectability
- Topology-based screening of radio-frequency blockage in reentry plasma using flight-test data
- Nuclear-powered propulsion systems for space exploration
- Dynamic Characteristics of a High-Speed Electric Canned Pump Affected by Balancing-Hole Configuration in Rocket Engines
- Investigation of heat and mass transfer nonuniformities and tailored coolant supply strategies in nose cone transpiration cooling
- Artificial intelligence assisted analysis of three-dimensional Casson quaternary hybrid nanofluid flow over a Riga plate in porous media for advanced aerospace thermal management applications
- Nonlinear dynamic stability of a blisk model under Poisson white noise
- Dynamic modeling and vibration characteristics of cracked rotating thin plates based on the absolute nodal coordinate formulation
- Physics informed reduced-order modelling of supersonic jet-induced cratering
- Predefined-time attitude control of liquid-filled spacecraft in microgravity environment
- Orbital phase deployment and maintenance of Disksat via atmospheric differential drag control
- Influence of tolerance on lubrication of the slipper/swashplate interface in aviation fuel piston pumps: A transient Fluid-Structure-Thermal-Cavitation Interaction model
- A multi-candidate semantic safe-corridor planner for incremental UAV path recovery in grid-coded low-altitude airspace
- RAPID-DETR: replay-augmented and pseudo-label-guided class-incremental object detection of aero-engine components
- Evolution of flame dynamics and combustion instability during transient fuel switching in a centrally staged swirl combustor
- Continuous risk field-based kinodynamic planning for RLVs in uncertain debris environments: A multi-strategy approach for representative risk–maneuver candidate generation
- A novel efficient algorithm for quad-dominant structured mesh generation of aircraft wingbox structures
- Compliant-boundary modeling and dual-rotor experimental assessment of an elastic ring squeeze film damper for aero-engine main-bearing support
- Self-attention-guided vibration suppression for mistuned bladed disks
- Waverider design based on the physics-informed neural networks with artificial viscosity
- A bi-gain fixed-time ESO for abrupt disturbance estimation under measurement noise with its application to structurally damaged aircraft
- Kinematic-aware spatio-temporal graph neural network for multi-step UAV trajectory prediction
- Lossless convex trajectory optimization for solar-sail transfers from Earth–Moon NRHOs to Sun–Earth halo orbits
- On the consistency of turbomachinery RANS solvers in predicting axial compressor flows: A perspective from the GPPS CFD workshop
- Terminal time and angle-constrained nonlinear intercept guidance
- A task-driven distributed cooperative allocation algorithm for time-sensitive target tracking in LEO constellations
- Ultrasonic regulation of residual stress and mechanical properties in two-stage HTPB solid propellants during the curing and molding process
- Multi-objective optimization and mechanism analysis of an aero-engine scavenge centrifugal pump under high gas volume fraction conditions
- Additively-manufactured hierarchal IsoTruss lattice conical shells for payload adapter: Design, vibration and axial compression behaviors
- Characteristics of flow and heat transfer dominated by combustion mode transition in a cavity-based scramjet
- Effects of jet-jet interaction on crater formation and particle ejection during plume-surface interaction at Martian pressure
- Multi-objective impeller optimisation of a gas–liquid multiphase pump under surge conditions: flow stabilisation and performance enhancement
- Three-dimensional guidance law for maneuvering-target interception with prescribed terminal angle and field-of-view constraints
- A numerical decomposition of the tonal noise sources of an electric ducted fan
- Wide-temperature oxidation resistance and thermal protection performance of a novel Ti3AlC2-TiB2−MoSi2 co-modified ceramizable composite
- Hierarchical collaborative dynamics modeling for unmanned aerial vehicles driven by subdomain complexity
- Data-driven investigation of low-Reynolds-number flow mechanisms and multi-Reynolds-number optimization of compressor cascades
- Optimization of multiple parameters in the Beddoes-Leishman dynamic stall model for large wind turbine blades
- Multi-objective optimization and performance evaluation of a deployable antenna mechanism based on triangular-hexagonal heterogeneous pyramid modules
- Real-time on-orbit spacecraft thermal prediction using an optimized physics-informed neural network
- Effects of Tilt Speed and Freestream Velocity on Tilt-Wing eVTOL Conversion Aerodynamics: High-Fidelity Comparison of Forward and Backward Transitions
- Pre-Fusion IMU Error Compensation Driven by Flight Excitation for UAV Navigation Under Intermittent GNSS Outages
- A novel failure mechanism of plastic bending in a low-pressure turbine shaft induced by dual-rotor coupled vibration
- A multi-scenario aerodynamic model extension and prediction framework for high-spin projectiles under partially unmeasurable conditions
- Real-time arrival flight control: A reinforcement learning approach with sequencing constraints
- Effects of swirl number on the flow field characteristics in a full-annular swirl intake combustor with jet impingement
- Design of Experiments Framework for Experimental Total Impulse Optimization of a Reduced-Scale Solid Rocket Motor
- Machine-Learning Surrogates for the Aerothermal Environment of Blunt Bodies in Hypersonic Re-entry
- Safe learning-scheduled allocation for spacecraft with variable-speed control moment gyroscopes
- Estimation of aircraft initial mass based on takeoff and early climb performance
- Propeller Icing Under Forward and Transition Flight Conditions: An Experimental Study
- Rapid prediction of three-dimensional turbine vane flow fields via radial-sectional decomposition and a multi-scale swin transformer
- Signed leakage transport and phase-dependent pressure response in an axial compressor
- The Effect of Spray’s Droplet Size Distribution on the Turbulent Swirl Stabilized Flame in a Model Combustor
- Impact-induced reaction evolution in solid rocket motors: SPH simulation and physics-informed prediction
- Optical Diagnostics of Liquid Contamination in Liquid Propellant Thruster Plumes: Part III–Experimental Results from a 10 N Bipropellant Thruster
- Environmental effects on ground modal test and on-orbit modal estimation of low-frequency flexible solar arrays
- Aeroelastic Mechanism analysis between flapwise and torsion in sweep tip rotor blade
- Quasi-steady performance of surface jets for load alleviation on flexible aircraft wings
- Design method and optimization of hypersonic blended wing-body vehicle based on parametric subdivision surfaces
- Enhanced mechanical properties of bionic re-entrant honeycomb under in-plane compression
- Safety-critical predefined-time flight control of tailless aircraft for automatic carrier landing
- A big-data-driven foundation model for flutter control and energy harvesting of smart viscoelastic lattice sandwich plates
- A Q-learning approach for optimal tracking constrained control using unknown user-define cost and advantage function with applications to F-16 aircraft
- State-triggered coordinated attitude–deployment–propulsion transition strategy for a tube-launched tandem-wing unmanned aerial vehicle
- Predictive models of acoustic dynamics of a contra-rotating propeller UAV during ascent, hover, and descent
- Chance-Constrained Sequential Convex Programming for Rocket-Powered Landing Trajectory Optimization
- Aeroelastic flutter analysis and multi-parameter optimization of auxetic honeycomb-corrugated sandwich conical shells in supersonic flow
- Event-triggered aero-RCS coordination via incremental ADP for performance guaranteed control under degraded aerodynamic authority
- Reduced-order contraction-based tracking control for input-affine systems: Application to multi-phase maneuvering flight
- A novel blade leading edge design method for low shock-associated tone noise
- Experimental study on rotating detonation ramjet in a hollow combustor under different expansion sections
- Feasibility of force-controlled contact capacitor-discharge stud welding in vacuum for local interface creation on spacecraft-relevant aluminium surfaces
- Groove–hole topology and placement effects on axial-force oscillations in cavitating high-speed electric canned motor pumps
- An integrated framework for noise prediction, auralization, and psychoacoustic assessment of unmanned aircraft systems
- Cooperative mission planning for persistent tracking of multiple maritime moving targets using agile Earth observation satellites
- Application of a time-marching tight coupling method for helicopter rotor aeroelastic analyses in steady and unsteady flight conditions
- Thermodynamic cycle analysis and CFD of a two-stage rotating detonation afterburning propulsion system
- Robust multi-source fusion positioning in integrated air-to-ground networks via maximum entropy principle
- Investigation of acoustic signatures associated with vortex ring state in helicopter flight
- Blade vibration difference amplitude constraint-based enhanced multiple signal classification algorithm for blade asynchronous vibration frequency identification
- Wind tunnel study of the time-averaged performance of a stacked rotor in forward flight and hover
- Small-signal stability analysis and control design for eVTOL PDCM
- Analytical synthesis of control laws for lateral motion of an aircraft-type spacecraft during landing at the lack of information on several components of the state vector
- Discharge Hysteresis in a Microwave Cusped Field Thruster: Characteristics, Mechanism, and Suppression
- Numerical Modeling of Hypervelocity Damage to Protected Spacecraft Ammonia Fluid Lines using Physics-Informed Machine Learning
- Multi-Agent Cooperative Exploration Scheme Construction and Cluster Intelligent Path Planning for Asteroid Surface Roving
- Comparative study on the impact energy absorption of contact and spaced aluminum honeycomb structures
- Effects of structural parameters on pressure-to-thrust oscillation transfer in solid rocket motors with a backward-facing step
- Research on the influence of water-laden airflow on non-equilibrium wet compression characteristics of axial compressors and the rapid prediction method
- A climb-coupled Breguet model and parametric sensitivity analysis of cruise design points for RBCC-powered hypersonic vehicles
- Effects of dynamic valve opening and multi-chamber staged gas supply on the performance of a supercritical CO₂ pneumatic launch system
- Physics-informed autoencoder transfer learning for multi-fidelity aerodynamic data fusion
- Implementation of a synthetic turbulent inflow condition in OpenFOAM for predicting the flow dynamics and aeroacoustics of a NACA 65(12)-10 airfoil at Re = 100,000
- Shock and secondary flow interactions for non-axisymmetric endwall profiling in a transonic turbine
- Surrogate modelling and conditional safety-envelope analysis of aircraft veer-off risk during landing under coupled crosswind and non-uniform runway-water conditions
- EAVC-GAN: A Semi-supervised transfer learning framework for cross-condition aero-engine gas path fault diagnosis
- A graph-based multi-scenario aircraft conceptual design framework for system-of-systems
- Lift augmentation of Martian UAV airfoils via plasma-based flow control
- A geometry-aware hybrid graph neural operator-driven method for sparse wall-pressure reconstruction in supersonic two-phase flow fields
- U3DWind: A low altitude wind field dataset and benchmark for urban air mobility
- Aerodynamic loads and their impact on the structural response of high bypass ratio aeroengines
- Acoustic–inertial coupling effects on particle behavior and thermal feedback in solid rocket motors
- Experimental investigation of vortex ring state for multicopters
- Mission constraints can reverse sustainable aviation fuel rankings: Model-form, property-uncertainty, and aircraft-constraint effects
- Ram-air cooling for fuel cell aircraft
- Reduced-order evaluation of superconducting magnetoplasma propulsion in aircraft and rocket flight
- Physics-informed surrogate optimization of aerospace high-speed solenoid valves under multiphysics dynamic coupling
- Uncertainty quantification of effects of coupled manufacturing deviations on centrifugal impeller performance
- Rapid computation of reachable touchdown set for Mars soft landing via convex optimization
- Development and verification of versatile laser satellite link emulator for laser satellite communications
- Transition mechanism of combustion mode and shock wave trains affected by scramjet wall temperature and equivalence ratio
- IGV-Induced fragment redistribution and cumulative blade damage in sequential bird ingestion
- High-fidelity aerostructural optimization of UAV propellers with experimental validation
- Feature extraction and multiple failures identification of bearing of aeroengine based on adaptive feature mode decomposition and co-occurrence 1D-LBP
- Design optimization of N2O-powered hybrid rocket first stage with alternative fuels and architectures
- Spinner/nacelle blockage over propellers: A blade-element/momentum theory approach
- Uncertainty-aware visual servoing predictive control for small quadcopter landing on moving decks
- Optimization-based beacon observation planning for autonomous optical spacecraft navigation
- Robust adaptive active inference for resilient UAV state estimation under sensor and actuator faults
- Intelligent identification method for stiffness states and loading positions of a large-scale hypersonic vehicle model
- Design and electro-thermo-mechanical optimization of an anti-icing/de-icing electrothermal sandwich composite
- GateFuse: Gradient-gated multi-scale routing for compressible flow reconstruction
- Fluid-structure interaction mechanism and suppression methods for spin instability of cruciform parachutes
- A volume-based dynamic simulation method for aero-engines using Isomap-BP manifold reconstruction and power turbine efficiency correction
- Buckling behavior of a propellant tank dome assembly for a small launch vehicle considering geometric imperfections and manufacturing defects
- Uncertainty quantification of thermochemical and wall-catalysis model parameters for high-speed flows
- Applied-field magnetoplasmadynamic thruster–based particle flow generator for very low Earth orbit (VLEO)–relevant environment
- Integrated modeling and vibration control of aeroengine external system with variable stiffness brackets
- Experimental and Numerical Investigation of Aeroacoustic Sources in a Strut-Braced Wing Configuration
- A Gaussian-Embedded Hybrid Neural Network Method for Rotor Airfoil Dynamic Stall Loading Noise Prediction
- Numerical investigation of Ram air turbine icing and associated impacts
- An advanced physics–system-identification integrated framework for the pressure coupled response of AP/HTPB solid propellants
- Robust mixed-integer predictive planning for multi-robot lunar construction
- Autonomous navigation and control of spacecraft swarms for multipoint in situ aeronomy
- Adaptive Precision Temperature Control with Full-Domain Reduced-Order Perception for Space-Borne Gravitational Wave Detection
- On the satellite constellation launching techniques and their implications for spacecraft structural design
- Composition-dependent Albedo radiation environment on the lunar surface and its implications for COTS electronics single-event effect rates
- Modelling-based estimates of spaceflight energy expenditure in individuals of short stature associated with skeletal dysplasias
- Feasibility of capillary-driven orbital liquid mirror telescopes
- Mission-oriented maneuverability assessment framework for a satellite integrated with atmosphere-breathing electric propulsion
- Data-driven reachable-set-based receding-horizon adaptive dynamic programming for proximity operations of non-cooperative targets
- A methodology for integrating Life Cycle Assessment into a multidisciplinary design analysis and optimization framework for sustainable launcher development
- Charging analysis and shielding strategy for high-energy particles in TianQin spacecraft
- Observer-assisted fixed-time control allocation for flexible sloshing launch vehicles under thrust-vector amplitude constraints
- Sensorimotor adaptation to gravity-compensated and augmented upper-limb loading assessed by electromyographic and behavioral measures
- Hierarchical configuration and lattice design of an ultra-large space factory with gravity-gradient and spin stabilization
- Deep Learning-Based Comprehensive Operating Cost Optimization for Active Modulation of Gas Turbine Cooling Air Flow: Trade-Offs among Efficiency, Emissions, and Vane Creep Life
- Design and FEA-Based Multi-Parameter Optimization of a Permanent-Magnet Motor for UAV Propulsion: Effects of Winding Configuration, Air Gap, and Stator Geometry
- Development and Characterisation of Non-Hypergolic–Restartable Hybrid Rocket Fuel
- An integrated end wall and suction surface inverse design method for an axial compressor cascade based on a target velocity distribution
- Gain Identifiability and Performance Limits in Uncertainty-Aware Tuning for Reusable-Launcher Recovery Control
- Uncertainty-aware fault diagnosis method of aircraft structures via manifold-embedded interval process modelling
- Development and application of a hydrogen aircraft fuel system mass estimation framework
- Input-constrained coordinated control of chamber pressure and mixture ratio in a LOX/CH₄ rocket engine with venturi–pintle throttling
- Inverse Design Optimization of Profile-truncated Busemann Intake Using Surrogate Models
- Heat Transfer Investigation of Regenerative Cooling for Hydrogen Peroxide Rocket Engines
- Thermo-mechanical coupling analysis of heat pipes in space precision measurement payloads based on a thermoelastic model
- Near optimal lead-angle polynomial shaping guidance with multiple constraints
- Research on real-time defect detection for aero-engine blade surface images based on laser scanning technology and improved real-time detection transformer
- Similarity Theory Based Scaling of an Integrated Afterburner: Methodology and Experimental Validation
- Improved probability hypothesis density filter for inaccurate model and heavy-tailed noise
- Machine learning based prediction of three-dimensional MHD casson nanofluid flow over a bidirectionally stretching surface incorporating hall and ion slip effects
- A structural ROM-assisted CFD/VPM framework for elastic rotor aerodynamics and wake evolution
- Synthetic jet control of unsteady separated flow over flying wing aircraft
- Disruptive Helicopter Composite Engine Deck Architectures using Fiber Reinforced Ceramics
- Transition control for STOVL aircraft during take-off: A Lyapunov-guided reinforcement learning approach for hierarchical control allocation
- Model-enhanced ADP-based guidance law for maneuvering target cooperative interception via online PINN identifier
- The EMA Justitia probe: Terminator frame-based deployment orbit selection and surface coverage analysis
- Model-based requirements definition for the delta development of the LISA release mechanism
- Hierarchical optimal spacecraft attitude control under pointing constraints via successive Galerkin approximation
- A deployed net shape maintenance method for space debris removal using energy-dissipating plastic tethers
- An MBSE framework for the feasibility assessment of a modular Planetary Sunshade System
- New families of periodic orbits for solar-sail satellites about photo-gravitational equilibrium points in the restricted two body problem and circular restricted three body problem
- Effects of fuel injection modes on flow and lean combustion characteristics of a novel vortex-controlled flameholder for aircraft engine
- Thermal ablation and acceleration zone division in pulsed plasma thruster discharge channels
- Precooler-transonic compressor matching in precooled engines: radial combined distortion effects and duct design trade-off
- Development of a multi-mineral martian regolith simulant benchmarked against NWA 10153
- Physics-informed Hierarchical Controller for Adaptive Gait Transition of Multi-Legged Space Robots in Microgravity
- Inversion-free Picard-quasilinear collocation method for large-step spacecraft orbit propagation
- A hybrid TFT-SGP4 framework for long-term orbit prediction of uncontrolled LEO objects under disturbed space-weather conditions
- Surrogate-assisted multi-objective optimization of blowing-assisted suppression strategy for tail stall flutter
- An improved in-motion optimization-based alignment method for GNSS-aided low-cost SINS with stochastic error-aware multi-vector construction
- Mechanism of leakage suppression in honeycomb seal structures via inclined wall-holes
- Aviation kerosene atomization and outlet spray distribution in a confined transition duct of a wave rotor combustor: Roles of fuel-manifold configuration, air mass flow rate and injection pressure
- Unified parameterization and flow-regulation mechanisms of transonic compressor blade profiles based on an exponential camber line
- Dynamic response of adjustable sheet-rod with hinge connection under base excitation
- A cross-model adaptable atmospheric density error suppression method for SINS/RCNS integrated navigation
- Coverage-aware LLM-guided reweighting for limited-label cross-domain aero-engine remaining useful life prediction
- A fractional-power-free predefined-time guidance law with asymmetric disturbance feedforward for high-speed target interception under field-of-view constraints
- LLM-driven hyper-heuristic optimization for integrated internal-external trajectory design
- Dynamic modeling and uncertainty analysis of bolted flange-drum structures
- Integrated scheduling of satellite observation and data transmission via two-stage interactive scheduling algorithm assisted by large language model
