Journal of Guidance Control and Dynamics

Papers
(The TQCC of Journal of Guidance Control and Dynamics is 2. 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
Atmospheric Density Uncertainty Quantification for Satellite Conjunction Assessment3
Shortest Dubins Paths to Intercept a Target Moving on a Circle3
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
Implementation of a Map Relative Localization System for Planetary Landing2
Dynamics of a Nonrigid Orbital Siphon at a Near-Earth Asteroid2
Neural-Network-Based Dynamic Flight Envelop Protection Within Integrated Aircraft Control System2
Trilateration Positioning Using Hybrid Camera–LiDAR System with Spherical Landmark Surface Fitting2
Gravitational Force Model Aliasing with Nongravitational Force Coefficients in Dynamic Prediction2
Analytical State Approximation of Electric Sail with Fixed Pitch Angle2
Incremental Passive Fault-Tolerant Control for Quadrotors Subjected to Complete Rotor Failures2
Analytical Staring Attitude Control Command Generation Method for Earth Observation Satellites2
Passively Safe and Robust Multi-Agent Optimal Control with Application to Distributed Space Systems2
Landing Simulation in the Full Two-Body Problem of Binary Asteroids2
Earth–Moon L2 Quasi-Halo Orbit Family: Characteristics and Manifold Applications2
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
Plasma Detumbling of Failed Spacecraft by Using Hall Effect Thrusters2
Dynamic Soaring Under Different Atmospheric Stability Conditions2
Non-Cooperative Space Target De-Tumbling Approach Using Multiple High-Temperature Superconducting Coils2
Low-Thrust Guidance for Geocentric Transfers Using Single-Rotation-Axis Steering2
Standoff Target Tracking Using Line-of-Sight Distance Bifurcation2
Kustaanheimo–Stiefel Variables for Planetary Protection Compliance Analysis2
Autonomous Spacecraft Attitude Reorientation Using Robust Sampled-Data Control Barrier Functions2
Spacecraft Rendezvous in Closed Keplerian Orbits Using Constant Radial Thrust Acceleration2
Spacecraft Relative Motion Dynamics and Control Using Fundamental Modal Solution Constants2
Risk-Aware Path Planning for Unmanned Aerial Systems in a Spreading Wildfire2
Identity Management of Clustered Satellites with a Generalized Labeled Multi-Bernoulli Filter2
Rapid Suboptimal Low-Thrust Space Trajectory Design2
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
Optimal Reaction Wheel Disturbance Avoidance via Torque Allocation Algorithms2
Approximation of Optimal Impulsive Flyby Transfer with Terminal Inspection Constraints2
Robust Stall Spin Flight Path Control with Flight Test Validation2
Three-Dimensional Spatial–Temporal Cooperative Guidance Without Active Speed Control2
Gap Traversal Guidance Using Bearing Information2
Reachable Domain Under J2 Perturbation for Satellites with a Single Impulse2
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
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