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Argumentation
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keywords:(Argumentation)
Angles-Only Navigation to a Noncooperative Satellite Using Relative Orbital Elements
Spacecraft Relative Motion Dynamics and Control Using Fundamental Modal Solution Constants
Multispacecraft Refueling Optimization Considering the Perturbation and Window Constraints
Locally Geostationary Orbits: Optimal Geometry of Elliptic Orbit for Earth Coverage
Atmospheric Interface Reentry Point Targeting Using Aerodynamic Drag Control
Bounded Relative Orbits in the Zonal Gravitational Field for Formation Flying
Satellite Swarm Reconfiguration Planning Based on Surrogate Models
Designing a Reference Trajectory for Frozen Repeat Near-Equatorial Low Earth Orbits
Cluster Flight Algorithms for Disaggregated Satellites
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective
Ground Track Control Using Differential Drag for Small Earth Observation Satellite Constellations
Novel Orbit Control Approach for Earth Observation with Multiple Targets
Analytic Transformation Between Osculating and Mean Elements in the J2 Problem
Optimal Servicing of Geostationary Satellites Considering Earth’s Triaxiality and Lunisolar Effects
Relative Reachable Domain for Spacecraft with Initial State Uncertainties
New Solution for Rendezvous Between Geosynchronous Satellites Using Low Thrust
Constant, Radial Low-Thrust Problem Including First-Order Effects of J2