ProfileLambertProfile

class ansys.stk.core.stkobjects.astrogator.ProfileLambertProfile

Bases: IProfile, IRuntimeTypeInfoProvider

The Lambert profile.

Overview

Methods

set_target_coord_type

Select a target coordinate type.

Properties

coord_system_name	Get or set the coordinate system.
target_coordinate_type	Get the target coordinate type.
enable_second_maneuver	Enable to calculate second maneuver at destination.
target_position_x	Get or set the X component of the target position for the end of the Lambert transfer.
target_position_y	Get or set the Y component of the target position for the end of the Lambert transfer.
target_position_z	Get or set the Z component of the target position for the end of the Lambert transfer.
target_velocity_x	Get or set the X component of the target velocity for the end of the Lambert transfer.
target_velocity_y	Get or set the Y component of the target velocity for the end of the Lambert transfer.
target_velocity_z	Get or set the Z component of the target velocity for the end of the Lambert transfer.
target_semimajor_axis	Get or set the target semimajor axis for the end of the Lambert transfer.
target_eccentricity	Get or set the target eccentricity for the end of the Lambert transfer.
target_inclination	Get or set the target inclination for the end of the Lambert transfer.
target_right_ascension_of_ascending_node	Get or set the target right ascension of the ascending node for the end of the Lambert transfer.
target_argument_of_periapsis	Get or set the target argument of periapsis for the end of the Lambert transfer.
target_true_anomaly	Get or set the target true anomaly for the end of the Lambert transfer.
solution_option	Lambert solution calculation type.
time_of_flight	Get or set the time of flight between departure and arrival for the Lambert solution.
revolutions	Get or set the number of revolutions. Dimensionless.
orbital_energy	Get or set the orbital energy for the Lambert solution.
direction_of_motion	Get or set the direction of motion (long or short) for the Lambert solution.
central_body_collision_altitude_padding	Get or set the minimum altitude below which the Lambert algorithm will consider the spacecraft to have hit the central body.
enable_write_to_first_maneuver	Set this to true to write the Delta-V solution from Lambert at the start of the transfer to the linked maneuver.
first_maneuver_segment	Get or set the first maneuver segment to manipulate that occurs at the start of the transfer.
enable_write_duration_to_propagate	Set this to true to write the Lambert duration of transfer to the ‘LambertDuration’ stopping condition in the linked propagate segment.
disable_non_lambert_propagate_stop_conditions	Set this to true to disable all non-LambertDuration stopping conditions in the propagate segment.
propagate_segment	Get or set the propagate segment to manipulate that contains the transfer duration.
enable_write_to_second_maneuver	Set this to true to write the Delta-V solution from Lambert at the end of the transfer to the linked maneuver.
second_maneuver_segment	Get or set the second maneuver segment to manipulate that occurs at the end of the transfer.

Import detail

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

Property detail

property ProfileLambertProfile.coord_system_name: str

Get or set the coordinate system.

property ProfileLambertProfile.target_coordinate_type: LambertTargetCoordinateType

Get the target coordinate type.

property ProfileLambertProfile.enable_second_maneuver: bool

Enable to calculate second maneuver at destination.

property ProfileLambertProfile.target_position_x: float

Get or set the X component of the target position for the end of the Lambert transfer.

property ProfileLambertProfile.target_position_y: float

Get or set the Y component of the target position for the end of the Lambert transfer.

property ProfileLambertProfile.target_position_z: float

Get or set the Z component of the target position for the end of the Lambert transfer.

property ProfileLambertProfile.target_velocity_x: float

Get or set the X component of the target velocity for the end of the Lambert transfer.

property ProfileLambertProfile.target_velocity_y: float

Get or set the Y component of the target velocity for the end of the Lambert transfer.

property ProfileLambertProfile.target_velocity_z: float

Get or set the Z component of the target velocity for the end of the Lambert transfer.

property ProfileLambertProfile.target_semimajor_axis: float

Get or set the target semimajor axis for the end of the Lambert transfer.

property ProfileLambertProfile.target_eccentricity: float

Get or set the target eccentricity for the end of the Lambert transfer.

property ProfileLambertProfile.target_inclination: float

Get or set the target inclination for the end of the Lambert transfer.

property ProfileLambertProfile.target_right_ascension_of_ascending_node: float

Get or set the target right ascension of the ascending node for the end of the Lambert transfer.

property ProfileLambertProfile.target_argument_of_periapsis: float

Get or set the target argument of periapsis for the end of the Lambert transfer.

property ProfileLambertProfile.target_true_anomaly: float

Get or set the target true anomaly for the end of the Lambert transfer.

property ProfileLambertProfile.solution_option: LambertSolutionOptionType

Lambert solution calculation type.

property ProfileLambertProfile.time_of_flight: float

Get or set the time of flight between departure and arrival for the Lambert solution.

property ProfileLambertProfile.revolutions: int

Get or set the number of revolutions. Dimensionless.

property ProfileLambertProfile.orbital_energy: LambertOrbitalEnergyType

Get or set the orbital energy for the Lambert solution.

property ProfileLambertProfile.direction_of_motion: LambertDirectionOfMotionType

Get or set the direction of motion (long or short) for the Lambert solution.

property ProfileLambertProfile.central_body_collision_altitude_padding: float

Get or set the minimum altitude below which the Lambert algorithm will consider the spacecraft to have hit the central body.

property ProfileLambertProfile.enable_write_to_first_maneuver: bool

Set this to true to write the Delta-V solution from Lambert at the start of the transfer to the linked maneuver.

property ProfileLambertProfile.first_maneuver_segment: str

Get or set the first maneuver segment to manipulate that occurs at the start of the transfer.

property ProfileLambertProfile.enable_write_duration_to_propagate: bool

Set this to true to write the Lambert duration of transfer to the ‘LambertDuration’ stopping condition in the linked propagate segment.

property ProfileLambertProfile.disable_non_lambert_propagate_stop_conditions: bool

Set this to true to disable all non-LambertDuration stopping conditions in the propagate segment.

property ProfileLambertProfile.propagate_segment: str

Get or set the propagate segment to manipulate that contains the transfer duration.

property ProfileLambertProfile.enable_write_to_second_maneuver: bool

Set this to true to write the Delta-V solution from Lambert at the end of the transfer to the linked maneuver.

property ProfileLambertProfile.second_maneuver_segment: str

Get or set the second maneuver segment to manipulate that occurs at the end of the transfer.

Method detail

ProfileLambertProfile.set_target_coord_type(self, element_type: LambertTargetCoordinateType) → None

Select a target coordinate type.

Parameters:

element_type : LambertTargetCoordinateType

Returns:

None