Journal of Guidance Control and Dynamics

Papers
(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 2020-11-01 to 2024-11-01.)
ArticleCitations
Koopman-Operator-Based Attitude Dynamics and Control on SO(3)27
Varying-Gain Proportional Navigation Guidance for Precise Impact Time Control24
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture22
Convex Approach to Covariance Control with Application to Stochastic Low-Thrust Trajectory Optimization19
Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation18
Image-Based Meta-Reinforcement Learning for Autonomous Guidance of an Asteroid Impactor17
Onboard Orbit Determination for Deep-Space CubeSats16
Unified Method for Field-of-View-Limited Homing Guidance16
Information-Based Guidance and Control Architecture for Multi-Spacecraft On-Orbit Inspection15
Nonlinear Optimal Guidance for Intercepting Stationary Targets with Impact-Time Constraints14
Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories14
Numerical Study on Low-Velocity Impact Between Asteroid Lander and Deformable Regolith14
Guidance Strategy for Autonomous Inspection of Unknown Non-Cooperative Resident Space Objects13
Cooperative Circular Guidance with Nonuniform Field-of-View Constraints13
Absolute Triangulation Algorithms for Space Exploration13
Adaptive Neural-Network-Based Unscented Kalman Filter for Robust Pose Tracking of Noncooperative Spacecraft13
Global Incremental Flight Control for Agile Maneuvering of a Tailsitter Flying Wing13
Assessment of a Scalogram-Based Pilot-Induced Oscillation Metric with Flight-Test and Simulation Data12
Robust Space Trajectory Design Using Belief Optimal Control12
Low-Thrust Collision Avoidance Maneuver Optimization12
Three-Dimensional Spatial–Temporal Cooperative Guidance Without Active Speed Control11
Nonlinear Dynamic Inversion with Actuator Dynamics: An Incremental Control Perspective11
Atlas of Optimal Low-Thrust Rephasing Solutions in Circular Orbit11
Multi-Objective Hidden Genes Genetic Algorithm for Multigravity-Assist Trajectory Optimization10
UAV Collision Avoidance Using Mixed-Integer Second-Order Cone Programming10
Hierarchical Reinforcement Learning Approach for Autonomous Cross-Country Soaring10
Linear Quadratic Guidance Laws with Intercept Angle Constraints and Varying Speed Adversaries10
Impact Angle Guidance Using State-Dependent (Differential) Riccati Equation: Unified Applicability Analysis10
Uniform Satellite Constellation Reconfiguration10
Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint10
Two-Stage Dynamic-Assignment Optimization Method for Multispacecraft Debris Removal10
Equinoctial Lyapunov Control Law for Low-Thrust Rendezvous9
Fast Model Predictive Control for Spacecraft Rendezvous and Docking with Obstacle Avoidance9
Flexible Spacecraft Vibration Suppression by Distributed Actuators9
Optimal Tuning of Adaptive Augmenting Controller for Launch Vehicles in Atmospheric Flight9
Propellant-Optimal Powered Descent Guidance Revisited8
Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex–Concave Decomposition8
Geometrical Analysis of Station-Keeping Strategies About Libration Point Orbits8
Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints8
Dynamics Near the Three-Body Libration Points via Koopman Operator Theory8
Analytical Costate Estimation by a Reference Trajectory-Based Least-Squares Method8
Cooperative Circular Guidance of Multiple Missiles: A Practical Prescribed-Time Consensus Approach8
Analytical State Propagation for Continuous-Thrust Linear Relative Motion8
Multistep Newton–Picard Method for Nonlinear Differential Equations8
Designing Sun–Earth L2 Halo Orbit Stationkeeping Maneuvers via Reinforcement Learning8
Incremental Passive Fault-Tolerant Control for Quadrotors Subjected to Complete Rotor Failures8
Relative Navigation Strategy About Unknown and Uncooperative Targets7
Hierarchical Four-Dimensional Trajectories Planning Method for Manned and Unmanned Aircraft Integrated Airspace7
Efficient Event-Based Adaptive Sliding Mode Control for Spacecraft Attitude Stabilization7
Fault-Tolerant Optimal Spacecraft Attitude Maneuver: An Incremental Model Approach7
Tube-Based Model Predictive Control with Uncertainty Identification for Autonomous Spacecraft Maneuvers7
Tackling Nonconvex Collision Avoidance Constraints for Optimal Trajectory Planning Using Saturation Functions7
Hybrid Gaussian Mixture Splitting Techniques for Uncertainty Propagation in Nonlinear Dynamics7
Use of Statistical Linearization for Nonlinear Least-Squares Problems in Pulsar Navigation7
Dynamic Modeling and Attitude Control of Large-Scale Flexible Parallel Multibody Spacecraft7
Prescribed Performance-Based Fixed-Time Adaptive Control Allocation for Overactuated Spacecraft6
Backstepping-Based Steering Control for Spacecraft Attitude Control Using Two-Skewed Control Moment Gyroscopes6
Cooperative Estimation and Guidance Strategy Using Bearings-Only Measurements6
Switched Control Design for Quadrotor in Target Tracking with Complex Intermittent Measurements6
Harmonic Decomposition Models of Flapping-Wing Flight for Stability Analysis and Control Design6
Semianalytical Measures of Nonlinearity Based on Tensor Eigenpairs6
Novel Orbit Control Approach for Earth Observation with Multiple Targets6
Shortest Dubins Paths to Intercept a Target Moving on a Circle6
Analysis of an Unmanned Underwater Vehicle Propulsion Model for Motion Control6
Relative Dynamics and Station-Keeping Strategy of Satellite–Sail Transverse Formation6
Reachable Domain Under J2 Perturbation for Satellites with a Single Impulse6
Gust Load Alleviation Using Reduced-Order Aeroelastic Models and Observer-Based Robust Control6
Collision Probability of Debris Clouds Based on Higher-Order Boundary Value Problems6
Optimization of Low-Thrust Rendezvous Between Circular Orbits via Thrust-Switch Strategy6
Neuro-Adaptive Prescribed Performance Control for Aerial-Recovery Drogue with Actuator Constraints6
Directional State Transition Tensors for Capturing Dominant Nonlinear Effects in Orbital Dynamics6
Encirclement of Moving Targets Using Noisy Range and Bearing Measurements6
Improved Neural Adaptive Control for Nonlinear Oscillatory Dynamic of Flapping Wings6
Minimum Effort Pursuit Guidance with Multiple Delayed Engagement Decisions5
Implementation of a Map Relative Localization System for Planetary Landing5
Minimum Power Control Allocation for Incremental Control of Over-Actuated Transition Aircraft5
Factorized Partial-Update Schmidt–Kalman Filter5
Null-Space-Excitation-Based Adaptive Control for an Overactuated Hexacopter Model5
Worst-Case Analysis of Complex Nonlinear Flight Control Designs Using Deep Q-Learning5
Maneuverability Set Estimation and Trajectory Feasibility Evaluation for eVTOL Aircraft5
Non-Self-Intersecting Trajectories and Their Applications to Satellite Constellation Design and Orbital Capacity5
Autonomous Spacecraft Rendezvous Using Tube-Based Model Predictive Control: Design and Application5
Asteroid Flyby Cycler Trajectory Design Using Deep Neural Networks5
Atmospheric Density Uncertainty Quantification for Satellite Conjunction Assessment5
Integrated Control of Continuum-Manipulator Space Robots with Actuator Saturation and Disturbances5
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
Decentralized Weapon–Target Assignment Under Asynchronous Communications5
Fast Analysis of Multi-Asteroid Exploration Mission Using Multiple Electric Sails5
Generalized Triangle Guidance for Safeguarding Target Using Barrier Lyapunov Function5
Laboratory Experimentation of Spacecraft Robotic Capture Using Deep-Reinforcement-Learning–Based Guidance5
Direct Solution of the Keplerian State Transition Matrix5
Nonlinear Guidance Law for Target Enclosing with Arbitrary Smooth Shapes4
Sequential Convex Programming Using Augmented Lagrange Multiplier Method and Concave–Convex Decomposition4
Impact Angle Control Guidance Considering Seeker’s Field-of-View Limit Based on Reinforcement Learning4
Dynamic Programming and Model Predictive Control Approach for Autonomous Landings4
Three-Dimensional Nonlinear Impact Time Guidance Using Predicted Interception Point4
Unwinding-Free Fast Finite-Time Sliding Mode Satellite Attitude Tracking Control4
Resident Space Object Characterization Using Polarized Light Curves4
Optimal Trajectory Design Accounting for Robust Stability of Path-Following Controller4
Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets4
Evaluation Model and Exact Optimization Algorithm in Missile–Target Assignment4
Exploiting Scaling Constants to Facilitate the Convergence of Indirect Trajectory Optimization Methods4
Station-Keeping of L2 Halo Orbits Under Sampled-Data Model Predictive Control4
Three-Dimensional Optimal Homing Guidance Without Terminal Maneuverability Advantage4
Fast Homotopy for Spacecraft Rendezvous Trajectory Optimization with Discrete Logic4
In-Wing Pressure Measurements for Airspeed and Airflow Angle Estimation and High Angle-of-Attack Flight4
Fourier Pseudospectral Method for Trajectory Optimization with Stability Requirements4
Composite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around Asteroids4
Convex Trajectory Optimization Using Thrust Regularization4
Mass-Optimized Gravity Tractor for Asteroid Deflection4
Cooperative Multilift Slung Load Transportation Using Haptic Admittance Control Guidance4
Cascaded Lyapunov Vector Fields for Acceleration-Constrained Spacecraft Path Planning4
Range-Based Relative Navigation for a Swarm of Centimeter-Scale Femto-Spacecraft4
Kustaanheimo–Stiefel Variables for Planetary Protection Compliance Analysis4
Earth–Moon L2 Quasi-Halo Orbit Family: Characteristics and Manifold Applications4
Existence of Infinitely Many Optimal Iso-Impulse Trajectories in Two-Body Dynamics4
Command Governors with Inexact Optimization and Without Invariance4
Non-Cooperative Space Target De-Tumbling Approach Using Multiple High-Temperature Superconducting Coils4
Near-Linear Orbit Uncertainty Propagation Using the Generalized Equinoctial Orbital Elements4
Trajectory Optimization and Control of a Free-Floating Two-Arm Humanoid Robot4
Dynamic Modeling and Distributed Control of Asymmetric Flexible Spacecraft4
Neural-Network-Based Dynamic Flight Envelop Protection Within Integrated Aircraft Control System3
Spacecraft Attitude Reorientation with Reaction Wheel Assembly via State-Dependent Coefficient Parameterizations3
Computing Natural Transitions Between Tori Near Resonances in the Earth–Moon System3
Higher-Order Soft-Trust-Region-Based Sequential Convex Programming3
Passively Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systems3
Fuel-Optimal Geometric Path Planning Algorithm for Spacecraft Formation Flying3
Local Orbital Elements for the Circular Restricted Three-Body Problem3
Vortex Ring State Avoidance Control Scheme Design for Nonlinear Autonomous Helicopter3
Load Alleviation of Flexible Aircraft by Dynamic Control Allocation3
Analytical Staring Attitude Control Command Generation Method for Earth Observation Satellites3
Controllability Properties of Solar Sails3
Impact Risk of a Debris Cloud to Spacecraft3
Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles3
Autonomous Reconnaissance Trajectory Guidance at Small Near-Earth Asteroids via Reinforcement Learning3
Integrating Nonlinear Controllability into a Multidisciplinary Design Process3
Longitudinal Flight Control Law Design with Integrated Envelope Protection3
Machine-Learning-Assisted Optimization of Aircraft Trajectories Under Realistic Constraints3
Deep Reinforcement Learning Approach for Integrated Updraft Mapping and Exploitation3
Guidance and Control of Spin-Stabilized Projectiles Based on Super Twisting Algorithm3
Risk-Aware Path Planning for Unmanned Aerial Systems in a Spreading Wildfire3
Dual-Quaternion-Based Dynamics Modeling for a Rigid–Flexible Coupling Satellite3
Solving Perturbed Dynamic Systems Using Schur Decomposition3
Nonholonomic Reorientation of Free-Flying Space Robots Using Parallelogram Actuation in Joint Space3
Intersatellite Distance-Keeping Control Based on Relative Motion Geometry3
Segmented Reconstruction of Low-Acceleration Orbital Maneuvers3
Resource-Constrained Constellation Scheduling for Rendezvous and Servicing Operations3
Generalized Analysis of Biased Proportional Navigation Guidance with Fractional Power Error Feedback3
Pseudo-Drag-Free System Simulation for Bepicolombo Radio Science Using Accelerometer Data3
Dynamic Soaring Under Different Atmospheric Stability Conditions3
Plasma Detumbling of Failed Spacecraft by Using Hall Effect Thrusters3
Disturbance Observer-Based Prescribed Performance Predictive Control for Spacecraft On-Orbit Inspection3
Wavelet Transform-Based Aircraft System Identification3
Advanced Algorithms for Verification and Validation of Flexible Aircraft with Adaptive Control3
Two-Stage Trajectory Planning for Autonomous Deployment and Target Capture of Space Manipulators3
Low-Altitude Fixed-Wing Robust and Optimal Control Using a Barrier Penalty Function Method3
Spacecraft Rendezvous Using Constant-Magnitude Low Thrust3
Analytical Gradient-Guided Nonlinear Programming Approach for Multitarget Rendezvous Mission3
Dynamics of a Nonrigid Orbital Siphon at a Near-Earth Asteroid3
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