Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements
Analytical Estimation of the Velocity Increment in J2-Perturbed Impulsive Transfers
Analytical Framework for Precise Relative Motion in Low Earth Orbits
Analytic Maneuver Sequence for Safety Ellipse Reconfigurations Using Relative Orbital Elements
Analytic Transformation Between Osculating and Mean Elements in the J2 Problem
Angles-Only Navigation to a Noncooperative Satellite Using Relative Orbital Elements
Atmospheric Interface Reentry Point Targeting Using Aerodynamic Drag Control
Autonomous Guidance for Rendezvous Phasing Based on Special-Point-Based Maneuvers
Bounded Relative Orbits in the Zonal Gravitational Field for Formation Flying
Closed-Form Approximation of Revisit Rate for Low-Altitude Satellites
Cluster Flight Algorithms for Disaggregated Satellites
Collision Probability Due to Space Debris Clouds Through a Continuum Approach
Constant, Radial Low-Thrust Problem Including First-Order Effects of J2
Designing a Reference Trajectory for Frozen Repeat Near-Equatorial Low Earth Orbits
Effects of In-Track Maneuver on the Ground Track of Near-Circular Orbits
Enabling Space-Based Computed Cloud Tomography with a Mixed Integer Linear Programming Scheduler
Equivalent Delta-V per Orbit of Gravitational Perturbations
Extended Lambert-Based Approach for Ground-Track Adjustment with Specified Overflight Altitude
Formation Establishment and Reconfiguration Using Differential Elements in J2-Perturbed Orbits