simIncludeGravBody

class simIncludeGravBody.gravBodyFactory(bodyNames=None)[source]

Bases: object

Factory cass to create gravitational bodies.

createBodies(bodyNames)[source]

A convenience function to create multiple typical solar system bodies.

Parameters

bodyNames (array_like) – Planet name strings. Each planet name must be a valid SPICE celestial body string.

Returns

gravBodies – A list of gravity body objects held by the gravity factory.

Return type

array_like

createCustomGravObject(label, mu, **kwargs)[source]

Create a custom gravity body object.

Parameters
  • label (string) – Gravity body name

  • mu (double) – Gravity constant

  • kwargs

    radEquatordouble

    Equatorial radius in meters

    radiusRatiodouble

    Ratio of the polar radius to the equatorial radius.

    planetFramestring

    Name of the spice planet frame

    displayName: string

    Vizard celestial body name, if not provided then planetFrame becomes the Vizard name

    modelDictionaryKey: string

    Vizard model key name. if not set, then either the displayName or planetName is used to set the model

createEarth()[source]

Create gravity body with Earth mass properties.

createJupiter()[source]

Create gravity body with Jupiter mass properties.

createMars()[source]

Create gravity body with Mars mass properties.

createMarsBarycenter()[source]

Create gravity body with Mars mass properties.

createMercury()[source]

Create gravity body with Mercury mass properties.

createMoon()[source]

Create gravity body with Moon mass properties.

createNeptune()[source]

Create gravity body with Neptune mass properties.

createSaturn()[source]

Create gravity body with Saturn mass properties.

createSpiceInterface(path, time, **kwargs)[source]

A convenience function to configure a NAIF Spice module for the simulation. It connect the gravBodyData objects to the spice planet state messages. Thus, it must be run after the gravBodyData objects are created.

Parameters
  • path (string) – The absolute path to the Basilisk source directory (default ‘’).

  • time (string) – The time string.

  • kwargs

    spiceKernalFileNames :

    A list of spice kernel file names including file extension.

    spicePlanetNames :

    A list of planet names whose Spice data is loaded, overriding the gravBodies list.

    spicePlanetFrames :

    A list of strings for the planet frame names. If left empty for a planet, then IAU_ + planetName is assumed for the planet frame.

    epochInMsg: bool

    Flag to set an epoch input message for the spice interface

createSun()[source]

Create gravity body with sun mass properties.

createUranus()[source]

Create gravity body with Uranus mass properties.

createVenus()[source]

Create gravity body with Venus mass properties.

unloadSpiceKernels()[source]

Method to unload spice kernals at the end of a simulation.

simIncludeGravBody.loadGravFromFile(fileName, spherHarm, maxDeg=2)[source]

Load the gravitational body spherical harmonics coefficients from a file.

Parameters
  • fileName (string) – The full path to the specified data file.

  • spherHarm – The spherical harmonics container of the gravity body.

  • maxDeg (integer) – maximum degree of spherical harmonics to load

Notes

This function is a convenience utility for loading in the spherical harmonics coefficients from a data file. The default harmonic degree is 2 unless specified. Note that this function calls the gravityEffector function loadGravFromFile().

simIncludeGravBody.loadPolyFromFile(fileName, poly)[source]

Load the gravitational body spherical harmonics coefficients from a file.

Parameters
  • fileName (string) – The full path to the specified data file.

  • spherHarm – The spherical harmonics container of the gravity body.

  • maxDeg (integer) – maximum degree of spherical harmonics to load

Notes

This function is a convenience utility for loading in the spherical harmonics coefficients from a data file. The default harmonic degree is 2 unless specified. Note that this function calls the gravityEffector function loadGravFromFile().