AttitudeProfileYawToNadir#

class ansys.stk.core.stkobjects.AttitudeProfileYawToNadir#

Bases: IVehicleAttitudeProfile

A profile useful for satellites with highly elliptical orbits.

Overview#

inertial

Get the body-fixed Z axis is fixed in inertial space using the selected coordinate type. The X axis is then constrained, via motion in the yaw sense about the body-fixed Z axis, toward the nadir direction.

Import detail#

from ansys.stk.core.stkobjects import AttitudeProfileYawToNadir

Property detail#

property AttitudeProfileYawToNadir.inertial: IDirection#

Get the body-fixed Z axis is fixed in inertial space using the selected coordinate type. The X axis is then constrained, via motion in the yaw sense about the body-fixed Z axis, toward the nadir direction.