Journal of Guidance Control and Dynamics

(The TQCC of Journal of Guidance Control and Dynamics 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 2020-07-01 to 2024-07-01.)
Koopman-Operator-Based Attitude Dynamics and Control on SO(3)27
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture21
Convex Approach to Covariance Control with Application to Stochastic Low-Thrust Trajectory Optimization17
Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation15
Onboard Orbit Determination for Deep-Space CubeSats15
Unified Method for Field-of-View-Limited Homing Guidance15
Information-Based Guidance and Control Architecture for Multi-Spacecraft On-Orbit Inspection14
Varying-Gain Proportional Navigation Guidance for Precise Impact Time Control14
Numerical Study on Low-Velocity Impact Between Asteroid Lander and Deformable Regolith13
Image-Based Meta-Reinforcement Learning for Autonomous Guidance of an Asteroid Impactor13
Guidance Strategy for Autonomous Inspection of Unknown Non-Cooperative Resident Space Objects12
Cooperative Circular Guidance with Nonuniform Field-of-View Constraints11
Absolute Triangulation Algorithms for Space Exploration11
Global Incremental Flight Control for Agile Maneuvering of a Tailsitter Flying Wing11
Assessment of a Scalogram-Based Pilot-Induced Oscillation Metric with Flight-Test and Simulation Data11
Low-Thrust Collision Avoidance Maneuver Optimization11
Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories11
Multi-Objective Hidden Genes Genetic Algorithm for Multigravity-Assist Trajectory Optimization10
Impact Angle Guidance Using State-Dependent (Differential) Riccati Equation: Unified Applicability Analysis10
Two-Stage Dynamic-Assignment Optimization Method for Multispacecraft Debris Removal10
Robust Space Trajectory Design Using Belief Optimal Control9
Nonlinear Dynamic Inversion with Actuator Dynamics: An Incremental Control Perspective9
Hierarchical Reinforcement Learning Approach for Autonomous Cross-Country Soaring9
Nonlinear Optimal Guidance for Intercepting Stationary Targets with Impact-Time Constraints9
Adaptive Neural-Network-Based Unscented Kalman Filter for Robust Pose Tracking of Noncooperative Spacecraft9
Atlas of Optimal Low-Thrust Rephasing Solutions in Circular Orbit9
UAV Collision Avoidance Using Mixed-Integer Second-Order Cone Programming9
Analytical State Propagation for Continuous-Thrust Linear Relative Motion8
Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint8
Dynamics Near the Three-Body Libration Points via Koopman Operator Theory8
Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight8
Flexible Spacecraft Vibration Suppression by Distributed Actuators8
Relative Navigation Strategy About Unknown and Uncooperative Targets7
Analytical Costate Estimation by a Reference Trajectory-Based Least-Squares Method7
Uniform Satellite Constellation Reconfiguration7
Incremental Passive Fault-Tolerant Control for Quadrotors Subjected to Complete Rotor Failures7
Multistep Newton–Picard Method for Nonlinear Differential Equations7
Efficient Event-Based Adaptive Sliding Mode Control for Spacecraft Attitude Stabilization7
Cooperative Circular Guidance of Multiple Missiles: A Practical Prescribed-Time Consensus Approach6
Equinoctial Lyapunov Control Law for Low-Thrust Rendezvous6
Neuro-Adaptive Prescribed Performance Control for Aerial-Recovery Drogue with Actuator Constraints6
Geometrical Analysis of Station-Keeping Strategies About Libration Point Orbits6
Harmonic Decomposition Models of Flapping-Wing Flight for Stability Analysis and Control Design6
Encirclement of Moving Targets Using Noisy Range and Bearing Measurements6
Hybrid Gaussian Mixture Splitting Techniques for Uncertainty Propagation in Nonlinear Dynamics6
Linear Quadratic Guidance Laws with Intercept Angle Constraints and Varying Speed Adversaries6
Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex–Concave Decomposition6
Tackling Nonconvex Collision Avoidance Constraints for Optimal Trajectory Planning Using Saturation Functions6
Fast Model Predictive Control for Spacecraft Rendezvous and Docking with Obstacle Avoidance6
Novel Orbit Control Approach for Earth Observation with Multiple Targets6
Hierarchical Four-Dimensional Trajectories Planning Method for Manned and Unmanned Aircraft Integrated Airspace6
Designing Sun–Earth L2 Halo Orbit Stationkeeping Maneuvers via Reinforcement Learning6
Integrated Control of Continuum-Manipulator Space Robots with Actuator Saturation and Disturbances5
Optimization of Low-Thrust Rendezvous Between Circular Orbits via Thrust-Switch Strategy5
Minimum Effort Pursuit Guidance with Multiple Delayed Engagement Decisions5
Analysis of an Unmanned Underwater Vehicle Propulsion Model for Motion Control5
Dynamic Modeling and Attitude Control of Large-Scale Flexible Parallel Multibody Spacecraft5
Factorized Partial-Update Schmidt–Kalman Filter5
Direct Solution of the Keplerian State Transition Matrix5
Collision Probability of Debris Clouds Based on Higher-Order Boundary Value Problems5
Maneuverability Set Estimation and Trajectory Feasibility Evaluation for eVTOL Aircraft5
Directional State Transition Tensors for Capturing Dominant Nonlinear Effects in Orbital Dynamics5
Three-Dimensional Spatial–Temporal Cooperative Guidance Without Active Speed Control5
Semianalytical Measures of Nonlinearity Based on Tensor Eigenpairs5
Null-Space-Excitation-Based Adaptive Control for an Overactuated Hexacopter Model5
Tube-Based Model Predictive Control with Uncertainty Identification for Autonomous Spacecraft Maneuvers5
Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique5
Closed-Loop, Exact-Time, Minimum-Energy Attitude Control with Analytic Gain Selection5
Minimum Power Control Allocation for Incremental Control of Over-Actuated Transition Aircraft5
Reachable Domain Under J2 Perturbation for Satellites with a Single Impulse5
Gust Load Alleviation Using Reduced-Order Aeroelastic Models and Observer-Based Robust Control5
Improved Neural Adaptive Control for Nonlinear Oscillatory Dynamic of Flapping Wings4
Composite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around Asteroids4
Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints4
Use of Statistical Linearization for Nonlinear Least-Squares Problems in Pulsar Navigation4
Laboratory Experimentation of Spacecraft Robotic Capture Using Deep-Reinforcement-Learning–Based Guidance4
Cooperative Multilift Slung Load Transportation Using Haptic Admittance Control Guidance4
Cascaded Lyapunov Vector Fields for Acceleration-Constrained Spacecraft Path Planning4
Autonomous Spacecraft Rendezvous Using Tube-Based Model Predictive Control: Design and Application4
Existence of Infinitely Many Optimal Iso-Impulse Trajectories in Two-Body Dynamics4
Shortest Dubins Paths to Intercept a Target Moving on a Circle4
Prescribed Performance-Based Fixed-Time Adaptive Control Allocation for Overactuated Spacecraft4
Propellant-Optimal Powered Descent Guidance Revisited4
Nonlinear Guidance Law for Target Enclosing with Arbitrary Smooth Shapes4
Relative Dynamics and Station-Keeping Strategy of Satellite–Sail Transverse Formation4
Fast Analysis of Multi-Asteroid Exploration Mission Using Multiple Electric Sails4
Worst-Case Analysis of Complex Nonlinear Flight Control Designs Using Deep Q-Learning4
Non-Cooperative Space Target De-Tumbling Approach Using Multiple High-Temperature Superconducting Coils4
Fourier Pseudospectral Method for Trajectory Optimization with Stability Requirements4
Cooperative Estimation and Guidance Strategy Using Bearings-Only Measurements4
Exploiting Scaling Constants to Facilitate the Convergence of Indirect Trajectory Optimization Methods4
Fast Homotopy for Spacecraft Rendezvous Trajectory Optimization with Discrete Logic4
Analytical Gradient-Guided Nonlinear Programming Approach for Multitarget Rendezvous Mission3
Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets3
Spacecraft Attitude Reorientation with Reaction Wheel Assembly via State-Dependent Coefficient Parameterizations3
Station-Keeping of L2 Halo Orbits Under Sampled-Data Model Predictive Control3
Range-Based Relative Navigation for a Swarm of Centimeter-Scale Femto-Spacecraft3
Kustaanheimo–Stiefel Variables for Planetary Protection Compliance Analysis3
Asteroid Flyby Cycler Trajectory Design Using Deep Neural Networks3
Wavelet Transform-Based Aircraft System Identification3
Vortex Ring State Avoidance Control Scheme Design for Nonlinear Autonomous Helicopter3
Resident Space Object Characterization Using Polarized Light Curves3
Solving Perturbed Dynamic Systems Using Schur Decomposition3
Trajectory Optimization and Control of a Free-Floating Two-Arm Humanoid Robot3
Neural-Network-Based Dynamic Flight Envelop Protection Within Integrated Aircraft Control System3
Integrating Nonlinear Controllability into a Multidisciplinary Design Process3
Passively Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systems3
Longitudinal Flight Control Law Design with Integrated Envelope Protection3
Computing Natural Transitions Between Tori Near Resonances in the Earth–Moon System3
Plasma Detumbling of Failed Spacecraft by Using Hall Effect Thrusters3
Generalized Triangle Guidance for Safeguarding Target Using Barrier Lyapunov Function3
Unwinding-Free Fast Finite-Time Sliding Mode Satellite Attitude Tracking Control3
Fault-Tolerant Optimal Spacecraft Attitude Maneuver: An Incremental Model Approach3
Nonholonomic Reorientation of Free-Flying Space Robots Using Parallelogram Actuation in Joint Space3
Optimal Trajectory Design Accounting for Robust Stability of Path-Following Controller3
Dynamics of a Nonrigid Orbital Siphon at a Near-Earth Asteroid3
Resource-Constrained Constellation Scheduling for Rendezvous and Servicing Operations3
Generalized Analysis of Biased Proportional Navigation Guidance with Fractional Power Error Feedback3
Sequential Convex Programming Using Augmented Lagrange Multiplier Method and Concave–Convex Decomposition3
Dynamic Soaring Under Different Atmospheric Stability Conditions3
In-Wing Pressure Measurements for Airspeed and Airflow Angle Estimation and High Angle-of-Attack Flight3
Command Governors with Inexact Optimization and Without Invariance3
Dynamic Programming and Model Predictive Control Approach for Autonomous Landings3
Atmospheric Density Uncertainty Quantification for Satellite Conjunction Assessment3
Spacecraft Rendezvous Using Constant-Magnitude Low Thrust3
Load Alleviation of Flexible Aircraft by Dynamic Control Allocation3