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Osculating orbit

  • Low Thrust Manoeuvres to Perform Large Changes of RAAN Or Inclination in LEO

    Low Thrust Manoeuvres to Perform Large Changes of RAAN Or Inclination in LEO

  • Osculating Orbit Elements and the Perturbed Kepler Problem

    Osculating Orbit Elements and the Perturbed Kepler Problem

  • Astrodynamics

    Astrodynamics

  • Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object

    Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object

  • Orbit Determination Using Modern Filters/Smoothers and Continuous Thrust Modeling

    Orbit Determination Using Modern Filters/Smoothers and Continuous Thrust Modeling

  • Orbit Conjunction Filters Final

    Orbit Conjunction Filters Final

  • Satellite Orbits

    Satellite Orbits

  • Statistical Orbit Determination

    Statistical Orbit Determination

  • New Closed-Form Solutions for Optimal Impulsive Control of Spacecraft Relative Motion

    New Closed-Form Solutions for Optimal Impulsive Control of Spacecraft Relative Motion

  • Lecture Notes on Space Mechanics

    Lecture Notes on Space Mechanics

  • Non-Averaged Regularized Formulations As an Alternative to Semi-Analytical Orbit Propagation Methods

    Non-Averaged Regularized Formulations As an Alternative to Semi-Analytical Orbit Propagation Methods

  • A Delta-V Map of the Known Main Belt Asteroids

    A Delta-V Map of the Known Main Belt Asteroids

  • Analytical Low-Thrust Trajectory Design Using the Simplified General Perturbations Model J

    Analytical Low-Thrust Trajectory Design Using the Simplified General Perturbations Model J

  • In-Orbit Lifetime Prediction for Leo and Heo Based on Orbit Determination from Tle Data

    In-Orbit Lifetime Prediction for Leo and Heo Based on Orbit Determination from Tle Data

  • Arxiv:2004.00037V2 [Astro-Ph.EP] 26 May 2020

    Arxiv:2004.00037V2 [Astro-Ph.EP] 26 May 2020

  • Symplectic Map Description of Halley's Comet Dynamics

    Symplectic Map Description of Halley's Comet Dynamics

  • New Method and Analysis of Proximity Trajectory-Only Learned Dynamics for Small Body Gravity Fields

    New Method and Analysis of Proximity Trajectory-Only Learned Dynamics for Small Body Gravity Fields

  • Determination of Mean Atmospheric Densities from the Explorer Ix Satellite

    Determination of Mean Atmospheric Densities from the Explorer Ix Satellite

Top View
  • ISTS-2017-D-023ⅠISSFD-2017-023
  • Orbital Mechanics Third Edition
  • Relative Orbital Motion Dynamical Models for Orbits About Nonspherical Bodies
  • Reference Systems in Satellite Geodesy
  • MONITORING and MITIGATION of CLOSE PROXIMITIES in LOW EARTH ORBIT S. Aida(1)
  • Of Satemite Mition to a Lunar Orbiter
  • C 2018 by Bindu Bhargavi Jagannatha. All Rights Reserved. SPACE LOGISTICS NETWORK OPTIMIZATION with EMBEDDED PROPULSION TECHNOLOGY SELECTION
  • Spacecraft Formation Flying Control Using Mean Orbit Elements
  • 1 Chapter 13 Calculation of Orbital Elements 13.1
  • A Satellite Footprint Visualisation Tool
  • The Full Two-Body-Problem: Simulation, Analysis, and Application to the Dynamics, Characteristics, and Evolution of Binary Asteroid Systems
  • Direct Evaluation of the Earth's Gravity Anomaly Field from Orbital Analysis of Artificial Earth Satellites
  • Note on the Dynamical Evolution of C/2017 K2 PANSTARRS
  • Program Cover Design and Printing Costs Sponsored by Analytical Graphics
  • Near-Earth Objects in Earthlike Orbits
  • Symplectic Map Description of Halley's Comet Dynamics
  • 3 Newtonian Orbital Dynamics
  • Investigating Analytical and Numerical Methods to Predict Satellite Orbits Using Two-Line Element Sets Adam T


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