IsothermalHelio:

Path: Thermal/ThermalAnalysis

% Isothermal model in heliocentric orbit.
 Calculates the temperature derivative.
--------------------------------------------------------------------------
   Form:
   tempDot	= IsothermalHelio( qECIToBody, nEclipse, mass, heat, temp, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   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)

   -------
   Outputs
   -------
   tempDot   (1,1) Temperature derivative (deg-K/s)

--------------------------------------------------------------------------

Children:

Common: Quaternion/QForm
Math: Linear/Dot
Math: Linear/Mag

Back to the Thermal Module page