RelativeDisturb:
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Relative disturbances for use with a relative state.
Since version 7.
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Form:
aDiff = RelativeDisturb( jD, r, v, dr, dA )
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Inputs:
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jD (1) Epoch (Julian date)
r (3,1) Reference position in ECI frame (km)
v (3,1) Reference velocity in ECI frame (km/s)
dr (3,1) Relative position between the spacecraft (km)
dA (1) Differential area between the spacecraft (m2)
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Outputs:
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aDiff (3,1) sum of all the terms (m/s/s)
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Children:
AeroUtils: AtmosphericCalculations/AtmDens1
Math: Linear/Mag
Math: Linear/Unit
SC: Ephem/SunV1
