示例#1
0
def magnSatRing(JD, lon, lat):
    """Compute the apparent visual magnitude of Saturn's rings.
    
    Args:
      JD (float):   Julian Day (days).
      lon (float):  Geocentric ecliptical longitude of Saturn (rad).
      lat (float):  Geocentric ecliptical latitude of Saturn (rad).
    
    Returns:
      float:  magnSatRing: Apparent visual magnitude of the planet.
    
    References:
      - [Explanatory Supplement to the Astronomical Almanac 3rd Ed, Table 10.6, p.413 +
        errata](https://aa.usno.navy.mil/publications/docs/exp_supp.php)
    
    Note:
      - This is a simplified expression, which uses phi instead of Delta U.  The mean absolute deviation from
        the full expression: is 0.014m, the maximum deviation found: 0.041m in 10^5 trials, over the last 5000
        years.

    """

    tJC = dt.jd2tjc(JD)  # Time since 2000 in Julian centuries

    incl = 0.49  # Inclination of Saturn's rotation axis (rad)
    ascNod = 2.96 + 0.024 * tJC  # Ascending node of Saturn's orbit (rad)

    sinB = np.sin(incl) * np.cos(lat) * np.sin(lon - ascNod) - np.cos(
        incl) * np.sin(lat)
    magnSatRing = -2.60 * abs(sinB) + 1.25 * (sinB)**2

    return magnSatRing
示例#2
0
def precessHip(jd, ra,dec):
    """Compute precession in equatorial coordinates from the Hipparcos equinox (J2000) to that of the specified JD.
    
    Arguments:
      jd (float):   Julian day (days).
      ra (float):   Right ascension (rad).
      dec (float):  Declination (rad).
    
    Returns:
      tuple (float,float): tuple containing (raTarget, decTarget):
    
        - raNew (float):   Right ascension for the target equinox (rad).
        - decNew (float):  Declination for the target equinox (rad).
    
    """
    
    tJC  = dt.jd2tjc(jd)  # Time in Julian centuries since J2000.0
    tJC2 = tJC**2
    tJC3 = tJC*tJC2
    
    zeta  = (2306.2181*tJC + 0.30188*tJC2 + 0.017998*tJC3)*as2r
    z     = (2306.2181*tJC + 1.09468*tJC2 + 0.018203*tJC3)*as2r
    theta = (2004.3109*tJC - 0.42665*tJC2 - 0.041833*tJC3)*as2r
    
    raNew  = (np.arctan2( np.sin(ra + zeta) * np.cos(dec),  np.cos(ra + zeta) * m.cos(theta) * np.cos(dec) - m.sin(theta) * np.sin(dec) ) + z) % pi2
    decNew = np.arcsin( np.cos(ra + zeta) * m.sin(theta) * np.cos(dec)  +  m.cos(theta) * np.sin(dec) )
    
    return raNew,decNew
示例#3
0
def properMotion(startJD,targetJD, ra,dec, pma,pmd):
    """Compute the proper motion from startJD to targetJD for the given positions and proper motions.
    
    Arguments:
      startJD (float):   Julian day of the initial epoch (days).
      targetJD (float):  Julian day of the target epoch (days).
    
      ra (float):        Right ascension (numpy array, rad).
      dec (float):       Declination (numpy array, rad).
    
      pma (float):       Proper motion in right ascension (numpy array, rad/yr).
      pmd (float):       Proper motion in declination (numpy array, rad/yr).

    Returns:
      tuple (float,float): tuple containing (raTarget, decTarget):
    
        - raTarget (float):   Right ascension for the target epoch (rad).
        - decTarget (float):  Declination for the target epoch (rad).

    """
    
    dtYr   = (targetJD - startJD)/365.25
    raTarget  = ra  + pma*dtYr / np.cos(dec)
    decTarget = dec + pmd*dtYr
    
    return raTarget,decTarget
示例#4
0
def par2horiz(ha,dec, phi):
    """Convert parallactic coordinates to horizontal.

    Arguments:
      ha (float):   Hour angle (rad).
      dec (float):  Declination (rad).
      phi (float):  Geographical latitude (rad, N>0).
    
    Returns:
      tuple (float,float): tuple containing (az, alt):
    
        - az (float):   Azimuth (rad, S=0).
        - alt (float):  Altitude (rad).
    
    """
    
    az  = np.arctan2( np.sin(ha),   np.cos(ha) * m.sin(phi) - np.tan(dec) * m.cos(phi) ) % pi2
    alt = np.arcsin(  np.sin(dec) * m.sin(phi) + np.cos(ha) * np.cos(dec) * m.cos(phi) )
    
    return az,alt
示例#5
0
def eq2ecl(ra,dec, eps):
    """
    Convert equatorial coordinates to ecliptical.

    Arguments:
      ra (float):   Right ascension (rad).
      dec (float):  Declination (rad).
      eps (float):  Obliquity of the ecliptic (rad).
    
    Returns:
      tuple (float,float): tuple containing (lon, lat):
    
        - lon (float):  Ecliptical longitude (rad).
        - lat (float):  Ecliptical latitude (rad).
    
    """
    
    lon = np.arctan2( np.sin(ra)  * m.cos(eps) + np.tan(dec) * m.sin(eps),  np.cos(ra) ) % pi2
    lat =  np.arcsin( np.sin(dec) * m.cos(eps) - np.cos(dec) * m.sin(eps) * np.sin(ra) )
    
    return lon,lat
示例#6
0
def ecl2eq(lon,lat, eps):
    """Convert (geocentric) spherical ecliptical coordinates to spherical equatorial coordinates.
    
    Arguments:
      lon (float):  Ecliptical longitude (rad).
      lat (float):  Ecliptical latitude (rad).
      eps (float):  Obliquity of the ecliptic (rad).
    
    Returns:
      tuple (float,float): tuple containing (ra, dec):
    
        - ra (float):   Right ascension (rad).
        - dec (float):  Declination (rad).
    
    References:
      - [Explanatory Supplement to the Astronomical Almanac 3rd Ed,
        Eq.14.43](https://aa.usno.navy.mil/publications/docs/exp_supp.php)

    """
    
    ra  = np.arctan2( np.sin(lon) * np.cos(eps)  -  np.tan(lat) * np.sin(eps),  np.cos(lon) ) % pi2
    dec =  np.arcsin( np.sin(lat) * np.cos(eps)  +  np.cos(lat) * np.sin(eps) * np.sin(lon) )
    
    return ra,dec