BasicManeuverStrategyGlideProfile#

class ansys.stk.core.stkobjects.aviator.BasicManeuverStrategyGlideProfile#

Class defining the Glide profile strategy for a basic maneuver procedure.

Overview#

Methods

`set_airspeed`	Set the airspeed and airspeed type that the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled.
`set_glide_speed_control_mode`	Set the glide speed control mode and altitude.

Properties

`hold_initial_airspeed`	Select whether to maintain the airspeed of the aircraft at the beginning of the procedure throughout the maneuver.
`airspeed`	Get the airspeed the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled.
`airspeed_type`	Get the airspeed type.
`min_g`	Get or set the minimum load factor the aircraft can withstand.
`max_g`	Get or set the maximum load factor the aircraft can withstand.
`max_speed_limits`	Get or set the options of what the procedure will do if the aircraft has exceeded the maximum speed limits.
`compensate_for_coriolis_acceleration`	Get or set the option to compensate for the acceleration due to the Coriolis effect.
`powered_cruise_mode`	Get or set the powered cruise mode.
`powered_cruise_throttle`	Get or set the powered cruise throttle.
`powered_cruise_thrust_model`	Get the powered cruise thrust model.
`glide_speed_control_mode`	Get the glide speed control mode.
`glide_speed_control_altitude`	Get the glide speed altitude when using the altitude control mode.

from ansys.stk.core.stkobjects.aviator import BasicManeuverStrategyGlideProfile

property BasicManeuverStrategyGlideProfile.hold_initial_airspeed: bool#: Select whether to maintain the airspeed of the aircraft at the beginning of the procedure throughout the maneuver.

property BasicManeuverStrategyGlideProfile.airspeed: float#: Get the airspeed the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled.

property BasicManeuverStrategyGlideProfile.airspeed_type: AirspeedType#: Get the airspeed type.

property BasicManeuverStrategyGlideProfile.min_g: float#: Get or set the minimum load factor the aircraft can withstand.

property BasicManeuverStrategyGlideProfile.max_g: float#: Get or set the maximum load factor the aircraft can withstand.

property BasicManeuverStrategyGlideProfile.max_speed_limits: BasicManeuverStrategyAirspeedPerformanceLimits#: Get or set the options of what the procedure will do if the aircraft has exceeded the maximum speed limits.

property BasicManeuverStrategyGlideProfile.compensate_for_coriolis_acceleration: bool#: Get or set the option to compensate for the acceleration due to the Coriolis effect.

property BasicManeuverStrategyGlideProfile.powered_cruise_mode: BasicManeuverStrategyPoweredCruiseMode#: Get or set the powered cruise mode.

property BasicManeuverStrategyGlideProfile.powered_cruise_throttle: float#: Get or set the powered cruise throttle.

property BasicManeuverStrategyGlideProfile.powered_cruise_thrust_model: PropulsionThrust#: Get the powered cruise thrust model.

property BasicManeuverStrategyGlideProfile.glide_speed_control_mode: BasicManeuverGlideSpeedControlMode#: Get the glide speed control mode.

property BasicManeuverStrategyGlideProfile.glide_speed_control_altitude: float#: Get the glide speed altitude when using the altitude control mode.

BasicManeuverStrategyGlideProfile.set_airspeed(self, airspeed_type: AirspeedType, airspeed: float) → None#

Set the airspeed and airspeed type that the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled.

Parameters:

airspeed_type : AirspeedType

airspeed : float

Returns:

None

BasicManeuverStrategyGlideProfile.set_glide_speed_control_mode(self, glide_speed_mode: BasicManeuverGlideSpeedControlMode, control_altitude: float) → None#

Set the glide speed control mode and altitude.

Parameters:

glide_speed_mode : BasicManeuverGlideSpeedControlMode

control_altitude : float

Returns:

None