HillsDisturb:

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  Disturbances in Hills frame. Includes uncertainty.

   Since version 7.
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  Form:
  aHills = HillsDisturb( jD, r, v, rH, vH )
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  ------
  Inputs:
  -------
  jD        (1)   
  r        (3,1)  reference position in ECI frame (km)
  v        (3,1)  reference velocity in ECI frame (km/s)
  rH       (3,1)  relative position between the spacecraft (km)
  rH       (3,1)  relative position between the spacecraft (km)

  -------
  Outputs:
  --------
  aDiff     (3,1)  sum of all the terms (m/s/s)

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Children:

AeroUtils: AtmosphericCalculations/AtmDens1
Math: Linear/Cross
Math: Linear/Mag
Orbit: OrbitMechanics/APlanet
SC: Ephem/MoonV1
SC: Ephem/SunV1