BasicManeuverStrategyLoop#

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

Bases: IBasicManeuverStrategy

Class defining the loop strategy for a basic maneuver procedure.

Overview#

set_airspeeds

Set the speeds at the top and bottom of the loop.

loop_angle

Get or set the loop angle for maneuver. The total change in pitch angle the aircraft flies.

loop_angle_mode

Get or set the loop angle mode for the maneuver.

top_load_factor

Get or set the load factor at the top of the loop.

bottom_load_factor

Get or set the load factor at the bottom of the loop.

hold_init_tas

Get or set the option to hold the initial true airspeed.

airspeed_type

Get the airspeed type.

top_airspeed

Get the speed at the top of the loop.

bottom_airspeed

Get the speed at the bottom of the loop.

Import detail#

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

Property detail#

property BasicManeuverStrategyLoop.loop_angle: Any#

Get or set the loop angle for maneuver. The total change in pitch angle the aircraft flies.

property BasicManeuverStrategyLoop.loop_angle_mode: AngleMode#

Get or set the loop angle mode for the maneuver.

property BasicManeuverStrategyLoop.top_load_factor: float#

Get or set the load factor at the top of the loop.

property BasicManeuverStrategyLoop.bottom_load_factor: float#

Get or set the load factor at the bottom of the loop.

property BasicManeuverStrategyLoop.hold_init_tas: bool#

Get or set the option to hold the initial true airspeed.

property BasicManeuverStrategyLoop.airspeed_type: AirspeedType#

Get the airspeed type.

property BasicManeuverStrategyLoop.top_airspeed: float#

Get the speed at the top of the loop.

property BasicManeuverStrategyLoop.bottom_airspeed: float#

Get the speed at the bottom of the loop.

Method detail#

BasicManeuverStrategyLoop.set_airspeeds(self, airspeed_type: AirspeedType, top_airspeed: float, bottom_airspeed: float) None#

Set the speeds at the top and bottom of the loop.

Parameters:

airspeed_type : AirspeedType

top_airspeed : float

bottom_airspeed : float

Returns:

None