Journal of Guidance Control and Dynamics

Papers
(The median citation count of Journal of Guidance Control and Dynamics is 1. 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 2020-04-01 to 2024-04-01.)
ArticleCitations
Koopman-Operator-Based Attitude Dynamics and Control on SO(3)26
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture20
Convex Approach to Covariance Control with Application to Stochastic Low-Thrust Trajectory Optimization14
Numerical Study on Low-Velocity Impact Between Asteroid Lander and Deformable Regolith13
Unified Method for Field-of-View-Limited Homing Guidance13
Onboard Orbit Determination for Deep-Space CubeSats12
Information-Based Guidance and Control Architecture for Multi-Spacecraft On-Orbit Inspection12
Image-Based Meta-Reinforcement Learning for Autonomous Guidance of an Asteroid Impactor11
Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation11
Guidance Strategy for Autonomous Inspection of Unknown Non-Cooperative Resident Space Objects10
Varying-Gain Proportional Navigation Guidance for Precise Impact Time Control10
Impact Angle Guidance Using State-Dependent (Differential) Riccati Equation: Unified Applicability Analysis9
Low-Thrust Collision Avoidance Maneuver Optimization9
Assessment of a Scalogram-Based Pilot-Induced Oscillation Metric with Flight-Test and Simulation Data9
Global Incremental Flight Control for Agile Maneuvering of a Tailsitter Flying Wing8
Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight8
Dynamics Near the Three-Body Libration Points via Koopman Operator Theory8
Robust Space Trajectory Design Using Belief Optimal Control8
Multi-Objective Hidden Genes Genetic Algorithm for Multigravity-Assist Trajectory Optimization8
Atlas of Optimal Low-Thrust Rephasing Solutions in Circular Orbit7
Analytical Costate Estimation by a Reference Trajectory-Based Least-Squares Method7
Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories7
Absolute Triangulation Algorithms for Space Exploration7
Flexible Spacecraft Vibration Suppression by Distributed Actuators7
Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint7
Cooperative Circular Guidance with Nonuniform Field-of-View Constraints7
Multistep Newton–Picard Method for Nonlinear Differential Equations7
Nonlinear Optimal Guidance for Intercepting Stationary Targets with Impact-Time Constraints7
Analytical State Propagation for Continuous-Thrust Linear Relative Motion6
Hierarchical Four-Dimensional Trajectories Planning Method for Manned and Unmanned Aircraft Integrated Airspace6
Encirclement of Moving Targets Using Noisy Range and Bearing Measurements6
Two-Stage Dynamic-Assignment Optimization Method for Multispacecraft Debris Removal6
Hierarchical Reinforcement Learning Approach for Autonomous Cross-Country Soaring6
Nonlinear Dynamic Inversion with Actuator Dynamics: An Incremental Control Perspective6
Tackling Nonconvex Collision Avoidance Constraints for Optimal Trajectory Planning Using Saturation Functions6
Efficient Event-Based Adaptive Sliding Mode Control for Spacecraft Attitude Stabilization6
Novel Orbit Control Approach for Earth Observation with Multiple Targets6
Linear Quadratic Guidance Laws with Intercept Angle Constraints and Varying Speed Adversaries6
Harmonic Decomposition Models of Flapping-Wing Flight for Stability Analysis and Control Design6
UAV Collision Avoidance Using Mixed-Integer Second-Order Cone Programming6
Integrated Control of Continuum-Manipulator Space Robots with Actuator Saturation and Disturbances5
Analysis of an Unmanned Underwater Vehicle Propulsion Model for Motion Control5
Gust Load Alleviation Using Reduced-Order Aeroelastic Models and Observer-Based Robust Control5
Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique5
Geometrical Analysis of Station-Keeping Strategies About Libration Point Orbits5
Uniform Satellite Constellation Reconfiguration5
Factorized Partial-Update Schmidt–Kalman Filter5
Collision Probability of Debris Clouds Based on Higher-Order Boundary Value Problems4
Propellant-Optimal Powered Descent Guidance Revisited4
Nonlinear Guidance Law for Target Enclosing with Arbitrary Smooth Shapes4
Fast Analysis of Multi-Asteroid Exploration Mission Using Multiple Electric Sails4
Adaptive Neural-Network-Based Unscented Kalman Filter for Robust Pose Tracking of Noncooperative Spacecraft4
Hybrid Gaussian Mixture Splitting Techniques for Uncertainty Propagation in Nonlinear Dynamics4
Tube-Based Model Predictive Control with Uncertainty Identification for Autonomous Spacecraft Maneuvers4
Cooperative Estimation and Guidance Strategy Using Bearings-Only Measurements4
Closed-Loop, Exact-Time, Minimum-Energy Attitude Control with Analytic Gain Selection4
Exploiting Scaling Constants to Facilitate the Convergence of Indirect Trajectory Optimization Methods4
Improved Neural Adaptive Control for Nonlinear Oscillatory Dynamic of Flapping Wings4
Relative Navigation Strategy About Unknown and Uncooperative Targets4
Fourier Pseudospectral Method for Trajectory Optimization with Stability Requirements4
Equinoctial Lyapunov Control Law for Low-Thrust Rendezvous4
Optimization of Low-Thrust Rendezvous Between Circular Orbits via Thrust-Switch Strategy4
Neuro-Adaptive Prescribed Performance Control for Aerial-Recovery Drogue with Actuator Constraints4
Minimum Effort Pursuit Guidance with Multiple Delayed Engagement Decisions4
Relative Dynamics and Station-Keeping Strategy of Satellite–Sail Transverse Formation4
Existence of Infinitely Many Optimal Iso-Impulse Trajectories in Two-Body Dynamics4
Laboratory Experimentation of Spacecraft Robotic Capture Using Deep-Reinforcement-Learning–Based Guidance4
Direct Solution of the Keplerian State Transition Matrix4
Composite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around Asteroids4
Load Alleviation of Flexible Aircraft by Dynamic Control Allocation3
Maneuverability Set Estimation and Trajectory Feasibility Evaluation for eVTOL Aircraft3
Station-Keeping of L2 Halo Orbits Under Sampled-Data Model Predictive Control3
Spacecraft Attitude Reorientation with Reaction Wheel Assembly via State-Dependent Coefficient Parameterizations3
Range-Based Relative Navigation for a Swarm of Centimeter-Scale Femto-Spacecraft3
Fast Model Predictive Control for Spacecraft Rendezvous and Docking with Obstacle Avoidance3
In-Wing Pressure Measurements for Airspeed and Airflow Angle Estimation and High Angle-of-Attack Flight3
Vortex Ring State Avoidance Control Scheme Design for Nonlinear Autonomous Helicopter3
Wavelet Transform-Based Aircraft System Identification3
Spacecraft Rendezvous Using Constant-Magnitude Low Thrust3
Resident Space Object Characterization Using Polarized Light Curves3
Solving Perturbed Dynamic Systems Using Schur Decomposition3
Resource-Constrained Constellation Scheduling for Rendezvous and Servicing Operations3
Cascaded Lyapunov Vector Fields for Acceleration-Constrained Spacecraft Path Planning3
Minimum Power Control Allocation for Incremental Control of Over-Actuated Transition Aircraft3
Fast Homotopy for Spacecraft Rendezvous Trajectory Optimization with Discrete Logic3
Generalized Triangle Guidance for Safeguarding Target Using Barrier Lyapunov Function3
Null-Space-Excitation-Based Adaptive Control for an Overactuated Hexacopter Model3
Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints3
Worst-Case Analysis of Complex Nonlinear Flight Control Designs Using Deep Q-Learning3
Optimal Trajectory Design Accounting for Robust Stability of Path-Following Controller3
Cooperative Multilift Slung Load Transportation Using Haptic Admittance Control Guidance3
Integrating Nonlinear Controllability into a Multidisciplinary Design Process3
Designing Sun–Earth L2 Halo Orbit Stationkeeping Maneuvers via Reinforcement Learning3
Computing Natural Transitions Between Tori Near Resonances in the Earth–Moon System3
Asteroid Flyby Cycler Trajectory Design Using Deep Neural Networks3
Command Governors with Inexact Optimization and Without Invariance3
Fault-Tolerant Optimal Spacecraft Attitude Maneuver: An Incremental Model Approach3
Atmospheric Density Uncertainty Quantification for Satellite Conjunction Assessment3
Shortest Dubins Paths to Intercept a Target Moving on a Circle3
Neural-Network-Based Dynamic Flight Envelop Protection Within Integrated Aircraft Control System2
Gravitational Force Model Aliasing with Nongravitational Force Coefficients in Dynamic Prediction2
Trilateration Positioning Using Hybrid Camera–LiDAR System with Spherical Landmark Surface Fitting2
Incremental Passive Fault-Tolerant Control for Quadrotors Subjected to Complete Rotor Failures2
Analytical State Approximation of Electric Sail with Fixed Pitch Angle2
Passively Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systems2
Analytical Staring Attitude Control Command Generation Method for Earth Observation Satellites2
Earth–Moon L2 Quasi-Halo Orbit Family: Characteristics and Manifold Applications2
Landing Simulation in the Full Two-Body Problem of Binary Asteroids2
Nonholonomic Reorientation of Free-Flying Space Robots Using Parallelogram Actuation in Joint Space2
Dynamic Programming and Model Predictive Control Approach for Autonomous Landings2
Trajectory Optimization and Control of a Free-Floating Two-Arm Humanoid Robot2
Relative-Inclination Strategy for J2-Perturbed Low-Thrust Transfers Between Circular Orbits2
Intersatellite Distance-Keeping Control Based on Relative Motion Geometry2
Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets2
Latitude Estimation from Jupiter’s Banded Atmosphere2
Switched Control Design for Quadrotor in Target Tracking with Complex Intermittent Measurements2
Generalized Analysis of Biased Proportional Navigation Guidance with Fractional Power Error Feedback2
Dynamic Soaring Under Different Atmospheric Stability Conditions2
Plasma Detumbling of Failed Spacecraft by Using Hall Effect Thrusters2
Low-Thrust Guidance for Geocentric Transfers Using Single-Rotation-Axis Steering2
Non-Cooperative Space Target De-Tumbling Approach Using Multiple High-Temperature Superconducting Coils2
Kustaanheimo–Stiefel Variables for Planetary Protection Compliance Analysis2
Standoff Target Tracking Using Line-of-Sight Distance Bifurcation2
Spacecraft Rendezvous in Closed Keplerian Orbits Using Constant Radial Thrust Acceleration2
Autonomous Spacecraft Attitude Reorientation Using Robust Sampled-Data Control Barrier Functions2
Spacecraft Relative Motion Dynamics and Control Using Fundamental Modal Solution Constants2
Risk-Aware Path Planning for Unmanned Aerial Systems in a Spreading Wildfire2
Rapid Suboptimal Low-Thrust Space Trajectory Design2
Identity Management of Clustered Satellites with a Generalized Labeled Multi-Bernoulli Filter2
Trajectory Synthesis for the Coordinated Inspection of a Spacecraft with Safety Guarantees2
Design and Flight Test of a Stability Augmentation System for a Flexible Aircraft2
Satellite Attitude Control Using Double-Gimbal Variable-Speed Control Moment Gyro with Unbalanced Rotor2
Dynamic Modeling and Attitude Control of Large-Scale Flexible Parallel Multibody Spacecraft2
Communication-Aware Orbit Design for Small Spacecraft Swarms Around Small Bodies2
Approximation of Optimal Impulsive Flyby Transfer with Terminal Inspection Constraints2
Optimal Reaction Wheel Disturbance Avoidance via Torque Allocation Algorithms2
Three-Dimensional Spatial–Temporal Cooperative Guidance Without Active Speed Control2
Robust Stall Spin Flight Path Control with Flight Test Validation2
Reachable Domain Under J2 Perturbation for Satellites with a Single Impulse2
Gap Traversal Guidance Using Bearing Information2
Existence of Probability Density Function for Norm of Finite-Dimensional Random Vector2
Autonomous Spacecraft Rendezvous Using Tube-Based Model Predictive Control: Design and Application2
Use of Statistical Linearization for Nonlinear Least-Squares Problems in Pulsar Navigation2
Semianalytical Measures of Nonlinearity Based on Tensor Eigenpairs2
Longitudinal-Acceleration-Based Guidance Law for Maneuvering Targets Inspired by Hawk’s Attack Strategy2
Segmented Reconstruction of Low-Acceleration Orbital Maneuvers2
Implementation of a Map Relative Localization System for Planetary Landing2
Dynamics of a Nonrigid Orbital Siphon at a Near-Earth Asteroid2
Correction: Partial-Update Schmidt–Kalman Filter1
Flight Simulator Evaluation of Fuel-Efficient Arrival Profiles1
Prescribed Performance-Based Fixed-Time Adaptive Control Allocation for Overactuated Spacecraft1
Facing Future Challenges in Feedback Control of Aerospace Systems Through Scientific Experimentation1
Guidance and Control of Spin-Stabilized Projectiles Based on Super Twisting Algorithm1
Nonlinear Analysis for Wing-Rock System with Adaptive Control1
Augmented Plane Pursuit for Impact-Angle Control in Three Dimensions1
Cooperative Circular Guidance of Multiple Missiles: A Practical Prescribed-Time Consensus Approach1
Regular Celestial Mechanics and the Matrix Exponential1
Unwinding-Free Fast Finite-Time Sliding Mode Satellite Attitude Tracking Control1
Picard Iteration-Based Convexification for Fuel-Optimal Rocket Descent Inside Atmosphere1
Reduced-Order Identification of Aeroelastic Systems with Constrained and Imposed Poles1
Active Fault-Tolerant Incremental Sliding-Mode Flight Control Against Control Reversal1
Control of Aerodynamic-Driven Morphing1
Directional State Transition Tensors for Capturing Dominant Nonlinear Effects in Orbital Dynamics1
Hybrid Systems Approach to Autonomous Rendezvous and Docking of an Underactuated Satellite1
Sequential Convex Programming Using Augmented Lagrange Multiplier Method and Concave–Convex Decomposition1
Hybrid Multiscale Search for Dynamic Planning of Multi-Agent Drone Traffic1
Orthogonal Approximation of Invariant Manifolds in the Circular Restricted Three-Body Problem1
Fuel-Efficient Stationkeeping of Quasi-Satellite Orbits via Convex Optimization1
Evaluation Model and Exact Optimization Algorithm in Missile–Target Assignment1
Point-to-Point Jumping Transfer on Phobos by Prograde g′ Family1
Real-Time Quadrotor Trajectory Optimization with Time-Triggered Corridor Constraints1
Analytic Transformation Between Osculating and Mean Elements in the J2 Problem1
Mass-Optimized Gravity Tractor for Asteroid Deflection1
Disturbance Observer-Based Prescribed Performance Predictive Control for Spacecraft On-Orbit Inspection1
Experimental Validation of Constrained Spacecraft Attitude Planning via Invariant Sets1
Time-Constrained Interception with Bounded Field of View and Input Using Barrier Lyapunov Approach1
Angular-Momentum-Based Sizing of Control Moment Gyro Cluster for an Agile Spacecraft1
Theoretical Analysis of Fuel-Optimal Powered Descent Problem with State Constraints1
Correction: Optimal Impulsive Collision Avoidance in Low Earth Orbit1
Global Method to Compute Asteroid Equilibrium Points for Any Spin Rate1
Effects of Momentum Transfer Deflection Efforts on Small-Body Rotational State1
Relative Position Keeping for Precise Formation Flying Using Linear Momentum Exchange1
Neural Network Attitude Control System Design for the Wallops Arc-Second Pointer1
Minimum-Time Rendezvous via Simplified Initial Costate Normalization and Auxiliary Orbital Transfer1
Multi-Axis Nose-Pointing-and-Shooting in a Biomimetic Morphing-Wing Aircraft1
Longitudinal Flight Control Law Design with Integrated Envelope Protection1
Shock Absorber Leakage Impact on Aircraft Lateral Stability During Ground Handling Maneuvers1
Connecting the Equinoctial Elements and Rodrigues Parameters: A New Set of Elements1
Stochastic Convergence of Sobol-Based Mahalanobis Shell Sampling Collision Probability Computation1
Adaptive Finite Time Intercept Guidance1
Science Orbits with an Inner Disturbing Body and an Outer Disturbing Body1
Statistical Analysis of Autonomous Soaring Algorithm1
Slow Timescale Adaptive Control for Multiple-Timescale Systems1
Correction: Dynamic Optimization of High-Altitude Solar Aircraft Trajectories Under Station-Keeping Constraints1
Three-Dimensional Nonlinear Impact Time Guidance Using Predicted Interception Point1
Non-Self-Intersecting Trajectories and Their Applications to Satellite Constellation Design and Orbital Capacity1
Correction: Bounded Motions near Contact Binary Asteroids by Hamiltonian Structure-Preserving Control1
Local Orbital Elements for the Circular Restricted Three-Body Problem1
Autonomous Reconnaissance Trajectory Guidance at Small Near-Earth Asteroids via Reinforcement Learning1
Deep Space Navigation by Optical Pulsars1
Higher-Order Lambert Problem Solution Based on Differential Algebra1
Astrodynamics-Informed Kinodynamic Sampling-Based Motion Planning for Relative Spacecraft Motion1
Impact Risk of a Debris Cloud to Spacecraft1
Improvement of Constellation Orbit Determination Through the Incorporation of Intersatellite Ranging1
New Solution to Euler’s Equations for Asymmetric Bodies: Applications to Spacecraft Reorientation1
Near-Linear Orbit Uncertainty Propagation Using the Generalized Equinoctial Orbital Elements1
Higher-Order Soft-Trust-Region-Based Sequential Convex Programming1
Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles1
Three-Dimensional Guidance Law for Target Enclosing Within Arbitrary Smooth Shapes1
Pilot Behavior Model in Pursuit and Preview Tracking Tasks1
Enhanced Successive Convexification Based on Error-Feedback Index and Line Search Filter1
Fuel-Optimal Geometric Path Planning Algorithm for Spacecraft Formation Flying1
Three-Dimensional Guidance Law Mimicking Realistic Ballistic Trajectories1
Controllability Properties of Solar Sails1
Achieving Zero Sideslip Using Novel Control Surface Auxiron1
Optimized Escape Path Planning for Commercial Aircraft Formations1
Impartial Sensor Tasking via Forecasted Information Content Quantification1
Robust Neurocontrol for Autonomous Dynamic Soaring1
Transfers Between Moons with Escape and Capture Patterns via Lyapunov Exponent Maps1
Robust Hybrid Global Dual Quaternion Pose Control of Spacecraft-Mounted Robotic Systems1
Backstepping-Based Steering Control for Spacecraft Attitude Control Using Two-Skewed Control Moment Gyroscopes1
Impact Angle Control Guidance Considering Seeker’s Field-of-View Limit Based on Reinforcement Learning1
Aeroservoelastic Wind Tunnel Evaluation of Preview H2 and H∞ Gust Load Alleviation1
Spherically Constrained Relative Motion Trajectories in Low Earth Orbit1
Computationally Efficient Collision-Free Trajectory Planning of Satellite Swarms Under Unmodeled Orbital Perturbations1
Decentralized Weapon–Target Assignment Under Asynchronous Communications1
Two-Stage Trajectory Planning for Autonomous Deployment and Target Capture of Space Manipulators1
Advanced Algorithms for Verification and Validation of Flexible Aircraft with Adaptive Control1
Optimal Kinetic-Impact Geometry for Asteroid Deflection Exploiting Delta-V Hodograph1
Circular Restricted n-Body Problem1
Experimental Validation of Port-Hamiltonian-Based Control for Fixed-Wing Unmanned Aircraft1
Dynamic Modeling and Distributed Control of Asymmetric Flexible Spacecraft1
Analytical Gradient-Guided Nonlinear Programming Approach for Multitarget Rendezvous Mission1
Cutting Corners: Curvilinear-Surface-Based Gravity Models for Asteroids and Comets1
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