.. _msisAtmosphere: Module: msisAtmosphere ====================== Atmosphere class used to calculate temperature / density above a body using multiple models. This class is used to hold relevant atmospheric properties and to compute the density for a given set of spacecraft relative to a specified planet. Planetary parameters, including position and input message, are settable by the user. Internal support is provided for Venus, Earth, and Mars. In a given simulation, each planet of interest should have only one MsisAtmosphere model associated with it linked to the spacecraft in orbit about that body. For more information see the :download:`PDF Description `. ---- .. autodoxygenfile:: msisAtmosphere.h :project: MsisAtmosphere .. inheritance-diagram:: msisAtmosphere.h