Analytic Approximation for Fixed-Angle Constant Thrust Trajectories via Linear Perturbation Theory
Connecting the Equinoctial Elements and Rodrigues Parameters: A New Set of Elements
Higher-Order Lambert Problem Solution Based on Differential Algebra
Near-Linear Orbit Uncertainty Propagation Using the Generalized Equinoctial Orbital Elements
Multistep Newton–Picard Method for Nonlinear Differential Equations
Initial Orbit Determination from Bearing and Range-Rate Measurements Using the Orbital Hodograph
Onboard Estimation of Mean Orbital Elements Extended to State Jumping Case
Analytical State Propagation for Continuous-Thrust Linear Relative Motion
Analytic Impulsive Maneuver Sequences for Nominal Safety Ellipse Reconfigurations
Linear Cotangential Transfers and Safe Orbits for Elliptic Orbit Rendezvous