Spacecraft.ParticleFlux(Variable, Variable, Variable) Method |
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DescriptionThe ParticleFlux method uses the NASA AP-8 and AE-8 particle flux maps to calculate the omnidirectional flux of the specified particle type with the energy level specified by minimumEnergy. The AP/AE maps contain collected data of proton and electron fluxes in the Earth's radiation belt with energy ranges from 0.04 MeV to 7 MeV for electrons and from 0.1 MeV to 400 MeV for protons. See the help file for links to more detailed documentation on the AP/AE maps. The user has the option to specify epoch and longitude offsets to include in the flux calculation.
For more detailed information on the particle flux models, please see the Goddard Space Flight Center's description here: http://ccmc.gsfc.nasa.gov/modelweb/magnetos/aeap.html
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
Arguments
Return Value
Returns the particle flux evaluated at the Spacecraft's Earth-relative position using the magnetic field model at the epoch of the flux model specified by particleType and solarActivity.
Syntax
See also Coverage and Contact Analysis Guide
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