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True longitude
Elliptical Orbits
Moon-Earth-Sun: the Oldest Three-Body Problem
A Series Solution for Some Periodic Orbits in the Restricted Three-Body Problem According to the Perturbation Method*
Orbital Mechanics Course Notes
Low Thrust Orbit Transfer Optimiser for a Spacecraft Simulator (Espss -Ecosimpro® European Space Propulsion System Simulation)
1980: Solar Ephemeris Algorithm
1 CHAPTER 10 COMPUTATION of an EPHEMERIS 10.1 Introduction
An Adaptive Groundtrack Maintenance Scheme For
Positional Astronomy : Earth Orbit Around Sun
Low-Thrust Many-Revolution Trajectory Optimization
Mean Motions and Longitudes in Indian Astronomy
Keplerian Orbits and Dynamics of Exoplanets
High-Accuracy Orbital Dynamics Simulation Through Keplerian and Equinoctial Parameters
Planetary Orbital Equations in Externally-Perturbed Systems
Analytical Representation for Ephemeris with Short Time-Span : Application to the Longitude of Titan Xiaojin Xi
Heliospheric Coordinate Systems
Nonlinear Orbit Control with Longitude Tracking
An Advanced N-Body Model for Interacting Multiple Stellar Systems
Top View
Dynamics of a Geostationary Satellite Clément Gazzino
An Analytical Solution for Multi-Revolution Transfer Trajectory with Periodic Thrust and Non-Singular Elements
1 Fast and Robust Optimization of High Fidelity Continuous
ISTS-2017-D-101ⅠISSFD-2017-101
Positional Astronomy : Earth Orbit Around Sun
4.1.4 Describing Orbits
Heliospheric Coordinate Systems
The Pulsating Indian Epicycle of the Sun
9. Orbit in Space and Coordinate Systems
Orbital Mechanics: a Learning Tool on the Main Frame
Global Trajectory Optimisation of a Space-Based Very-Long-Baseline Interferometry Mission
Semianalytic Satellite Theory
Controlling the Perturbations of Solar Radiation Pressure on the Lorentz Spacecraft
ORBITER User Manual (C) 2000-2010 Martin Schweiger 131 Is the Angle Between Reference Direction (1,0,0) (E.G
Determination of the Orbit and Dynamic Origin of Meteoroids
On the Computation of Daily-Motion in Ancient Indian Astronomy
Computational Astronomy and the Earliest Visibility of Lunar Crescent
Analysis of Delta-V Losses During Lunar Capture Sequence Using Finite Thrust