SRPGSPM04aeIIR#
- class ansys.stk.core.stkobjects.astrogator.SRPGSPM04aeIIR#
Bases:
IComponentInfo
,ICloneable
GSPM04aeIIR SRP propagator function.
Overview#
Get or set the atmospheric altitude for eclipse. A simple model to account for some measure of attenuation that simply increases the shape of the Earth by the defined altitude height, often taken to be 23 km. Uses Distance Dimension. |
|
Get or set the shadow model type. |
|
Get or set the sun position computation. |
|
Other eclipsing bodies. |
|
True if shadow boundary mitigation should be performed; the state of the satellite after crossing a shadow boundary will be corrected for errors possibly caused by the sudden change in SRP which occurred during the integration step. |
|
True if solar radius should come from the Sun.cb file. |
|
Get or set the solar radius value to use in eclipse calculations. Uses Distance Dimension. |
Import detail#
from ansys.stk.core.stkobjects.astrogator import SRPGSPM04aeIIR
Property detail#
- property SRPGSPM04aeIIR.atmosphere_altitude: float#
Get or set the atmospheric altitude for eclipse. A simple model to account for some measure of attenuation that simply increases the shape of the Earth by the defined altitude height, often taken to be 23 km. Uses Distance Dimension.
- property SRPGSPM04aeIIR.shadow_model: ShadowModel#
Get or set the shadow model type.
- property SRPGSPM04aeIIR.sun_position: SunPosition#
Get or set the sun position computation.
- property SRPGSPM04aeIIR.eclipsing_bodies: CentralBodyComponentCollection#
Other eclipsing bodies.
- property SRPGSPM04aeIIR.include_boundary_mitigation: bool#
True if shadow boundary mitigation should be performed; the state of the satellite after crossing a shadow boundary will be corrected for errors possibly caused by the sudden change in SRP which occurred during the integration step.