Пример #1
0
def determine_satellite_visibility(sat, gs, gs_tz, gs_start, gs_end, night):
    satnum = sat[0]
    saturl = "http://www.celestrak.com/cgi-bin/TLE.pl?CATNR=%s" % satnum
    st = SatelliteTle(satnum, tle_url=saturl)

    [suntimes, pentimes, umtimes] = st.compute_sun_times(gs_start, gs_end)

    ic = InviewCalculator(gs, st)
    inviews = ic.compute_inviews(gs_start, gs_end)

    intersections = []
    for inview in inviews:
        i1 = intersect_times(night, inview)
        if (i1 is not None):
            #print_span(gs_tz, i1)
            for suntime in suntimes:
                i2 = intersect_times(i1, suntime)
                if (i2 is not None):
                    #print_span(gs_tz, i2)
                    i2startmjd = Time(i2[0]).mjd
                    href = "http://www.heavens-above.com/passdetails.aspx?lat=%f&lng=%f&loc=%s&alt=%f&tz=%s&satid=%d&mjd=%f" % \
                        (gs.get_latitude(), gs.get_longitude(), gs.get_name(), gs.get_elevation_in_meters(), gs.get_tz().localize(datetime(i2[0].year, i2[0].month, i2[0].day)).tzname(), satnum, i2startmjd)
                    intersections.append([
                        "<a href=%s>%s (mag:%s) %s %s-%s%s</a>" %
                        (href, satnum, sat[1], st.get_satellite_name(),
                         st.get_launch_year(), st.get_launch_year_number(),
                         st.get_launch_piece()), i2
                    ])

    #print_debug_times(gs_tz, satnum, night, suntimes, inviews)
    return intersections
def main():
    """Main function... makes 'forward declarations' of helper functions unnecessary"""
    # Constants
    satnum = 25544 # ISS = 25544
    saturl="http://www.celestrak.com/NORAD/elements/stations.txt"
    our_tzname = 'US/Eastern'

    # Times we need
    now = datetime.now()
    our_tz = timezone(our_tzname)
    our_today_start = our_tz.localize(datetime(now.year, now.month, now.day, \
                                               0, 0, 0))
    our_today_end = our_tz.localize(datetime(now.year, now.month, now.day, \
                                             23, 59, 59))

    st = SatelliteTle(satnum, tle_url=saturl)
    tables = st.compute_sun_times(our_today_start, our_today_end)
    print_sun_times_table(st, our_today_start, our_today_end, tables)
Пример #3
0
def main():
    """Main function... makes 'forward declarations' of helper functions unnecessary"""
    parser = argparse.ArgumentParser()
    parser.add_argument("-s", "--satnum", help="Specify satellite number (e.g. 25544=ISS, 43852=STF-1)", \
            type=int, metavar="[1-99999]", choices=range(1,99999), default=43852)
    parser.add_argument("-t",
                        "--time",
                        help="Specify date/time (UTC)",
                        type=ArgValidator.validate_datetime,
                        metavar="YYYY-MM-DDTHH:MM:SS",
                        default=datetime.now())
    parser.add_argument("-r", "--endtime", help="Specify date time range with this end date/time (UTC)", \
            type=ArgValidator.validate_datetime, metavar="YYYY-MM-DDTHH:MM:SS", default=None)
    parser.add_argument("-d", "--timestep", help="Specify time step (delta) in seconds for tabular data", \
            type=int, metavar="[1-86400]", choices=range(1,86400), default=60)
    parser.add_argument("-p",
                        "--tle",
                        help="Print TLE information",
                        action="store_true")
    parser.add_argument("-u",
                        "--sun",
                        help="Print sun/umbra/penumbra information",
                        action="store_true")
    parser.add_argument("-e",
                        "--ecef",
                        help="Print ECEF ephemeris",
                        action="store_true")
    parser.add_argument("-i",
                        "--eci",
                        help="Print ECI ephemeris",
                        action="store_true")
    parser.add_argument(
        "-l",
        "--lla",
        help=
        "Print latitude, longitude, altitude (geodetic degrees, altitude in km above WGS-84 ellipsoid) ephemeris",
        action="store_true")
    parser.add_argument(
        "-f",
        "--file",
        help="TLE file to use (instead of looking up the TLE on CelesTrak)",
        type=ArgValidator.validate_file,
        default=None)
    parser.add_argument("-m",
                        "--mag",
                        help="Print geomagnetic data",
                        action="store_true")
    parser.add_argument("-a",
                        "--aer",
                        help="Print az/el/range from ground station",
                        action="store_true")
    parser.add_argument("-x", "--longitude", help="Specify longitude (degrees) of ground station", \
            type=float, default=-79.825518056)
    parser.add_argument("-y", "--latitude", help="Specify latitude (degrees) of ground station", \
            type=float, default=38.43685028)
    parser.add_argument("-z", "--elevation", help="Specify elevation (meters) of ground station", \
            type=float, default=842.0)
    parser.add_argument("-v",
                        "--iirv",
                        help="Print improved interrange vector (IIRV) format",
                        action="store_true")
    args = parser.parse_args()

    if (args.file is not None):
        st = SatelliteTle(args.satnum, tle_file=args.file)
    else:
        saturl = "http://www.celestrak.com/cgi-bin/TLE.pl?CATNR=%s" % args.satnum
        st = SatelliteTle(args.satnum, tle_url=saturl)

    if (args.tle):
        print_tle_data(st)

    if (args.eci):
        if (args.endtime is None):
            point = st.compute_ephemeris_point(args.time)
            print_ephemeris_point(st, point)
        else:
            table = st.compute_ephemeris_table(args.time, args.endtime,
                                               args.timestep)
            print_ephemeris_table(st, table)

    if (args.ecef):
        #print "ECEF is not implemented"
        if (args.endtime is None):
            point = st.compute_ephemeris_point(args.time)
            print_ephemeris_point(st, point, False)
        else:
            table = st.compute_ephemeris_table(args.time, args.endtime,
                                               args.timestep)
            print_ephemeris_table(st, table, False)

    if (args.lla):
        if (args.endtime is None):
            llap = st.compute_lonlatalt_point(args.time)
            print_lonlatalt(st, llap)
        else:
            table = st.compute_lonlatalt_table(args.time, args.endtime,
                                               args.timestep)
            print_lonlatalt_table(st, table)

    if (args.mag):
        if (args.endtime is None):
            llap = st.compute_lonlatalt_point(args.time)
            print_mag(st, llap)
        else:
            table = st.compute_lonlatalt_table(args.time, args.endtime,
                                               args.timestep)
            print_mag_table(st, table)

    if (args.aer):
        gs = GroundStation(lat=args.latitude,
                           lon=args.longitude,
                           el_meters=args.elevation)
        ic = InviewCalculator(gs, st)
        if (args.endtime is None):
            args.endtime = args.time
        azels = ic.compute_azels(args.time, args.endtime, args.timestep)
        print_azelrange_table(azels)

    if (args.sun):
        if (args.endtime is None):
            sun_state = st.get_satellite_sun_state(args.time)
            if (sun_state == st.InSun):
                in_sun = "in sun"
            elif (sun_state == st.InPenumbra):
                in_sun = "in penumbra"
            else:
                in_sun = "in umbra"
            print("===== SUN =====")
            print("Satellite is %s" % in_sun)
        else:
            tables = st.compute_sun_times(args.time, args.endtime)
            print_sun_times_table(st, args.time, args.endtime, tables)

    if (args.iirv):
        if (args.endtime is None):
            point = st.compute_ephemeris_point(args.time)
            print_iirv_point(st, point)
        else:
            table = st.compute_ephemeris_table(args.time, args.endtime,
                                               args.timestep)
            print_iirv_points(st, table)