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Path: Thermal/ThermalAnalysis
% Isothermal model in heliocentric orbit.
Calculates the temperature derivative.
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Form:
tempDot = IsothermalHelio( qECIToBody, nEclipse, mass, heat, temp, d )
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Inputs
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r (3,1) Vector to sun
qECIToBody (4,1) Quaternion
nEclipse (1,1) Eclipse
mass (1,1) Mass (kg))
heat (1,1) Heat generated internally (W)
temp (1,1) Temperature (deg-K)
d (.) Data structure
.cP (1,1) Specific heat (J/kg-deg-K)
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Outputs
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tempDot (1,1) Temperature derivative (deg-K/s)
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Common: Quaternion/QForm Math: Linear/Dot Math: Linear/Mag
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