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Event Name: L3: Starting Cislunar - Configuring the Circular Restricted 3-body Problem
Location: Online
Date(s): Apr-4
Time: 12:00 p.m. - 1:00 p.m. (ET)
Price: Free

The Circular Restricted 3-body Problem (CR3BP) represents a medium level of model fidelity that simultaneously incorporates the gravitational effects of two massive bodies on some smaller body, like a spacecraft. This class will teach you how to use STK's Astrogator capability and the CR3BP Propagator Function to model an "Earth-Moon" CR3BP system. To do so currently requires the definition of an appropriate "circular orbit Moon," associated reference frames, and other necessary items.Upon completion of this class, you will be able to:

  • Create a custom central body
  • Create unique reference frames
  • Design a force model with the customized central bodies and reference frames