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True longitude

  • Elliptical Orbits

    Elliptical Orbits

  • Moon-Earth-Sun: the Oldest Three-Body Problem

    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*

    A Series Solution for Some Periodic Orbits in the Restricted Three-Body Problem According to the Perturbation Method*

  • Orbital Mechanics Course Notes

    Orbital Mechanics Course Notes

  • Low Thrust Orbit Transfer Optimiser for a Spacecraft Simulator (Espss -Ecosimpro® European Space Propulsion System Simulation)

    Low Thrust Orbit Transfer Optimiser for a Spacecraft Simulator (Espss -Ecosimpro® European Space Propulsion System Simulation)

  • 1980: Solar Ephemeris Algorithm

    1980: Solar Ephemeris Algorithm

  • 1 CHAPTER 10 COMPUTATION of an EPHEMERIS 10.1 Introduction

    1 CHAPTER 10 COMPUTATION of an EPHEMERIS 10.1 Introduction

  • An Adaptive Groundtrack Maintenance Scheme For

    An Adaptive Groundtrack Maintenance Scheme For

  • Positional Astronomy : Earth Orbit Around Sun

    Positional Astronomy : Earth Orbit Around Sun

  • Low-Thrust Many-Revolution Trajectory Optimization

    Low-Thrust Many-Revolution Trajectory Optimization

  • Mean Motions and Longitudes in Indian Astronomy

    Mean Motions and Longitudes in Indian Astronomy

  • Keplerian Orbits and Dynamics of Exoplanets

    Keplerian Orbits and Dynamics of Exoplanets

  • High-Accuracy Orbital Dynamics Simulation Through Keplerian and Equinoctial Parameters

    High-Accuracy Orbital Dynamics Simulation Through Keplerian and Equinoctial Parameters

  • Planetary Orbital Equations in Externally-Perturbed Systems

    Planetary Orbital Equations in Externally-Perturbed Systems

  • Analytical Representation for Ephemeris with Short Time-Span : Application to the Longitude of Titan Xiaojin Xi

    Analytical Representation for Ephemeris with Short Time-Span : Application to the Longitude of Titan Xiaojin Xi

  • Heliospheric Coordinate Systems

    Heliospheric Coordinate Systems

  • Nonlinear Orbit Control with Longitude Tracking

    Nonlinear Orbit Control with Longitude Tracking

  • An Advanced N-Body Model for Interacting Multiple Stellar Systems

    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


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