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Princeton Satellite Systems

Tag: orbits

  • Artemis: From Gateway to Low Lunar Orbit

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    by

    Michael Paluszek
    in

    One concept Gateway may be in a polar orbit with an apolune of 70,000 km and perilune of 3,000 km. One concept is for the lander and Orion to meet at Gateway. Our alternative is for Artemis to stay in a low lunar orbit and be met there by Orion, the cargo transfer vehicle and…

  • Lunar Cube Module for 2016.1

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    by

    Michael Paluszek
    in ,

    We are adding the Lunar Cube Module in 2016.1 to our CubeSat Toolbox for MATLAB! It allows users to analyze and simulateCubeSats in lunar transfer and lunar orbit. It includes a new dynamical model for CubeSats that includes: Earth, Moon and Sun gravity based on the JPL ephemerides Spherical harmonic lunar gravity model Reaction wheels…