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Astronomy Engine (C#)

This is the complete programming reference for the C# version of Astronomy Engine. Other programming languages are supported. See the home page for more info.


Quick Start

To get started quickly, here are some examples.


Contents


Topic Index

Position of Sun, Moon, and planets

Function Description
HelioVector Calculates vector with respect to the center of the Sun.
GeoVector Calculates vector with respect to the center of the Earth.
Equator Calculates right ascension and declination.
EquatorialToEcliptic Converts J2000 equatorial coordinates to J2000 ecliptic coordinates.
EclipticLongitude Calculates ecliptic longitude of a body in the J2000 system.
Horizon Calculates horizontal coordinates (azimuth, altitude) for a given observer on the Earth.
LongitudeFromSun Calculates a body's apparent ecliptic longitude difference from the Sun, as seen by an observer on the Earth.

Rise, set, and culmination times

Function Description
SearchRiseSet Finds time of rise or set for a body as seen by an observer on the Earth.
SearchHourAngle Finds when body reaches a given hour angle for an observer on the Earth. Hour angle = 0 finds culmination, the highest point in the sky.

Moon phases

Function Description
MoonPhase Determines the Moon's phase expressed as an ecliptic longitude.
SearchMoonPhase Finds the next instance of the Moon reaching a specific ecliptic longitude separation from the Sun.
SearchMoonQuarter Finds the first quarter moon phase after a given date and time.
NextMoonQuarter Finds the next quarter moon phase after a previous one that has been found.

Eclipses

Function Description
SearchLunarEclipse Search for the first lunar eclipse after a given date.
NextLunarEclipse Continue searching for more lunar eclipses.

Lunar perigee and apogee

Function Description
SearchLunarApsis Finds the next perigee or apogee of the Moon after a specified date.
NextLunarApsis Given an already-found apsis, finds the next perigee or apogee of the Moon.

Planet perihelion and aphelion

Function Description
SearchPlanetApsis Finds the next perihelion or aphelion of a planet after a specified date.
NextPlanetApsis Given an already-found apsis, finds the next perihelion or aphelion of a planet.

Visual magnitude and elongation

Function Description
Illumination Calculates visual magnitude and phase angle of bodies as seen from the Earth.
SearchPeakMagnitude Searches for the date and time Venus will next appear brightest as seen from the Earth.
AngleFromSun Returns full angle seen from Earth between body and Sun.
Elongation Calculates ecliptic longitude angle between a body and the Sun, as seen from the Earth.
SearchMaxElongation Searches for the next maximum elongation event for Mercury or Venus that occurs after the given date.

Oppositions and conjunctions

Function Description
SearchRelativeLongitude Finds oppositions and conjunctions of planets.

Equinoxes, solstices, and apparent solar motion

Function Description
SearchSunLongitude Finds the next time the Sun reaches a specified apparent ecliptic longitude in the true equator of date system.
Seasons Finds the equinoxes and solstices for a given calendar year.
SunPosition Calculates the Sun's apparent ecliptic coordinates as seen from the Earth.

Coordinate transforms

The following four orientation systems are supported. Astronomy Engine can convert a vector from any of these orientations to any of the others. It also allows converting from a vector to spherical (angular) coordinates and back, within a given orientation. Note the 3-letter codes for each of the orientation systems; these are used in function and type names.

  • EQJ = Equatorial J2000: Uses the Earth's equator on January 1, 2000, at noon UTC.
  • EQD = Equator of-date: Uses the Earth's equator on a given date and time, adjusted for precession and nutation.
  • ECL = Ecliptic: Uses the mean plane of the Earth's orbit around the Sun. The x-axis is referenced against the J2000 equinox.
  • HOR = Horizontal: Uses the viewpoint of an observer at a specific location on the Earth at a given date and time.
Function Description
RotateVector Applies a rotation matrix to a vector, yielding a vector in another orientation system.
InverseRotation Given a rotation matrix, finds the inverse rotation matrix that does the opposite transformation.
CombineRotation Given two rotation matrices, returns a rotation matrix that combines them into a net transformation.
VectorFromSphere Converts spherical coordinates to Cartesian coordinates.
SphereFromVector Converts Cartesian coordinates to spherical coordinates.
VectorFromEquator Given angular equatorial coordinates, calculates equatorial vector.
EquatorFromVector Given an equatorial vector, calculates equatorial angular coordinates.
VectorFromHorizon Given apparent angular horizontal coordinates, calculates horizontal vector.
HorizonFromVector Given a vector in horizontal orientation, calculates horizontal angular coordinates.
Rotation_EQD_EQJ Calculates a rotation matrix from equatorial of-date (EQD) to equatorial J2000 (EQJ).
Rotation_EQD_ECL Calculates a rotation matrix from equatorial of-date (EQD) to ecliptic J2000 (ECL).
Rotation_EQD_HOR Calculates a rotation matrix from equatorial of-date (EQD) to horizontal (HOR).
Rotation_EQJ_EQD Calculates a rotation matrix from equatorial J2000 (EQJ) to equatorial of-date (EQD).
Rotation_EQJ_ECL Calculates a rotation matrix from equatorial J2000 (EQJ) to ecliptic J2000 (ECL).
Rotation_EQJ_HOR Calculates a rotation matrix from equatorial J2000 (EQJ) to horizontal (HOR).
Rotation_ECL_EQD Calculates a rotation matrix from ecliptic J2000 (ECL) to equatorial of-date (EQD).
Rotation_ECL_EQJ Calculates a rotation matrix from ecliptic J2000 (ECL) to equatorial J2000 (EQJ).
Rotation_ECL_HOR Calculates a rotation matrix from ecliptic J2000 (ECL) to horizontal (HOR).
Rotation_HOR_EQD Calculates a rotation matrix from horizontal (HOR) to equatorial of-date (EQD).
Rotation_HOR_EQJ Calculates a rotation matrix from horizontal (HOR) to J2000 equatorial (EQJ).
Rotation_HOR_ECL Calculates a rotation matrix from horizontal (HOR) to ecliptic J2000 (ECL).