Class NRLMSIS

Namespace

NominalSystems.NRLMSIS

Assembly

NominalSystems.NRLMSIS.dll

This file contains the interface between the nrlmsise library that exists in the ThirdParty folder and the C# Nominal system.

public static class NRLMSIS

Inheritance

object

NRLMSIS

Methods

GHP7(NRLMSISInputs, NRLMSISApArray, NRLMSISFlags, double)

This subroutine provides Effective Total Mass Density for output d[5] which includes contributions from "anomalous oxygen" which can affect satellite drag above 500 km. See the section "output" for additional details.

public static NRLMSISOutputs GHP7(NRLMSISInputs input, NRLMSISApArray data, NRLMSISFlags flags, double pressure)

Parameters

input NRLMSISInputs

Input parameters

data NRLMSISApArray

An array of space weather data

flags NRLMSISFlags

Flags for the model

pressure double

The pressure at this level

Returns

NRLMSISOutputs

A reference to the output parameters

GTD7(NRLMSISInputs, NRLMSISApArray, NRLMSISFlags)

Neutral Atmosphere Empircial Model from the surface to lower exosphere.

public static NRLMSISOutputs GTD7(NRLMSISInputs input, NRLMSISApArray data, NRLMSISFlags flags)

Parameters

input NRLMSISInputs

Input parameters

data NRLMSISApArray

An array of space weather data

flags NRLMSISFlags

Flags for the model

Returns

NRLMSISOutputs

A reference to the output parameters

GTD7D(NRLMSISInputs, NRLMSISApArray, NRLMSISFlags)

This subroutine provides Effective Total Mass Density for output d[5] which includes contributions from "anomalous oxygen" which can affect satellite drag above 500 km. See the section "output" for additional details.

public static NRLMSISOutputs GTD7D(NRLMSISInputs input, NRLMSISApArray data, NRLMSISFlags flags)

Parameters

input NRLMSISInputs

Input parameters

data NRLMSISApArray

An array of space weather data

flags NRLMSISFlags

Flags for the model

Returns

NRLMSISOutputs

A reference to the output parameters

GTS7(NRLMSISInputs, NRLMSISApArray, NRLMSISFlags)

This subroutine provides Effective Total Mass Density for output d[5] which includes contributions from "anomalous oxygen" which can affect satellite drag above 500 km. See the section "output" for additional details.

public static NRLMSISOutputs GTS7(NRLMSISInputs input, NRLMSISApArray data, NRLMSISFlags flags)

Parameters

input NRLMSISInputs

Input parameters

data NRLMSISApArray

An array of space weather data

flags NRLMSISFlags

Flags for the model

Returns

NRLMSISOutputs

A reference to the output parameters