Description
Returns the entry and exit times when celestialBodyToView enters and leaves the Spacecraft's field of view.
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Click here to see the documentation for this object in millisecond 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
Arguments
celestialBodyToView
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Description:
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The numerical indentifier of the celestial body to use in the field of view calculation. 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.
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Valid Values:
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Celestial Object
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Value
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Mercury
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Mercury.BodyID or 1
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Venus
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Venus.BodyID or 2
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Earth
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Earth.BodyID or 3
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Mars
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Mars.BodyID or 4
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Jupiter
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Jupiter.BodyID or 5
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Saturn
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Saturn.BodyID or 6
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Uranus
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Uranus.BodyID or 7
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Neptune
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Neptune.BodyID or 8
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Pluto
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Pluto.BodyID or 9
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Moon
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Moon.BodyID or 10
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Sun
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Sun.BodyID or 11
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<Custom CelestialBody>
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<Custom CelestialBody>.BodyID, starting at 12 and assigned in the order the custom CelestialObjects are created.
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EventTime
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Description:
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The time that the event occurred.
The FF_Preferences.IntervalEventReportingBehavior property controls whether the start of propagation is reported as an event. By default, if contact starts before the beginning of the propagation span, FreeFlyer will label the start of the propagation as the start of contact.
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EventType
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Description:
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The type of the event that occurred. Event Type == 1 is entry into Contact. Event Type == 2 is exit from Contact.
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Return Value
Returns the number of elements filled into EventType and EventTime arrays.
Syntax
myVariable1 = mySpacecraft1.FOVTimes(myVariable2, myTimeSpanArray1, myArray1);
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See also
Spacecraft Object
Spacecraft.FOVTimes
Spacecraft Propagation Guide
Coverage and Contact Analysis Guide
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