Virtual-Chief Generalization of Hill–Clohessy–Wiltshire to Elliptic Orbits
Calibration of Linearized Solutions for Satellite Relative Motion
Spacecraft Formation Flying Dynamics and Control Using the Geomagnetic Lorentz Force
Optimal Constant-Thrust Radius Change in Circular Orbit
In-Plane Motion Control of Hill–Clohessy–Wiltshire Equations by Single Input
Active Formation Flying Along an Elliptic Orbit
Linear Coupled Attitude–Orbit Control Through Aerodynamic Drag
Analytical Assessment of Short-Duration Low-Thrust Collision-Avoidance Maneuvers
Hybrid Systems Approach to Autonomous Rendezvous and Docking of an Underactuated Satellite
Small Satellite Rendezvous Using Differential Lift and Drag
Constellation Phasing with Differential Drag on Planet Labs Satellites
Analytical Derivation of Single-Impulse Maneuvers Guaranteeing Bounded Relative Motion Under
Robust and Safe -Spacecraft Swarming in Perturbed Near-Circular Orbits
Suboptimal Power-Limited Rendezvous with Fixed Docking Direction and Collision Avoidance
Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements
Elliptic Displaced Orbit Approximation with Equally Spaced Impulses
Passively Safe Spacecraft Motion Using Reachable Sets and Orbital Element Differences
Formation-Flying Momentum Exchange Control by Separate Mass
Attitude Parameter Inspired Relative Motion Descriptions for Relative Orbital Motion Control