ControlThrusters#

class ansys.stk.core.stkobjects.astrogator.ControlThrusters#

IntEnum

Overview#

EQUIVALENT_ON_TIME_PERCENT

The equivalent on-time percentage is a factor multiplied by the thrust. The thrust is applied continuously throughout the maneuver and is reduced by the percentage. The mass flow rate is likewise reduced.

THRUST_EFFICIENCY

The thruster efficiency.

SPHERICAL_AZIMUTH

Thruster direction defined as a vector in the body frame. Spherical azimuth value.

SPHERICAL_ELEVATION

Thruster direction defined as a vector in the body frame. Spherical elevation value.

CARTESIAN_X

Thruster direction defined as a vector in the body frame. Cartesian X value.

CARTESIAN_Y

Thruster direction defined as a vector in the body frame. Cartesian Y value.

CARTESIAN_Z

Thruster direction defined as a vector in the body frame. Cartesian Z value.

Import detail#

from ansys.stk.core.stkobjects.astrogator import ControlThrusters