Journal of Guidance Control and Dynamics

Papers
(The H4-Index of Journal of Guidance Control and Dynamics is 20. 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 2021-08-01 to 2025-08-01.)
ArticleCitations
Hybrid Zero-Effort-Miss/Zero-Effort-Velocity Guidance for Powered Descent Phase48
Distributed Least Absolute Deviations Estimation31
Aerodynamic Feedforward-Feedback Architecture for Tailsitter Control in Hybrid Flight Regimes29
Optimal Sequence-Image Construction Method for Autonomous Relative Navigation Based on Camera Offset29
Fuel-Efficient Stationkeeping of Quasi-Satellite Orbits via Convex Optimization28
Two-Stage Dynamic-Assignment Optimization Method for Multispacecraft Debris Removal28
Slew Maneuver Constraints for Agile Flexible Spacecraft27
Computationally Efficient Collision-Free Trajectory Planning of Satellite Swarms Under Unmodeled Orbital Perturbations26
Deeper Learning Needed from Machine Learning26
Discrete-Time Gyro Measurements and Covariance Analysis with Time-Correlated Biases24
Cutting Corners: Curvilinear-Surface-Based Gravity Models for Asteroids and Comets23
Robust Model Predictive Control for Proximity Operations with Experimental Demonstrations23
Three-Dimensional Path-Following Nonlinear Guidance for Unmanned Aerial Vehicles23
Experimental Validation of Port-Hamiltonian-Based Control for Fixed-Wing Unmanned Aircraft22
Centralized and Distributed Strategies for Handover-Aware Task Allocation in Satellite Constellations22
Consensus-Based Merging and Spacing Method for Aircraft Self-Separation at Intersections22
Long-Term Fuel-Optimal Collision Avoidance Maneuvers with Station-Keeping Constraints21
Analytic Gradient Computation and Applications in Multitarget Multi-Impulse Trajectory Optimization21
Initial Pole Axis and Spin Direction Estimation of Asteroids Using Infrared Imagery21
Approximate Solutions for the Non-Hamiltonian Restricted Three-Body Problem20
0.10303688049316