PropagatorHPOPStaticForceModelSettings#

class ansys.stk.core.stkobjects.PropagatorHPOPStaticForceModelSettings#

Class defining static force model options for the HPOP propagator.

Overview#

satellite_mass

A value for the satellite’s mass to be used in atmospheric drag and solar radiation pressure calculations. Uses Mass Dimension.

include_relativistic_acceleration

Models the effects of general relativity in accordance with IERS Technical Note 32, IERS Conventions (2003).

Import detail#

from ansys.stk.core.stkobjects import PropagatorHPOPStaticForceModelSettings

Property detail#

property PropagatorHPOPStaticForceModelSettings.satellite_mass: float#

A value for the satellite’s mass to be used in atmospheric drag and solar radiation pressure calculations. Uses Mass Dimension.

property PropagatorHPOPStaticForceModelSettings.include_relativistic_acceleration: bool#

Models the effects of general relativity in accordance with IERS Technical Note 32, IERS Conventions (2003).