Aerospace Toolbox

Maps functionality from the MATLAB Aerospace Toolbox to equivalent(s) in Julia.

Related Julia packages

ReferenceFrameRotations.jl

Data Import

`datcomimport` Bring DATCOM file into MATLAB environment

Coordinate Systems

Axes Transformations

`angle2dcm` Convert rotation angles to direction cosine matrix

`angle2quat` Convert rotation angles to quaternion

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2angle` Create rotation angles from direction cosine matrix

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`quat2angle` Convert quaternion to rotation angles

`dcm2alphabeta` Convert direction cosine matrix to angle of attack and sideslip angle

`dcm2latlon` Convert direction cosine matrix to geodetic latitude and longitude

`dcm2quat` Convert direction cosine matrix to quaternion

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`dcmbody2wind` Convert angle of attack and sideslip angle to direction cosine matrix

`dcmecef2ned` Convert geodetic latitude and longitude to direction cosine matrix

`dcmeci2ecef` Convert Earth-centered inertial (ECI) to Earth-centered Earth-fixed (ECEF) coordinates

`quat2dcm` Convert quaternion to direction cosine matrix

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`ecef2lla` Convert Earth-centered Earth-fixed (ECEF) coordinates to geodetic coordinates

`eci2lla` Convert Earth-centered inertial (ECI) coordinates to latitude, longitude, altitude (LLA) geodetic coordinates

`flat2lla` Convert from flat Earth position to array of geodetic latitude, longitude, and altitude coordinates

`lla2ecef` Convert geodetic coordinates to Earth-centered Earth-fixed (ECEF) coordinates

`lla2eci` Convert geodetic latitude, longitude, altitude (LLA) coordinates to Earth-centered inertial (ECI) coordinates

`lla2flat` Convert from geodetic latitude, longitude, and altitude to flat Earth position

`geoc2geod` Convert geocentric latitude to geodetic latitude

`geod2geoc` Convert geodetic latitude to geocentric latitude

`angle2quat` Convert rotation angles to quaternion

`dcm2quat` Convert direction cosine matrix to quaternion

`quat2angle` Convert quaternion to rotation angles

`quat2dcm` Convert quaternion to direction cosine matrix

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2quat` Convert Euler-Rodrigues vector to quaternion

`eci2aer` Convert Earth-centered inertial (ECI) coordinates to azimuth, elevation, slant range (AER) coordinates

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`rod2quat` Convert Euler-Rodrigues vector to quaternion

Flight Parameters and Quaternion Math

`airspeed` Airspeed from velocity

`alphabeta` Incidence and sideslip angles

`correctairspeed` Convert from one of other two airspeeds to equivalent airspeed (EAS), calibrated airspeed (CAS), or true airspeed (TAS)

`dpressure` Compute dynamic pressure using velocity and density

`machnumber` Compute Mach number using velocity and speed of sound

`rrdelta` Compute relative pressure ratio

`rrsigma` Compute relative density ratio

`rrtheta` Compute relative temperature ratio

`quatconj` Calculate conjugate of quaternion

`quatdivide` Divide quaternion by another quaternion

`quatexp` Exponential of quaternion

`quatinterp` Quaternion interpolation between two quaternions

`quatinv` Calculate inverse of quaternion

`quatlog` Natural logarithm of quaternion

`quatmod` Calculate modulus of quaternion

`quatmultiply` Calculate product of two quaternions

`quatnorm` Calculate norm of quaternion

`quatnormalize` Normalize quaternion

`quatpower` Power of quaternion

`quatrotate` Rotate vector by quaternion

Unit Conversions

`aEROREadieRsdatA` File containing current International Astronomical Union (IAU) 2000A Earth orientation data

`convacc` Convert from acceleration units to desired acceleration units

`convang` Convert from angle units to desired angle units

`convangacc` Convert from angular acceleration units to desired angular acceleration units

`convangvel` Convert from angular velocity units to desired angular velocity units

`convdensity` Convert from density units to desired density units

`convforce` Convert from force units to desired force units

`convlength` Convert from length units to desired length units

`convmass` Convert from mass units to desired mass units

`convpres` Convert from pressure units to desired pressure units

`convtemp` Convert from temperature units to desired temperature units

`convvel` Convert from velocity units to desired velocity units

`Deltaut1` Calculate difference between Coordinated Universal Time (UTC) and Principal Universal Time (UT1)

`decyear` Decimal year calculator

`juliandate` Julian date calculator

`leapyear` Determine leap year

`mjuliandate` Modified Julian date calculator

`tdbjuliandate` terrConvert from Barycentric Dynamical Time Estimate to Julian date

Environment

`aeroDataPackage` Start Add-On Explorer to download, install, or uninstall aerospace-specific data

`atmoscira` Use COSPAR International Reference Atmosphere 1986 model

`atmoscoesa` Use 1976 COESA model

`atmoshwm` Implement horizontal wind model

`atmosisa` Use International Standard Atmosphere model

`atmoslapse` Use Lapse Rate Atmosphere model

`atmosnonstd` Use climatic data from MIL-STD-210 or MIL-HDBK-310

`atmosnrlmsise00` Implement mathematical representation of 2001 United States Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere

`atmospalt` Calculate pressure altitude based on ambient pressure

`earthNutation` Implement Earth nutation

`moonLibration` Moon librations

`planetEphemeris` Position and velocity of astronomical objects

`geocradius` Convert from geocentric latitude to radius of ellipsoid planet

`geoidegm96` Calculate geoid height as determined from EGM96 Geopotential Model

`geoidheight` Calculate geoid height

`gravitycentrifugal` Implement centrifugal effect of planetary gravity

`gravitysphericalharmonic` Implement spherical harmonic representation of planetary gravity

`gravitywgs84` Implement 1984 World Geodetic System (WGS84) representation of Earth's gravity

`gravityzonal` Implement zonal harmonic representation of planetary gravity

`igrfmagm` Calculate Earth magnetic field and secular variation using International Geomagnetic Reference Field

`wrldmagm` Use World Magnetic Model

Gas Dynamics

`flowfanno` Fanno line flow relations

`flowisentropic` Isentropic flow ratios

`flownormalshock` Normal shock relations

`flowprandtlmeyer` Calculate Prandtl-Meyer functions for expansion waves

`flowrayleigh` Rayleigh line flow relations

Visualize Trajectory and Attitude

Axes Transformations

`angle2dcm` Convert rotation angles to direction cosine matrix

`angle2quat` Convert rotation angles to quaternion

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2angle` Create rotation angles from direction cosine matrix

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`quat2angle` Convert quaternion to rotation angles

`angle2dcm` Convert rotation angles to direction cosine matrix

`dcm2alphabeta` Convert direction cosine matrix to angle of attack and sideslip angle

`dcm2latlon` Convert direction cosine matrix to geodetic latitude and longitude

`dcm2quat` Convert direction cosine matrix to quaternion

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`dcmbody2wind` Convert angle of attack and sideslip angle to direction cosine matrix

`dcmecef2ned` Convert geodetic latitude and longitude to direction cosine matrix

`dcmeci2ecef` Convert Earth-centered inertial (ECI) to Earth-centered Earth-fixed (ECEF) coordinates

`quat2dcm` Convert quaternion to direction cosine matrix

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`ecef2lla` Convert Earth-centered Earth-fixed (ECEF) coordinates to geodetic coordinates

`eci2lla` Convert Earth-centered inertial (ECI) coordinates to latitude, longitude, altitude (LLA) geodetic coordinates

`flat2lla` Convert from flat Earth position to array of geodetic latitude, longitude, and altitude coordinates

`lla2ecef` Convert geodetic coordinates to Earth-centered Earth-fixed (ECEF) coordinates

`lla2eci` Convert geodetic latitude, longitude, altitude (LLA) coordinates to Earth-centered inertial (ECI) coordinates

`lla2flat` Convert from geodetic latitude, longitude, and altitude to flat Earth position

`geoc2geod` Convert geocentric latitude to geodetic latitude

`geod2geoc` Convert geodetic latitude to geocentric latitude

`angle2quat` Convert rotation angles to quaternion

`dcm2quat` Convert direction cosine matrix to quaternion

`quat2angle` Convert quaternion to rotation angles

`quat2dcm` Convert quaternion to direction cosine matrix

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2quat` Convert Euler-Rodrigues vector to quaternion

`eci2aer` Convert Earth-centered inertial (ECI) coordinates to azimuth, elevation, slant range (AER) coordinates

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`rod2quat` Convert Euler-Rodrigues vector to quaternion

Flight Simulator Interfaces

`aero.FlightGearAnimation` Construct FlightGear animation object

MATLAB Based Animation

`aero.Animation` Visualize aerospace animation

`aero.Body` Create body object for use with animation object

`aero.Camera` Construct camera object for use with animation object

`aero.Geometry` Construct 3-D geometry for use with animation object

Virtual Reality Animation

`aero.Node` Create node object for use with virtual reality animation

`aero.Viewpoint` Create viewpoint object for use in virtual reality animation

`aero.VirtualRealityAnimation` Construct virtual reality animation object

Julia for MATLAB Users/Index/Toolboxes/Aerospace Toolbox

Aerospace Toolbox

Related Julia packages

Data Import

datcomimport Bring DATCOM file into MATLAB environment

Coordinate Systems

Axes Transformations

angle2dcm Convert rotation angles to direction cosine matrix

angle2quat Convert rotation angles to quaternion

angle2rod Convert rotation angles to Euler-Rodrigues vector

dcm2angle Create rotation angles from direction cosine matrix

rod2angle Convert Euler-Rodrigues vector to rotation angles

quat2angle Convert quaternion to rotation angles

dcm2alphabeta Convert direction cosine matrix to angle of attack and sideslip angle

dcm2latlon Convert direction cosine matrix to geodetic latitude and longitude

dcm2quat Convert direction cosine matrix to quaternion

dcm2rod Convert direction cosine matrix to Euler-Rodrigues vector

dcmbody2wind Convert angle of attack and sideslip angle to direction cosine matrix

dcmecef2ned Convert geodetic latitude and longitude to direction cosine matrix

dcmeci2ecef Convert Earth-centered inertial (ECI) to Earth-centered Earth-fixed (ECEF) coordinates

quat2dcm Convert quaternion to direction cosine matrix

rod2dcm Convert Euler-Rodrigues vector to direction cosine matrix

ecef2lla Convert Earth-centered Earth-fixed (ECEF) coordinates to geodetic coordinates

eci2lla Convert Earth-centered inertial (ECI) coordinates to latitude, longitude, altitude (LLA) geodetic coordinates

flat2lla Convert from flat Earth position to array of geodetic latitude, longitude, and altitude coordinates

lla2ecef Convert geodetic coordinates to Earth-centered Earth-fixed (ECEF) coordinates

lla2eci Convert geodetic latitude, longitude, altitude (LLA) coordinates to Earth-centered inertial (ECI) coordinates

lla2flat Convert from geodetic latitude, longitude, and altitude to flat Earth position

geoc2geod Convert geocentric latitude to geodetic latitude

geod2geoc Convert geodetic latitude to geocentric latitude

angle2quat Convert rotation angles to quaternion

dcm2quat Convert direction cosine matrix to quaternion

quat2angle Convert quaternion to rotation angles

quat2dcm Convert quaternion to direction cosine matrix

quat2rod Convert quaternion to Euler-Rodrigues vector

rod2quat Convert Euler-Rodrigues vector to quaternion

eci2aer Convert Earth-centered inertial (ECI) coordinates to azimuth, elevation, slant range (AER) coordinates

angle2rod Convert rotation angles to Euler-Rodrigues vector

dcm2rod Convert direction cosine matrix to Euler-Rodrigues vector

quat2rod Convert quaternion to Euler-Rodrigues vector

rod2angle Convert Euler-Rodrigues vector to rotation angles

rod2dcm Convert Euler-Rodrigues vector to direction cosine matrix

rod2quat Convert Euler-Rodrigues vector to quaternion

Flight Parameters and Quaternion Math

airspeed Airspeed from velocity

alphabeta Incidence and sideslip angles

correctairspeed Convert from one of other two airspeeds to equivalent airspeed (EAS), calibrated airspeed (CAS), or true airspeed (TAS)

dpressure Compute dynamic pressure using velocity and density

machnumber Compute Mach number using velocity and speed of sound

rrdelta Compute relative pressure ratio

rrsigma Compute relative density ratio

rrtheta Compute relative temperature ratio

quatconj Calculate conjugate of quaternion

quatdivide Divide quaternion by another quaternion

quatexp Exponential of quaternion

quatinterp Quaternion interpolation between two quaternions

quatinv Calculate inverse of quaternion

quatlog Natural logarithm of quaternion

quatmod Calculate modulus of quaternion

quatmultiply Calculate product of two quaternions

quatnorm Calculate norm of quaternion

quatnormalize Normalize quaternion

quatpower Power of quaternion

quatrotate Rotate vector by quaternion

Unit Conversions

aEROREadieRsdatA File containing current International Astronomical Union (IAU) 2000A Earth orientation data

convacc Convert from acceleration units to desired acceleration units

convang Convert from angle units to desired angle units

convangacc Convert from angular acceleration units to desired angular acceleration units

convangvel Convert from angular velocity units to desired angular velocity units

convdensity Convert from density units to desired density units

convforce Convert from force units to desired force units

convlength Convert from length units to desired length units

convmass Convert from mass units to desired mass units

convpres Convert from pressure units to desired pressure units

convtemp Convert from temperature units to desired temperature units

convvel Convert from velocity units to desired velocity units

Deltaut1 Calculate difference between Coordinated Universal Time (UTC) and Principal Universal Time (UT1)

decyear Decimal year calculator

juliandate Julian date calculator

`datcomimport` Bring DATCOM file into MATLAB environment

`angle2dcm` Convert rotation angles to direction cosine matrix

`angle2quat` Convert rotation angles to quaternion

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2angle` Create rotation angles from direction cosine matrix

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`quat2angle` Convert quaternion to rotation angles

`dcm2alphabeta` Convert direction cosine matrix to angle of attack and sideslip angle

`dcm2latlon` Convert direction cosine matrix to geodetic latitude and longitude

`dcm2quat` Convert direction cosine matrix to quaternion

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`dcmbody2wind` Convert angle of attack and sideslip angle to direction cosine matrix

`dcmecef2ned` Convert geodetic latitude and longitude to direction cosine matrix

`dcmeci2ecef` Convert Earth-centered inertial (ECI) to Earth-centered Earth-fixed (ECEF) coordinates

`quat2dcm` Convert quaternion to direction cosine matrix

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`ecef2lla` Convert Earth-centered Earth-fixed (ECEF) coordinates to geodetic coordinates

`eci2lla` Convert Earth-centered inertial (ECI) coordinates to latitude, longitude, altitude (LLA) geodetic coordinates

`flat2lla` Convert from flat Earth position to array of geodetic latitude, longitude, and altitude coordinates

`lla2ecef` Convert geodetic coordinates to Earth-centered Earth-fixed (ECEF) coordinates

`lla2eci` Convert geodetic latitude, longitude, altitude (LLA) coordinates to Earth-centered inertial (ECI) coordinates

`lla2flat` Convert from geodetic latitude, longitude, and altitude to flat Earth position

`geoc2geod` Convert geocentric latitude to geodetic latitude

`geod2geoc` Convert geodetic latitude to geocentric latitude

`angle2quat` Convert rotation angles to quaternion

`dcm2quat` Convert direction cosine matrix to quaternion

`quat2angle` Convert quaternion to rotation angles

`quat2dcm` Convert quaternion to direction cosine matrix

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2quat` Convert Euler-Rodrigues vector to quaternion

`eci2aer` Convert Earth-centered inertial (ECI) coordinates to azimuth, elevation, slant range (AER) coordinates

`angle2rod` Convert rotation angles to Euler-Rodrigues vector

`dcm2rod` Convert direction cosine matrix to Euler-Rodrigues vector

`quat2rod` Convert quaternion to Euler-Rodrigues vector

`rod2angle` Convert Euler-Rodrigues vector to rotation angles

`rod2dcm` Convert Euler-Rodrigues vector to direction cosine matrix

`rod2quat` Convert Euler-Rodrigues vector to quaternion

`airspeed` Airspeed from velocity

`alphabeta` Incidence and sideslip angles

`correctairspeed` Convert from one of other two airspeeds to equivalent airspeed (EAS), calibrated airspeed (CAS), or true airspeed (TAS)

`dpressure` Compute dynamic pressure using velocity and density

`machnumber` Compute Mach number using velocity and speed of sound

`rrdelta` Compute relative pressure ratio

`rrsigma` Compute relative density ratio

`rrtheta` Compute relative temperature ratio

`quatconj` Calculate conjugate of quaternion

`quatdivide` Divide quaternion by another quaternion

`quatexp` Exponential of quaternion

`quatinterp` Quaternion interpolation between two quaternions

`quatinv` Calculate inverse of quaternion

`quatlog` Natural logarithm of quaternion

`quatmod` Calculate modulus of quaternion

`quatmultiply` Calculate product of two quaternions

`quatnorm` Calculate norm of quaternion

`quatnormalize` Normalize quaternion

`quatpower` Power of quaternion

`quatrotate` Rotate vector by quaternion

`aEROREadieRsdatA` File containing current International Astronomical Union (IAU) 2000A Earth orientation data

`convacc` Convert from acceleration units to desired acceleration units

`convang` Convert from angle units to desired angle units

`convangacc` Convert from angular acceleration units to desired angular acceleration units

`convangvel` Convert from angular velocity units to desired angular velocity units

`convdensity` Convert from density units to desired density units

`convforce` Convert from force units to desired force units

`convlength` Convert from length units to desired length units

`convmass` Convert from mass units to desired mass units

`convpres` Convert from pressure units to desired pressure units

`convtemp` Convert from temperature units to desired temperature units

`convvel` Convert from velocity units to desired velocity units

`Deltaut1` Calculate difference between Coordinated Universal Time (UTC) and Principal Universal Time (UT1)

`decyear` Decimal year calculator

`juliandate` Julian date calculator

`leapyear` Determine leap year

`mjuliandate` Modified Julian date calculator

`tdbjuliandate` terrConvert from Barycentric Dynamical Time Estimate to Julian date

`aeroDataPackage` Start Add-On Explorer to download, install, or uninstall aerospace-specific data

`atmoscira` Use COSPAR International Reference Atmosphere 1986 model

`atmoscoesa` Use 1976 COESA model

`atmoshwm` Implement horizontal wind model

`atmosisa` Use International Standard Atmosphere model