dust Module

Mass gravitational term G * mass (units GU * MU)

Semimajor axis (pericentric distance for a parabolic orbit)

Acceleration due to post-Newtonian correction

Total heliocentric acceleration

Barycentric accelerations of bodies due to central body oblatenes

Tanngential component of acceleration of bodies due to tides

semimajor axis following perihelion passage

Mean anomaly

Longitude of ascending node

Body mass density - calculated internally (units MU / DU**3)

Eccentricity

Identifier

Inclination

Particle metadata information

Inverse heliocentric radius term (1/rh**3)

perihelion passage flag

Index array used to convert flattened the body-body comparison upper triangular matrix

flag indicating whether body has merged with another this time step

Body should be discarded

flag indicating whether body is part of an encounter this time step

Run the current step as a first

Logical mask used to select a subset of bodies when performing certain operations (drift, kick, accel, etc.)

Body mass (units MU)

G * (Mcb + [m])

Number of bodies

number of encounters with planets this time step

Number of pl-tp comparisons in the flattened upper triangular matrix

Argument of pericenter

perihelion distance

Barycentric position

Heliocentric position

An integrator-specific status indicator

Barycentric velocity

Heliocentric velocity

Compute heliocentric accelerations of massive bodies

Acceleration term arising from the post-Newtonian correction

Compute direct cross (third) term heliocentric accelerations of test particles by massive bodies

Compute the barycentric accelerations of bodies due to the oblateness of the central body

Add user-supplied heliocentric accelerations to planets

Appends elements from one structure to another

Convert test particles from barycentric to heliocentric coordinates (position and velocity)

Deallocates all allocatable arrays

Check to see if test particles should be discarded based on their positions relative to the massive bodies

Method for Danby drift in Democratic Heliocentric coordinates

Convert orbital elements to position and velocity vectors

“Fills” bodies from one object into another depending on the results of a mask (uses the UNPACK intrinsic)

Determine nbody_system pericenter passages for test particles

Position kick due to p**4 term in the post-Newtonian correction

Convert test particles from heliocentric to barycentric coordinates (position and velocity)

Kicks the barycentric velocities

Method for linear drift of massive bodies due to barycentric momentum of Sun

Converts from psudeovelocity to velocity for GR calculations using symplectic integrators

Add the generic read frame for Fortran binary files

I/O routine for writing out a single frame of time-series data for the central body

Read in body initial conditions from an ascii file

Rearranges the order of array elements of body based on an input index array. Used in sorting methods

Clean up the test particle structures to remove discarded bodies

Checks the current size of a Swiftest body against the requested size and resizes it if it is too small.

Convert test particles from heliocentric to barycentric coordinates (position only)

Saves a snapshot of the this body to the collision storage object

Sets the inverse heliocentric radius term (1/rh**3)

Method used to construct the vectorized form of the central body mass

A base constructor that sets the number of bodies and

Sorts body arrays by a sortable component

“Spills” bodies from one object to another depending on the results of a mask (uses the PACK intrinsic)

Steps the body forward one stepsize

Converts from velocity to psudeovelocity for GR calculations using symplectic integrators

Convert test particles from barycentric to heliocentric coordinates (velocity only)

Convert test particles from heliocentric to barycentric coordinates (velocity only)

I/O routine for writing out a single frame of time-series data for all bodies in the nbody_system in NetCDF format

Dump contents of particle information metadata to file

Convert position and velocity vectors to orbital elements

Mass gravitational term G * mass (units GU * MU)

Semimajor axis (pericentric distance for a parabolic orbit)

Acceleration due to post-Newtonian correction

Total heliocentric acceleration

Barycentric accelerations of bodies due to central body oblatenes

Tanngential component of acceleration of bodies due to tides

semimajor axis following perihelion passage

Mean anomaly

Longitude of ascending node

Body mass density - calculated internally (units MU / DU**3)

Eccentricity

Identifier

Inclination

Particle metadata information

Inverse heliocentric radius term (1/rh**3)

perihelion passage flag

Index array used to convert flattened the body-body comparison upper triangular matrix

flag indicating whether body has merged with another this time step

Body should be discarded

flag indicating whether body is part of an encounter this time step

level at which this particle should be moved

deepest encounter level achieved this time step

Run the current step as a first

Logical mask used to select a subset of bodies when performing certain operations (drift, kick, accel, etc.)

Body mass (units MU)

G * (Mcb + [m])

Number of bodies

number of encounters with planets this time step

Number of pl-tp comparisons in the flattened upper triangular matrix

Argument of pericenter

perihelion distance

Body radius (units DU)

Barycentric position

Heliocentric position

An integrator-specific status indicator

Barycentric velocity

Heliocentric velocity

Compute heliocentric accelerations of test particles

Acceleration term arising from the post-Newtonian correction

Compute direct cross (third) term heliocentric accelerations of test particles by massive bodies

Compute the barycentric accelerations of bodies due to the oblateness of the central body

Add user-supplied heliocentric accelerations to planets

Appends elements from one structure to another

Convert test particles from barycentric to heliocentric coordinates (position and velocity)

Deallocates all allocatable arrays

Check to see if test particles should be discarded based on their positions relative to the massive bodies

Method for Danby drift in Democratic Heliocentric coordinates. Sets the mask to the current recursion level

Convert orbital elements to position and velocity vectors

Checks if any test particles are undergoing a close encounter with a massive body

“Fills” bodies from one object into another depending on the results of a mask (uses the UNPACK intrinsic)

Determine nbody_system pericenter passages for test particles

Position kick due to p**4 term in the post-Newtonian correction

Convert test particles from heliocentric to barycentric coordinates (position and velocity)

Kicks the barycentric velocities

Method for linear drift of massive bodies due to barycentric momentum of Sun

Converts from psudeovelocity to velocity for GR calculations using symplectic integrators

Add the generic read frame for Fortran binary files

I/O routine for writing out a single frame of time-series data for the central body

Read in body initial conditions from an ascii file

Rearranges the order of array elements of body based on an input index array. Used in sorting methods

Clean up the test particle structures to remove discarded bodies

Checks the current size of a Swiftest body against the requested size and resizes it if it is too small.

Convert test particles from heliocentric to barycentric coordinates (position only)

Saves a snapshot of the this body to the collision storage object

Sets the inverse heliocentric radius term (1/rh**3)

Method used to construct the vectorized form of the central body mass

Constructor method - Allocates space for the input number of bodies

Sorts body arrays by a sortable componen

“Spills” bodies from one object to another depending on the results of a mask (uses the PACK intrinsic)

Steps the body forward one stepsize

Converts from velocity to psudeovelocity for GR calculations using symplectic integrators

Convert test particles from barycentric to heliocentric coordinates (velocity only)

Convert test particles from heliocentric to barycentric coordinates (velocity only)

I/O routine for writing out a single frame of time-series data for all bodies in the nbody_system in NetCDF format

Dump contents of particle information metadata to file

Convert position and velocity vectors to orbital elements

Mass gravitational term G * mass (units GU * MU)

Semimajor axis (pericentric distance for a parabolic orbit)

Acceleration due to post-Newtonian correction

Total heliocentric acceleration

Barycentric accelerations of bodies due to central body oblatenes

Tanngential component of acceleration of bodies due to tides

semimajor axis following perihelion passage

Mean anomaly

Longitude of ascending node

Body mass density - calculated internally (units MU / DU**3)

Eccentricity

Identifier

Inclination

Particle metadata information

Inverse heliocentric radius term (1/rh**3)

perihelion passage flag

Index array used to convert flattened the body-body comparison upper triangular matrix

flag indicating whether body has merged with another this time step

Body should be discarded

flag indicating whether body is part of an encounter this time step

Run the current step as a first

Logical mask used to select a subset of bodies when performing certain operations (drift, kick, accel, etc.)

Body mass (units MU)

G * (Mcb + [m])

Number of bodies

number of encounters with planets this time step

Number of pl-tp comparisons in the flattened upper triangular matrix

Argument of pericenter

perihelion distance

Barycentric position

Heliocentric position

An integrator-specific status indicator

Barycentric velocity

Heliocentric velocity

Compute heliocentric accelerations of test particles

Acceleration term arising from the post-Newtonian correction

Compute direct cross (third) term heliocentric accelerations of test particles by massive bodies

Compute the barycentric accelerations of bodies due to the oblateness of the central body

Add user-supplied heliocentric accelerations to planets

Appends elements from one structure to another

Convert test particles from barycentric to heliocentric coordinates (position and velocity)

Deallocates all allocatable arrays

Check to see if test particles should be discarded based on their positions relative to the massive bodies

Loop through bodies and call Danby drift routine on heliocentric variables

Convert orbital elements to position and velocity vectors

“Fills” bodies from one object into another depending on the results of a mask (uses the UNPACK intrinsic)

Determine nbody_system pericenter passages for test particles

Position kick due to p**4 term in the post-Newtonian correction

Convert test particles from heliocentric to barycentric coordinates (position and velocity)

Kick heliocentric velocities of test particles

Converts from psudeovelocity to velocity for GR calculations using symplectic integrators

Add the generic read frame for Fortran binary files

I/O routine for writing out a single frame of time-series data for the central body

Read in body initial conditions from an ascii file

Rearranges the order of array elements of body based on an input index array. Used in sorting methods

Clean up the test particle structures to remove discarded bodies

Checks the current size of a Swiftest body against the requested size and resizes it if it is too small.

Convert test particles from heliocentric to barycentric coordinates (position only)

Saves a snapshot of the this body to the collision storage object

Sets the inverse heliocentric radius term (1/rh**3)

Method used to construct the vectorized form of the central body mass

A base constructor that sets the number of bodies and

Sorts body arrays by a sortable component

“Spills” bodies from one object to another depending on the results of a mask (uses the PACK intrinsic)

Steps the particle forward one stepsize

Converts from velocity to psudeovelocity for GR calculations using symplectic integrators

Convert test particles from barycentric to heliocentric coordinates (velocity only)

Convert test particles from heliocentric to barycentric coordinates (velocity only)

I/O routine for writing out a single frame of time-series data for all bodies in the nbody_system in NetCDF format

Dump contents of particle information metadata to file

Convert position and velocity vectors to orbital elements