publication venue for

• Augmented Reality-Enabled Intuitive Trajectory Design with HoloAstro 2026
• Improving Electron Emission Observability for Spacecraft Touchless Potential Sensing 2026
• Autonomous Vision-Based Navigation at Small Bodies Combining Centroiding and Visual Odometry 2026
• Spacesuit Thermal Control System Requirements for Martian Surface Operations Using Analytical Modeling 2025
• Meta-Reinforcement Learning for Spacecraft Proximity Operations Guidance and Control in Cislunar Space 2025
• Optimal Agile Satellite Target Scheduling with Learned Dynamics 2025
• Stochastic Mission Exploration Tool for Asteroid Tours 2025
• A Conceptual Modeling Approach for Performance of Magnetohydrodynamic Drag During Planetary Entry 2025
• Dimensionality Reduction for Onboard Modeling of Uncertain Atmospheres 2025
• Three-Dimensional Radiation Analysis of the Hypersonic Jules Verne Reentry Spectra 2025
• In-Situ Turbulence and Particulate Measurements in Support of the BOLT II Flight Experiment 2024
• Coupled Spacecraft Charging Due to Continuous Electron Beam Emission and Impact 2024
• General Dynamics for Single- and Dual-Axis Rotating Rigid Spacecraft Components 2024
• Investigation of Surface-Catalycity Effects on Hypersonic Glide Vehicle Trajectory Optimization 2024
• Single-Agent Reinforcement Learning for Scalable Earth-Observing Satellite Constellation Operations 2024
• Co-Delivery of a Martian Probe Network 2023
• Passively Safe Spacecraft Motion Using Reachable Sets and Orbital Element Differences 2023
• Relative Motion in the Velocity Frame for Atmospheric Entry Trajectories 2023
• Atmospheric Density Estimation Techniques for Aerocapture 2023
• Designing Low-Thrust Transfers near Earth-Moon L₂ via Multi-Objective Reinforcement Learning 2023
• Touchless Potential Sensing of Differentially Charged Spacecraft Using X-Rays 2023
• Methods to Detect Impact-Induced Orbit Perturbations Using Spacecraft Navigation Data 2023
• Decentralized Formation and Constellation Stability Design Requirements Using Differential Mean Orbit Elements 2022
• Data-Driven Analysis of the Stiffness Degradation of a Woven Thermal Protection System 2022
• Remote Electrostatic Potential Sensing for Proximity Operations: Comparison and Fusion of Methods 2022
• Touchless Potential Sensing of Differentially Charged Spacecraft Using Secondary Electrons 2022
• Constrained Attitude Maneuvering via Modified Rodrigues Parameters Based Motion Planning Algorithms 2022
• Constrained Guidance for Spacecraft Proximity Operations Under Electrostatic Perturbations 2022
• Using Plasma-Induced X-Ray Emission to Estimate Electrostatic Potentials on Nearby Space Objects 2022
• Landing Site Selection Using a Geometrically Conforming Footprint on Hazardous Small Bodies 2022
• Quantifying Uncertainty in Predictions of Spacecraft Erosion Induced by a Hall Thruster 2022
• Simulation and Uncertainty Quantification of Electron Beams in Active Spacecraft Charging Scenarios 2022
• Assessment of Hypersonic Double-Cone Experiments for Validation of Thermochemistry Models 2022
• Deployment Dynamics Analysis of an Origami-Folded Spacecraft Structure with Elastic Hinges 2022
• Effects of Electric Potential Uncertainty on Electrostatic Tractor Relative Motion Control Equilibria 2022
• Generation of Spacecraft Operations Procedures Using Deep Reinforcement Learning 2022
• Optimal Information Filtering for Robust Aerocapture Trajectory Generation and Guidance 2022
• Diamagnetically Enhanced Electrolysis and Phase Separation in Low Gravity 2022
• Extendable Origami Multilayer Insulation Design and Thermal Performance Characterization (Jan, 10.2514/1.A34883, 2021) 2022
• Flight Mechanics Feasibility Assessment for Co-Delivery of Direct-Entry Probe and Aerocapture Orbiter 2022
• Multi-Event Jettison Guidance Approaches for Drag-Modulation Aerocapture 2022
• Electron-Based Touchless Potential Sensing of Shape Primitives and Differentially-Charged Spacecraft 2021
• Designing Low-Thrust Transfers to High-Inclination Science Orbits via Hybrid Optimization 2021
• Centroid and Apparent Diameter Optical Navigation on Mars Orbit 2021
• Cislunar Periodic Orbit Analysis for Persistent Space Object Detection Capability 2021
• Extendable Origami Multilayer Insulation Design and Thermal Performance Characterization 2021
• Global Steering for Control Moment Gyroscope Clusters Using Heuristic Variable Search Techniques 2021
• Effect of N Atoms on O-Atom Reactivity with Carbon 2021
• Lyapunov Optimal Touchless Electrostatic Detumbling of Space Debris in GEO Using a Surface Multisphere Model 2021
• Attitude Estimation with Albedo Interference on Sun Sensor Measurements 2021
• Chip Scale Atomic Clock-Driven One-Way Radiometric Tracking for Low-Earth-Orbit CubeSat Navigation 2021
• Ionic-Liquid-Based Contactors for Carbon Dioxide Removal from Simulated Spacecraft Cabin Atmospheres 2020
• Removing Rate Unobservability in Sun-Heading Filters Without Rate Gyroscopes 2020
• Improved Modal Damping Characterization for Small-Scale Heliogyro Blades 2020
• Active Mass Ejection for Asteroid Manipulation and Deflection 2020
• Development of an Achievability Propellant Limit Algorithm for a Piloted, Lunar Lander 2020
• Prospects of a Hybrid Magnetic/Electrostatic Sample Container Retriever 2020
• Multisphere Method for Flexible Conducting Space Objects: Modeling and Experiments 2020
• Arcjet Thruster Influence on Local Magnetic Field Measurements from a Geostationary Satellite 2020
• Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude 2020
• Simulation of Nonspherical Asteroid Landers: Contact Modeling and Shape Effects on Bouncing 2020
• Conjugate Analyses of Ablation in Rocket Nozzles 2019
• Heterogeneous Surface Multisphere Models Using Method of Moments Foundations 2019
• Orbital Stability Regions for Hypothetical Natural Satellites of (101955) Bennu 2019
• General Hinged Rigid-Body Dynamics Approximating First-Order Spacecraft Solar Panel Flexing 2018
• Robust Attitude Control Using a Double-Gimbal Variable-Speed Control Moment Gyroscope 2018
• Prearrival Deployment Analysis of Rovers on Hayabusa2 Asteroid Explorer 2018
• Conceptual Design of an Air-Breathing Electric Thruster for CubeSat Applications 2018
• Convex Optimization for Power Tracking of Double-Gimbal Variable-Speed Control Moment Gyroscopes 2018
• Modeling Magnetohydrodynamic Energy Generation and Storage in Planetary Entry System Conceptual Design 2018
• Parametric Study of Ballistic Lander Deployment to Small Bodies 2017
• Unsteady Simulations of Rocket Plume Expansions in Geostationary Earth Orbit 2017
• Steady-State Attitude and Control Effort Sensitivity Analysis of Discretized Thruster Implementations 2017
• Thermal Vacuum Evaluation of Simulated Spacecraft Radiators with Discretized Emissivity Surface Properties 2017
• Two-Dimensional Modeling of Ablation and Pyrolysis with Application to Rocket Nozzles 2017
• Comparative Analysis of Satellite Aerodynamics and Its Application to Space-Object Identification 2016
• Miniature X-Ray Solar Spectrometer: A Science-Oriented, University 3U CubeSat 2016
• Characterizing a Transient Heat Flux Envelope for Lunar-Surface Spacesuit Thermal Control Applications 2015
• Computation of Hypersonic Flows Using the Direct Simulation Monte Carlo Method 2015
• Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation 2015
• Contact Motion on Surface of Asteroid 2014
• Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether 2014
• Nonlinear Dynamics of Objects in Transition Flow During Atmospheric Entry 2014
• Investigations of Peripheral Propulsive Deceleration Jets on a Mars Science Laboratory Aeroshell 2014
• Human Spatial Orientation Perception During Simulated Lunar Landing Motions 2014
• Rigid-Body Dynamics in Free-Molecular and Transition Flow 2014
• Aerodynamic Analysis Based on Challenging Minisatellite Payload Satellite Lift-to-Drag Measurements 2013
• Effect of Density Model Time-Delay Errors on Orbit Prediction 2013
• Propulsion Deceleration Studies Using Planar Laser-Induced Iodine Fluorescence and Computational Fluid Dynamics 2013
• Characterizing Human Spacecraft Safety and Operability Through a Minimum Functionality Design Methodology 2013
• Semi-Empirical Satellite Accommodation Model for Spherical and Randomly Tumbling Objects 2013
• Hypersonic Flow and Radiation Analysis of the Automated Transfer Vehicle Jules Verne 2013
• Effectiveness of a Magnetohydrodynamics System for Mars Entry 2012
• Effectiveness of a Magnetohydrodynamics System for Mars Entry 2012
• Tethered Coulomb Structure Applied to Close Proximity Situational Awareness 2012
• Sequential Orbit Determination with the Cubed-Sphere Gravity Model 2012
• Attitude and Power Analysis of Two-Node Multitetheral Coulomb Structures 2011
• Interactions of Single-Nozzle Sonic Propulsive Deceleration Jets on Mars Entry Aeroshells 2011
• Rotational Stiffness Study of Two-Element Tethered Coulomb Structures 2011
• Drag Coefficients of Satellites with Concave Geometries: Comparing Models and Observations 2011
• Modeling of Stardust Entry at High Altitude, Part 2: Radiation Analysis 2010
• Semiempirical Model for Satellite Energy-Accommodation Coefficients 2010
• Modeling of Stardust Entry at High Altitude, Part 1: Flowfield Analysis 2010
• Numerical Study of Magnetoaerodynamic Flow Around a Hemisphere 2010
• Modeling of Electromagnetic Manipulation of Plasmas for Communication During Reentry Flight 2010
• Coning Control of Solar Sails Using Magnetic Momentum Error Reduction 2009
• Sensitivity of Orbit Predictions to Density Variability 2009
• Numerical Study of Plasma-Assisted Aerodynamic Control for Hypersonic Vehicles 2009
• Analysis of an Electromagnetic Mitigation Scheme for Reentry Telemetry Through Plasma 2008
• Comment on Special Section: New Perspectives on the Satellite Drag Environments of Earth, Mars, and Venus Reply 2008
• Multiscale Particle-Continuum Simulations of Hypersonic Flow over a Planetary Probe 2008
• Improved Atomic Oxygen Quantification Within the Earth's Upper Atmosphere Through Numerical Corrections 2008
• Electromagnetic reduction of plasma density during atmospheric reentry and hypersonic flights 2008
• Collisionless gas expanding into vacuum 2007
• Density and winds in the thermosphere deduced from accelerometer data 2007
• Introduction: New perspectives on the satellite drag environments of Earth, Mars, and Venus 2007
• Satellite drag variability at Earth, Mars, and Venus due to solar rotation 2007
• Storm-time equatorial density enhancements observed by CHAMP and GRACE 2007
• Finite Element Modeling of Sail Deformation Under Solar Radiation Pressure 2007
• Theoretical and numerical study of free-molecular flow problems 2007
• Erratum on simulation of aerodynamic influences on rocket-mounted oxygen sensors (vol 43, pg 1387, 2006) 2007
• Automated operational orbit determination for the Ice Cloud and Land Elevation Satellite mission 2006
• Distributed and localized active vibration isolation in membrane structures 2006
• Maximizing payload mass fractions of spacecraft for interplanetary electric propulsion missions 2006
• Applying analysis of international space station crew-time utilization to mission design 2006
• Computational Analysis of High-Altitude Ionization Gauge Flight Measurements 2006
• Dynamic wrinkle reduction strategies for cable-suspended membrane structures 2005
• Estimating parameterized post-Newtonian parameters from spacecraft radiometric tracking data 2005
• Generalized model for solar 2005
• Solar-system escape trajectories using solar sails 2004
• Energy accommodation in hyperthermal gas-surface collisions: Aerobraking in planetary atmospheres 2004
• Orbit determination for the QuikSCAT spacecraft 2002
• Development of a target marker for landing on asteroids 2001
• Interactions between spacecraft and thruster plumes 2001
• Review of Hall thruster plume modeling 2001
• Wear-field measurement and modeling results for flight-type arcjet: Hydrogen atom 2001
• Solar sail orbit operations at asteroids 2001
• Near-field measurement and modeling results for flight-type arcjet: NH molecule 2001
• Modeling of a pulsed plasma thruster from plasma generation to plume far field 2000
• Particle simulations of a Hall thruster plume 2000
• Detailed simulation of surface chemistry leading to spacecraft glow 1999
• Detailed computation of ultraviolet spectra in rarefied hypersonic flow 1998
• Precision orbit determination for the GEOSAT Follow-On satellites 1998
• Charged-particle telescope experiment on Clementine 1995
• PARTICLE SIMULATIONS OF HELIUM MICROTHRUSTER FLOWS 1994
• NON-LINEAR DYNAMIC PHENOMENA IN THE SPACE-SHUTTLE THERMAL PROTECTION SYSTEM 1982
• Supported Ionic Liquid Membranes for Carbon Dioxide Management in Spacecraft Cabin Atmospheres 2022
• Constrained Attitude Maneuvering via Modified-Rodrigues-Parameter-Based Motion Planning Algorithms 2021
• Impact of Electrostatic Perturbations on Proximity Operations in High Earth Orbits 2020
• Active Mass Ejection for Asteroid Manipulation and Deflection 2019
• Rapid Modeling of Electrostatic Forces and Torques Considering Dielectrics 2018
• Electrostatic Tractor Analysis Using a Measured Flux Model 2018
• Numerical Investigation of Multinozzle Propulsive Deceleration Jets for Mars Entry Aeroshells 2011
• Estimation and Modeling of Enceladus Plume Jet Density Using Cassini Flight Data 2010
• Comparison of TIMED satellite drag with solar EUV experiment (SEE) measurements 2006
• Simulation of aerodynamic influences on rocket-mounted oxygen sensors 2005
• Direct simulation Monte Carlo investigation of hyperthermal oxygen beam exposures 2004
• Erosion of Kapton® H by hyperthermal atomic oxygen 2004
• Homogeneous silica formed by the oxidation of Si(100) in hyperthermal atomic oxygen 2004