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APPULDIS

APPULDIS

Name


  appuldis

Purpose (one Line Only)


  Find the circumstances of an appulse between a star and a solar system object

Description


  Given the ephemeris
  The approximate time of the appulse must be within +/-30 minutes or this
    will fail.

Category


  Astronomy

Calling Sequence


  appuldis,objcode,obscode,jd,ra,dec,jdmin,sep

Inputs


  objcode - Standard object code (see ephem.pro)
  obscode - Standard observatory code or a structure with the observatory
              information.
  jd - Approximate time of appulse
  ra - right ascension of the star, J2000
  dec - declination of the star, J2000

Optional Input Parameters


Keyword Input Parameters


  ET - Flag, if set, all times are in Ephemeris Time, default is UTC
              This is most important for the output. You can get away with
              inputing either.
  VERBOSE - Flag, if set, prints information about event to terminal
  STARERR - Star position uncertainty (arcsec), default is 0.050 arcsec

Outputs


  jdmin - Time of the minimum separation
  sep - Separation between star and object at jdmin (arcsec)
                If you get a negative number it means the search was not
                successful in finding a minimum near the input time.

Keyword Output Parameters


  info - Anonymous structure with auxillary information about the object
            at the time of the minimum separation.
          objname - Full name/designation of object
          jd - Time of close approach
          hv - Absolute magnitude of object
          et - Flag, set if time is ET
          minsep - separate at close approach time (arcsec)
          pa - Position angle of object wrt star at minimum separation
          sun - Heliocentric distance of object
          earth - topocentric distance of object
          phang - phase angle (degrees)
          selong - solar elongation (degrees)
          melong - lunar elongation (degrees)
          mphase - Lunar phase
          kmscale - scale on plane of sky in km/arcsec
          oam - Airmass of object at time of event
          oalt - object elevation (degrees)
          oaz - object azimuth, westward from south
          salt - solar elevation (degrees)
          malt - lunar elevation (degrees)
          speed - projected speed of object relative to the star (km/sec)
          rate - projected speed of object ralative to the star (arcsec/hr)
          diam1 - Diameter of object assuming 5% albedo (km)
          diam2 - Diameter of object assuming 30% albedo (km)
          chord1 - Maximum occultation duration assuming a 5% albedo size
          chord2 - Maximum occultation duration assuming a 30% albedo size
          angsha - Position angle of track on the plane of the sky, E of N
          etime - 1-sigma error in event time (seconds)
          etrack - 1-sigma error in cross-track position (km)
          coverage - Fraction of the 1-sigma cross track error that could
                        be covered if track is centered on network
          err - 1-sigma ephemeris uncertainty for the object at the
                      time of the close approach
          errkm - 1-sigma ephemeris uncertainty in km.

Common Blocks


Side Effects


Restrictions


Procedure


Modification History


  Written by Marc W. Buie, Southwest Research Institute, 2015/03/07
  2015/09/24, MWB, Added position angle output



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