This Xcos block computes temperature, pressure and atmosphere dencity using US76 atmospheric model.
This Xcos block computes temperature, pressure and atmosphere dencity using US76 atmospheric model. It has a single input accepting altitude information in meters. Three outputs (counting from top) provide temperature [K], pressure [Pa] and density [kg/m^3] information for given altitude. The US76 atmospheric model can be used for altitudes up to 1000 km. Negative altitude values are enforced to 0.
Input: Altitude [m] (1xN)
Output 1: Kinetic temperature [K] (1xN)
Output 2: Pressure [Pa] (1xN)
Output 3: Density [kg/m^3] (1xN)
Accept herited events (0/1) - If 1 the block will accept herited events, if 0 it will have its own event input.
This example can be found under: {Aerospace Toolbox}/help/en_US/US76_atm_model.xcos
macros/US76_ATM_MODEL.sci
macros/AB_mod_atmUS76.sci