예제 #1
0
bool ScopeSim::SetDefaultPark()
{
    // By default set RA to HA
    SetAxis1Park(get_local_sidereal_time(LocationN[LOCATION_LONGITUDE].value));

    // Set DEC to 90 or -90 depending on the hemisphere
    SetAxis2Park((LocationN[LOCATION_LATITUDE].value > 0) ? 90 : -90);

    return true;
}
예제 #2
0
bool SynscanDriver::updateLocation(double latitude, double longitude, double elevation)
{
    INDI_UNUSED(elevation);

    char cmd[SYN_RES] = {0}, res[SYN_RES] = {0};
    bool IsWest = false;

    ln_lnlat_posn p1 { 0, 0 };
    lnh_lnlat_posn p2;

    LocationN[LOCATION_LATITUDE].value  = latitude;
    LocationN[LOCATION_LONGITUDE].value = longitude;
    IDSetNumber(&LocationNP, nullptr);

    if (isSimulation())
    {
        if (!CurrentDE)
        {
            CurrentDE = latitude > 0 ? 90 : -90;
            CurrentRA = get_local_sidereal_time(longitude);
        }
        return true;
    }

    if (longitude > 180)
    {
        p1.lng = 360.0 - longitude;
        IsWest = true;
    }
    else
    {
        p1.lng = longitude;
    }
    p1.lat = latitude;
    ln_lnlat_to_hlnlat(&p1, &p2);
    LOGF_INFO("Update location to latitude %d:%d:%1.2f longitude %d:%d:%1.2f",
              p2.lat.degrees, p2.lat.minutes, p2.lat.seconds, p2.lng.degrees, p2.lng.minutes, p2.lng.seconds);

    cmd[0] = 'W';
    cmd[1] = p2.lat.degrees;
    cmd[2] = p2.lat.minutes;
    cmd[3] = rint(p2.lat.seconds);
    cmd[4] = (p2.lat.neg == 0) ? 0 : 1;
    cmd[5] = p2.lng.degrees;
    cmd[6] = p2.lng.minutes;
    cmd[7] = rint(p2.lng.seconds);
    cmd[9] = IsWest ? 1 : 0;

    return sendCommand(cmd, res, 10);
}
예제 #3
0
bool ScopeSim::initProperties()
{
    /* Make sure to init parent properties first */
    INDI::Telescope::initProperties();

    /* Simulated periodic error in RA, DEC */
    IUFillNumber(&EqPEN[RA_AXIS], "RA_PE", "RA (hh:mm:ss)", "%010.6m", 0, 24, 0, 15.);
    IUFillNumber(&EqPEN[DEC_AXIS], "DEC_PE", "DEC (dd:mm:ss)", "%010.6m", -90, 90, 0, 15.);
    IUFillNumberVector(&EqPENV, EqPEN, 2, getDeviceName(), "EQUATORIAL_PE", "Periodic Error", MOTION_TAB, IP_RO, 60,
                       IPS_IDLE);

    /* Enable client to manually add periodic error northward or southward for simulation purposes */
    IUFillSwitch(&PEErrNSS[DIRECTION_NORTH], "PE_N", "North", ISS_OFF);
    IUFillSwitch(&PEErrNSS[DIRECTION_SOUTH], "PE_S", "South", ISS_OFF);
    IUFillSwitchVector(&PEErrNSSP, PEErrNSS, 2, getDeviceName(), "PE_NS", "PE N/S", MOTION_TAB, IP_RW, ISR_ATMOST1, 60,
                       IPS_IDLE);

    /* Enable client to manually add periodic error westward or easthward for simulation purposes */
    IUFillSwitch(&PEErrWES[DIRECTION_WEST], "PE_W", "West", ISS_OFF);
    IUFillSwitch(&PEErrWES[DIRECTION_EAST], "PE_E", "East", ISS_OFF);
    IUFillSwitchVector(&PEErrWESP, PEErrWES, 2, getDeviceName(), "PE_WE", "PE W/E", MOTION_TAB, IP_RW, ISR_ATMOST1, 60,
                       IPS_IDLE);

    /* How fast do we guide compared to sidereal rate */
    IUFillNumber(&GuideRateN[RA_AXIS], "GUIDE_RATE_WE", "W/E Rate", "%g", 0, 1, 0.1, 0.3);
    IUFillNumber(&GuideRateN[DEC_AXIS], "GUIDE_RATE_NS", "N/S Rate", "%g", 0, 1, 0.1, 0.3);
    IUFillNumberVector(&GuideRateNP, GuideRateN, 2, getDeviceName(), "GUIDE_RATE", "Guiding Rate", MOTION_TAB, IP_RW, 0,
                       IPS_IDLE);

    IUFillSwitch(&SlewRateS[SLEW_GUIDE], "SLEW_GUIDE", "Guide", ISS_OFF);
    IUFillSwitch(&SlewRateS[SLEW_CENTERING], "SLEW_CENTERING", "Centering", ISS_OFF);
    IUFillSwitch(&SlewRateS[SLEW_FIND], "SLEW_FIND", "Find", ISS_OFF);
    IUFillSwitch(&SlewRateS[SLEW_MAX], "SLEW_MAX", "Max", ISS_ON);
    IUFillSwitchVector(&SlewRateSP, SlewRateS, 4, getDeviceName(), "TELESCOPE_SLEW_RATE", "Slew Rate", MOTION_TAB,
                       IP_RW, ISR_1OFMANY, 0, IPS_IDLE);

    // Add Tracking Modes
    AddTrackMode("TRACK_SIDEREAL", "Sidereal", true);
    AddTrackMode("TRACK_CUSTOM", "Custom");

    // Let's simulate it to be an F/7.5 120mm telescope
    ScopeParametersN[0].value = 120;
    ScopeParametersN[1].value = 900;
    ScopeParametersN[2].value = 120;
    ScopeParametersN[3].value = 900;

    TrackState = SCOPE_IDLE;

    SetParkDataType(PARK_RA_DEC);

    initGuiderProperties(getDeviceName(), MOTION_TAB);

    /* Add debug controls so we may debug driver if necessary */
    addDebugControl();

    setDriverInterface(getDriverInterface() | GUIDER_INTERFACE);

    double longitude=0, latitude=90;
    // Get value from config file if it exists.
    IUGetConfigNumber(getDeviceName(), "GEOGRAPHIC_COORD", "LONG", &longitude);
    currentRA  = get_local_sidereal_time(longitude);
    IUGetConfigNumber(getDeviceName(), "GEOGRAPHIC_COORD", "LAT", &latitude);
    currentDEC = latitude > 0 ? 90 : -90;

    return true;
}
예제 #4
0
파일: paramount.cpp 프로젝트: azwing/indi
bool Paramount::initProperties()
{
    /* Make sure to init parent properties first */
    INDI::Telescope::initProperties();

    for (int i = 0; i < SlewRateSP.nsp-1; i++)
    {
        sprintf(SlewRateSP.sp[i].label, "%.fx", slewspeeds[i]);
        SlewRateSP.sp[i].aux = (void *)&slewspeeds[i];
    }

    // Set 64x as default speed
    SlewRateSP.sp[5].s = ISS_ON;

    /* How fast do we guide compared to sidereal rate */
    IUFillNumber(&JogRateN[RA_AXIS], "JOG_RATE_WE", "W/E Rate (arcmin)", "%g", 0, 600, 60, 30);
    IUFillNumber(&JogRateN[DEC_AXIS], "JOG_RATE_NS", "N/S Rate (arcmin)", "%g", 0, 600, 60, 30);
    IUFillNumberVector(&JogRateNP, JogRateN, 2, getDeviceName(), "JOG_RATE", "Jog Rate", MOTION_TAB, IP_RW, 0,
                       IPS_IDLE);

    /* How fast do we guide compared to sidereal rate */
    IUFillNumber(&GuideRateN[RA_AXIS], "GUIDE_RATE_WE", "W/E Rate", "%1.1f", 0.0, 1.0, 0.1, 0.5);
    IUFillNumber(&GuideRateN[DEC_AXIS], "GUIDE_RATE_NS", "N/S Rate", "%1.1f", 0.0, 1.0, 0.1, 0.5);
    IUFillNumberVector(&GuideRateNP, GuideRateN, 2, getDeviceName(), "GUIDE_RATE", "Guiding Rate", MOTION_TAB, IP_RW, 0,
                       IPS_IDLE);

    // Tracking Mode
#if 0
    IUFillSwitch(&TrackModeS[TRACK_SIDEREAL], "TRACK_SIDEREAL", "Sidereal", ISS_OFF);
    IUFillSwitch(&TrackModeS[TRACK_SOLAR], "TRACK_SOLAR", "Solar", ISS_OFF);
    IUFillSwitch(&TrackModeS[TRACK_LUNAR], "TRACK_LUNAR", "Lunar", ISS_OFF);
    IUFillSwitch(&TrackModeS[TRACK_CUSTOM], "TRACK_CUSTOM", "Custom", ISS_OFF);
    IUFillSwitchVector(&TrackModeSP, TrackModeS, 4, getDeviceName(), "TELESCOPE_TRACK_MODE", "Track Mode",
                       MAIN_CONTROL_TAB, IP_RW, ISR_ATMOST1, 0, IPS_IDLE);
#endif

    AddTrackMode("TRACK_SIDEREAL", "Sidereal", true);
    AddTrackMode("TRACK_SOLAR", "Solar");
    AddTrackMode("TRACK_LUNAR", "Lunar");
    AddTrackMode("TRACK_CUSTOM", "Custom");

    // Custom Tracking Rate
#if 0
    IUFillNumber(&TrackRateN[0], "TRACK_RATE_RA", "RA (arcsecs/s)", "%.6f", -16384.0, 16384.0, 0.000001, 15.041067);
    IUFillNumber(&TrackRateN[1], "TRACK_RATE_DE", "DE (arcsecs/s)", "%.6f", -16384.0, 16384.0, 0.000001, 0);
    IUFillNumberVector(&TrackRateNP, TrackRateN, 2, getDeviceName(), "TELESCOPE_TRACK_RATE", "Track Rates",
                       MAIN_CONTROL_TAB, IP_RW, 60, IPS_IDLE);
#endif

    // Let's simulate it to be an F/7.5 120mm telescope with 50m 175mm guide scope
    ScopeParametersN[0].value = 120;
    ScopeParametersN[1].value = 900;
    ScopeParametersN[2].value = 50;
    ScopeParametersN[3].value = 175;

    TrackState = SCOPE_IDLE;

    SetParkDataType(PARK_RA_DEC);

    initGuiderProperties(getDeviceName(), MOTION_TAB);

    setDriverInterface(getDriverInterface() | GUIDER_INTERFACE);

    addAuxControls();

    double longitude=0, latitude=90;
    // Get value from config file if it exists.
    IUGetConfigNumber(getDeviceName(), "GEOGRAPHIC_COORD", "LONG", &longitude);
    currentRA  = get_local_sidereal_time(longitude);
    IUGetConfigNumber(getDeviceName(), "GEOGRAPHIC_COORD", "LAT", &latitude);
    currentDEC = latitude > 0 ? 90 : -90;

    return true;
}