ControlThrusters#
- class ansys.stk.core.stkobjects.astrogator.ControlThrusters#
IntEnum
Overview#
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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. |
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The thruster efficiency. |
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Thruster direction defined as a vector in the body frame. Spherical azimuth value. |
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Thruster direction defined as a vector in the body frame. Spherical elevation value. |
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Thruster direction defined as a vector in the body frame. Cartesian X value. |
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Thruster direction defined as a vector in the body frame. Cartesian Y value. |
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Thruster direction defined as a vector in the body frame. Cartesian Z value. |
Import detail#
from ansys.stk.core.stkobjects.astrogator import ControlThrusters