Description
Returns the angle between the reference-to-target vector and the x-y plane of the reference object in the GroundVehicle body frame.
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.
Method Signature
GroundVehicle.Elevation(
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Variable celestialBodyIdentifier)
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Arguments
celestialBodyIdentifier
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Description:
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The numerical identifier of the target celestial body to be used in the elevation 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 Range:
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celestialBodyIdentifier ≥ 0
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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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Return Value
Returns the elevation angle of the argument as seen from the reference object.
Syntax
myVariable1 = myGroundVehicle1.Elevation(myVariable2);
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See also
GroundVehicle Object
GroundVehicle.Elevation
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