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two_body_ode_test:
  MATLAB/Octave version 4.2.2
  Test two_body_ode().
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INITIAL_ORBIT:
  MATLAB version
  This simulation follows a small body for two orbits
  around a relatively massive body - such as Mercury around
  the sun.
  Kepler's equations for a two body system are used.
  Note that the orbit is NOT an ellipse.  But that's OK,
  because the planet is far from its equilibrium orbit.

INITIAL_ORBIT:
  Normal end of execution.

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ORBITAL_DECAY
  MATLAB version
  This simulation follows a small body for 20 orbits
  around a relatively massive body - such as Mercury around
  the sun.
  Kepler's equations for a two body system are used.
  Initially, the orbit is NOT an ellipse, but as time passes,
  the orbit decays into an elliptical shape.

ORBITAL_DECAY:
  Normal end of execution.

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two_body_ode_test:
  Normal end of execution.

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