ReferenceStateWeightOnWheelsOptions#
- class ansys.stk.core.stkobjects.aviator.ReferenceStateWeightOnWheelsOptions#
Class defining the Weight on Wheels options for a Reference State procedure.
Overview#
Set the longitudinal acceleration. |
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Set the lateral acceleration. |
Get or set the aircraftβs speed relative to the ground. |
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Get the true airspeed acceleration. |
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Get the groundspeed acceleration. |
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Get the mode to specify the longitudinal acceleration. |
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Get or set the direction the aircraft is pointing. |
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Opt whether to specify the heading using magnetic North. |
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Get the heading rate of change. |
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Get the course rate of change. |
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Get the mode to specify the lateral acceleration. |
Import detail#
from ansys.stk.core.stkobjects.aviator import ReferenceStateWeightOnWheelsOptions
Property detail#
- property ReferenceStateWeightOnWheelsOptions.groundspeed: float#
Get or set the aircraftβs speed relative to the ground.
- property ReferenceStateWeightOnWheelsOptions.groundspeed_dot: float#
Get the groundspeed acceleration.
- property ReferenceStateWeightOnWheelsOptions.longitudinal_acceleration_type: ReferenceStateLongitudinalAccelerationMode#
Get the mode to specify the longitudinal acceleration.
- property ReferenceStateWeightOnWheelsOptions.heading: Any#
Get or set the direction the aircraft is pointing.
- property ReferenceStateWeightOnWheelsOptions.heading_is_magnetic: bool#
Opt whether to specify the heading using magnetic North.
- property ReferenceStateWeightOnWheelsOptions.lateral_acceleration_type: ReferenceStateLateralAccelerationMode#
Get the mode to specify the lateral acceleration.
Method detail#
- ReferenceStateWeightOnWheelsOptions.set_longitudinal_acceleration(self, accel_type: ReferenceStateLongitudinalAccelerationMode, value: float) None #
Set the longitudinal acceleration.