ostk.astrodynamics.event_condition.COECondition

class COECondition

Bases: pybind11_object

A COE Event Condition.

Methods

aop	Overloaded function.
argument_of_latitude	Overloaded function.
eccentric_anomaly	Overloaded function.
eccentricity	Create a COE condition based on the eccentricity.
inclination	Overloaded function.
mean_anomaly	Overloaded function.
raan	Overloaded function.
semi_major_axis	Create a COE condition based on the semi-major axis.
true_anomaly	Overloaded function.

static aop(*args, **kwargs)

Overloaded function.

1. aop(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, aop: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the argument of perigee.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. aop (EventConditionTarget): The argument of perigee. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. aop(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the argument of perigee being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static argument_of_latitude(*args, **kwargs)

Overloaded function.

1. argument_of_latitude(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, argument_of_latitude: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the argument of latitude.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. argument_of_latitude (EventConditionTarget): The argument of latitude. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. argument_of_latitude(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the argument of latitude being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static eccentric_anomaly(*args, **kwargs)

Overloaded function.

1. eccentric_anomaly(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, eccentric_anomaly: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the eccentric anomaly.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. eccentric_anomaly (EventConditionTarget): The eccentric anomaly. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. eccentric_anomaly(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the eccentric anomaly being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static eccentricity(

criterion: ostk.astrodynamics.event_condition.RealCondition.Criterion,

frame: ostk.physics.coordinate.Frame,

eccentricity: ostk.astrodynamics.EventCondition.Target,

gravitational_parameter: ostk.physics.unit.Derived,

) → ostk.astrodynamics.event_condition.RealCondition

Create a COE condition based on the eccentricity.

Parameters:

• criterion (Criterion) -- The criterion.

• frame (Frame) -- The reference frame.

• eccentricity (EventConditionTarget) -- The eccentricity.

• gravitational_parameter (Derived) -- The gravitational parameter.

Returns:

The COE condition.

Return type:

COECondition

static inclination(*args, **kwargs)

Overloaded function.

1. inclination(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, inclination: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the inclination.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. inclination (EventConditionTarget): The inclination. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. inclination(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the inclination being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static mean_anomaly(*args, **kwargs)

Overloaded function.

1. mean_anomaly(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, mean_anomaly: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the mean anomaly.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. mean_anomaly (EventConditionTarget): The mean anomaly. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. mean_anomaly(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the mean anomaly being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static raan(*args, **kwargs)

Overloaded function.

1. raan(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, raan: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the right ascension of the ascending node.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. raan (EventConditionTarget): The right ascension of the ascending node. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. raan(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the right ascension of the ascending node being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

static semi_major_axis(

criterion: ostk.astrodynamics.event_condition.RealCondition.Criterion,

frame: ostk.physics.coordinate.Frame,

semi_major_axis: ostk.astrodynamics.EventCondition.Target,

gravitational_parameter: ostk.physics.unit.Derived,

) → ostk.astrodynamics.event_condition.RealCondition

Create a COE condition based on the semi-major axis.

Parameters:

• criterion (Criterion) -- The criterion.

• frame (Frame) -- The reference frame.

• semi_major_axis (EventConditionTarget) -- The semi-major axis.

• gravitational_parameter (Derived) -- The gravitational parameter.

Returns:

The COE condition.

Return type:

COECondition

static true_anomaly(*args, **kwargs)

Overloaded function.

1. true_anomaly(criterion: ostk.astrodynamics.event_condition.AngularCondition.Criterion, frame: ostk.physics.coordinate.Frame, true_anomaly: ostk.astrodynamics.EventCondition.Target, gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the true anomaly.

   Args:

   criterion (Criterion): The criterion. frame (Frame): The reference frame. true_anomaly (EventConditionTarget): The true anomaly. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.

2. true_anomaly(frame: ostk.physics.coordinate.Frame, target_range: tuple[ostk.physics.unit.Angle, ostk.physics.unit.Angle], gravitational_parameter: ostk.physics.unit.Derived) -> ostk.astrodynamics.event_condition.AngularCondition

   Create a COE condition based on the true anomaly being within a range.

   Args:

   frame (Frame): The reference frame. target_range (tuple[Angle, Angle]): A tuple of two angles defining the range. gravitational_parameter (Derived): The gravitational parameter.

   Returns:

   COECondition: The COE condition.