Enabling Space-Based Computed Cloud Tomography with a Mixed Integer Linear Programming Scheduler
Extended Lambert-Based Approach for Ground-Track Adjustment with Specified Overflight Altitude
Orbital Impulsive Pursuit–Evasion Game Formulation and Stackelberg Equilibrium Solutions
Analytic Transformation Between Osculating and Mean Elements in the J2 Problem
Stable Nonlinear Feedback Control Using Quaternionic Orbital Elements
Spacecraft Relative Motion Dynamics and Control Using Fundamental Modal Solution Constants
Ground Track Control Using Differential Drag for Small Earth Observation Satellite Constellations
Novel Orbit Control Approach for Earth Observation with Multiple Targets
Designing a Reference Trajectory for Frozen Repeat Near-Equatorial Low Earth Orbits
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective
Analytical Estimation of the Velocity Increment in J2-Perturbed Impulsive Transfers
Analytic Maneuver Sequence for Safety Ellipse Reconfigurations Using Relative Orbital Elements
Satellite Swarm Reconfiguration Planning Based on Surrogate Models
Saddle Point of Orbital Pursuit-Evasion Game Under -Perturbed Dynamics
Analytical Framework for Precise Relative Motion in Low Earth Orbits
In-Plane Formation Reconfiguration with Radial Maneuvers
Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements
Impulsive Control of Earth Satellites on Low-Eccentricity Kolmogorov–Arnold–Moser Tori
Locally Geostationary Orbits: Optimal Geometry of Elliptic Orbit for Earth Coverage
Bounded Relative Orbits in the Zonal Gravitational Field for Formation Flying
Spacecraft Fast Fly-Around Formations Design Using the Bi-Teardrop Configuration
New Solution for Rendezvous Between Geosynchronous Satellites Using Low Thrust
Relative Reachable Domain for Spacecraft with Initial State Uncertainties
Route Satellite Constellations for Earth Discontinuous Coverage and Optimal Solution Peculiarities
Nonlinear Analytical Uncertainty Propagation for Relative Motion near -Perturbed Elliptic Orbits
Equivalent Delta-V per Orbit of Gravitational Perturbations
Constant, Radial Low-Thrust Problem Including First-Order Effects of J2
Quadratically Constrained Least Squares with Aerospace Applications
Sensor Allocation for Tracking Geosynchronous Space Objects
Invariant Manifold and Bounds of Relative Motion Between Heliocentric Displaced Orbits
Iterative Pseudostate Method for Transfer Trajectory Design of Interplanetary Orbiter Missions
Atmospheric Interface Reentry Point Targeting Using Aerodynamic Drag Control
Optimal Servicing of Geostationary Satellites Considering Earth’s Triaxiality and Lunisolar Effects
Collision Probability Due to Space Debris Clouds Through a Continuum Approach
Homotopic Perturbed Lambert Algorithm for Long-Duration Rendezvous Optimization
Formation Establishment and Reconfiguration Using Differential Elements in J2-Perturbed Orbits
Safe Picosatellite Release from a Small Satellite Carrier
Effects of In-Track Maneuver on the Ground Track of Near-Circular Orbits
Angles-Only Navigation to a Noncooperative Satellite Using Relative Orbital Elements
Autonomous Guidance for Rendezvous Phasing Based on Special-Point-Based Maneuvers
Lambert Targeting for On-Orbit Delivery of Debris Remediation Dust
Impulsive Maneuvers for Formation Reconfiguration Using Relative Orbital Elements