Spacecraft.FOVInterference(Star, Variable, Variable, Sensor) Method

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Description

Returns the time of entry into an area of interference, the time of exit from the area of interference, and the duration of interference. Interference is defined to be the period when both an object of interest and an interfering object are within the field-of-view of a Spacecraft sensor, and the interfering object lies within a user-specified cone about the Spacecraft to object-of-interest vector.

 

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

 

Note: This is an interval method. See the Interval Methods page for more information.

Note: This method has a state. See the Methods and Properties with State page for more information.

 

Method Signature

Spacecraft.FOVInterference(

Star objectOfInterest,


Variable interferenceObject,


Variable coneAngle,


Sensor sensor)

 

 

Arguments

objectOfInterest


Description:

The Star object in which the calling Spacecraft's sensor is interested. An element of a StarField object can be specified, i.e. myStarField[0].

 

 

interferenceObject


Description:

The CelestialObject that will impose interference on the calling Spacecraft's sensor if it is positioned such that it meets the criteria above. The CelestialObject is specified by a numeric ID. Body ID's 1-11 are assigned to the default Solar System objects, as shown below. Custom CelestialObjects will have body ID's starting at 12 and assigned in the order they are created.

Valid Values:

Celestial Object

Value

Mercury

Mercury.BodyID or 1

Venus

Venus.BodyID or 2

Earth

Earth.BodyID or 3

Mars

Mars.BodyID or 4

Jupiter

Jupiter.BodyID or 5

Saturn

Saturn.BodyID or 6

Uranus

Uranus.BodyID or 7

Neptune

Neptune.BodyID or 8

Pluto

Pluto.BodyID or 9

Moon

Moon.BodyID or 10

Sun

Sun.BodyID or 11

<Custom CelestialBody>

<Custom CelestialBody>.BodyID, starting at 12 and assigned in the order the custom CelestialObjects are created.

 

 

 

coneAngle


Description:

This is the half angle of the cone in degrees for which the interference is determined.

Units:

deg

Valid Range:

-360 ≤ coneAngle ≤ 360

 

 

sensor


Description:

Sensor to consider when evaluating interference.

 

 

 

Return Value

Type:

string

 

 

Returns the Calendar time of entry into an area of interference, the time of exit from the area of interference, and the duration of interference.

 

The FF_Preferences.IntervalEventReportingBehavior property controls whether the start and end of propagation are reported as events. By default, if the interference starts before the beginning of the propagation span, FreeFlyer will label the start of the propagation as the start of the interference. If the interference extends past the end of the propagation span, FreeFlyer labels the end of propagation as the end of the interference.

 

Syntax

myString1 = mySpacecraft1.FOVInterference(myStar1, myVariable1, myVariable2, mySensor1);

 

 

See also

Spacecraft Object

Spacecraft.FOVInterference

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide