CSIRO Astronomy and Space Science
Parkes Users Guide
Preface
Operators
Conventions
(1) Introducing the Parkes Observatory
/1./Introducing the Parkes Observatory
/1.1/The Parkes RadioTelescope
/1.2/Transport to the Observatory
/1.3/Other Information
/1.4/Observers Quarters
/1.5/Booking Your Accomodation
/1.6/Visitors Centre and Dish Cafe
/1.7/Observatory Contact Details
(2) Planning Your Observations
/2./Planning Your Observations
/2.1/Applying for Observing Time
/2.2/Radio-Frequency Interference Considerations
/2.3/Observing Modes
/2.4/Preparing Schedule Files
/2.5/Sensitivity
/2.6/Parkes Receiver Fleet
/2.7/Conversion System
/2.8/Signal Path
/2.9/Standing Wave Reduction
/2.10/Correlators
/2.11/Dish Surface Quality
(3) Observer Training & Safety
/3./Observer Training & Safety
/3.1/Introduction
/3.2/Duties of an LICENSED OPERATOR
/3.3/Duties of a DESIGNATED CONTACT PERSON (DCP)
/3.4/Questions and Answers
/3.5/Definitions
(4) Observing
/4./Observing
/4.1/The Call–out person
/4.2/The Telescope Hardware
/4.3/The Telescope Control Software
/4.4/Master Control Panel
/4.5/Weather and wind restrictions
/4.6/Stowing and Unstowing
/4.7/Power Supply via Mains/Diesel/UPS
(5) Observing Checklist
/5./Observing Checklist
/5.1/Observing Checklist UPSTAIRS
/5.2/Observing Checklist DOWNSTAIRS
(6) Data Reduction and End of Observing
/6./Data Reduction and End of Observing
/6.1/ATNF Data Format
/6.2/LIVEDATA & GRIDZILLA
/6.3/ASAP
/6.4/MIRIAD
/6.5/Source finding programs
/6.6/Other Packages
/6.7/Magnetic Tape Storage
/6.8/Portable Storage
/6.9/Laptop Storage
/6.10/DVD Archiving with PKARC
/6.11/Disk Cleanup
/6.12/Observer Report
(7) TroubleShooting
/7./TroubleShooting
/7.1/Correlator issues
/7.2/Australia Telescope Distributed Clock Displays all zeros
/7.3/Azimuth and/or Zenith Drives Disabled
/7.4/PKDESK requires a restart or crashes
/7.5/Mouse seems to have disappeared on BOURBON
/7.6/OPERFCC Reports Y2 Axis Following Error
/7.7/Loss of 1MHz sampling clock and/or 0.2pps (5-second) pulse
/7.8/Pulsar Data Acquisition Problems
/7.9/ME or SERVO stops/crashes
/7.10/Safety Timer fails to reset
/7.11/SPD display shows rubbish
(8) Appendicies
/8./Appendicies
/8.1/Trainers Guide to Training Observers
/8.2/Site Alarms
Index
[Printable Guide]

2. Planning Your Observations

2.1 Applying for Observing Time

Proposal forms and submission deadlines can be found here, while current and archived observing schedules can be found here.

Information regarding system capabilities not listed here can be addressed to parkes-operations@csiro.au

2.2 Radio-Frequency Interference Considerations

An introduction to RFI observed at the observatory and surveys performed is available here.

2.3 Observing Modes

Spectral and continuum-line observations can be performed with all currently-available receivers and back-ends. Possible observing modes include:

There are three methods of switching. Not all methods are available with all receivers/back-ends.

2.4 Preparing Schedule Files

For the majority of programs, you will be using the Telescope Control Software (TCS). The TCS graphical user interface (TCS GUI) is written in Glish/Tk and runs on a Solaris workstation. A glish client runs on the same host as the TCS GUI which serves as a communications channel between the TCS GUI and the (Linux) controller.

There are two ways to use TCS. The first is to select observing parameters from the TCS GUI via widgets and entry boxes. The second (and recommended) is to use schedule files which are loaded values become the default parameters on the TCS GUI. Until accustomed with the system, first-time users are strongly urged to use schedule files. Detailed information on keywords used in schedule files and examples can be found in the TCS documentation

Some of the main items to worry about in your schedule file(s) are as follows, but note this is not an exhaustive list!

There are online utilities to assist in the preparation of schedules for position–switching, beam–switching, tracking (with or without frequency switching) and on-the-fly mapping. These can be found on the Parkes utilities page. Note that these tools DO NOT cater for Pulsar observations.

2.5 Sensitivity

When preparing your observing proposal, you are required to estimate the expected brightness and sensitivity of your source for your particular Correlator/receiver combinations. For spectral-line observations, sensitivity per bandwidth channel can be estimated from the following equations of line brightness and line flux respectively:

$T_{rms} (mK) \sim {{1.8 T_{sys}} \over {\sqrt{npol {BW \over chan} \delta T}}}$

$S_{rms} ({mJy \over beam}) \sim T_{rms} G \eta_b$

In the above, G is the gain (Jy/K) for a receiver defined from tab:rxprops, npol is the number of polarisations(2), BW is the bandwidth [MHz], nchan is the number of channels and $\delta T$ is the on-source integration time in seconds. $\eta_{b}$ is the beam efficiency factor: $\Omega_{mb} \over \Omega_{tot}$ = 0.7. For continuum, we need to calculate the sensitivity over the whole bandwidth. The continuum line brightness and line flux respectively become:

$T_{rms} (mK) \sim {{1.8 T_{sys} \over {\sqrt{npol BW \delta T}}}}$

$S_{rms} ({mJy \over beam}) \sim T_{rms} G \eta_b$

For both the line and continuum flux, the source is assumed to fill the main beam which has efficiency $\Omega_{mb} \over \Omega_{tot}$ = 0.7. 1-sigma theoretical RMS noise estimates for line and continuum observations can be estimated by using the on-line Sensitivity Calculator.

2.6 Parkes Receiver Fleet

Click on the receiver links below in tab:rxprops to show information regarding receiver information such as characterization tests, gain-elevation curves and pointing accuracy. Please note this information is being uploaded when receivers are installed and may not be available at the present time.

 
----------------------------------------------------------------------------
Receiver   Band     Range   Diameter  FWHP    Tsys  Sen[a]    Pols[b]  Bandw 
           [cm]     [GHz]      [m]    [']     [K]   [Jy/K]             [MHz]
----------------------------------------------------------------------------
70cm         
            70     0.44        64    30      65       2       2xL       36
1050cm      
            50     0.70-0.764  64    30      40      1.7?     2xL       64
            10     2.60-3.600  64     7      30      1.5?     2xL     1000
MB20   
            21     1.23-1.53   64    14      23.5    1.5     26xL      300
H-OH         
            21/18  1.2-1.8     64    14      25.5      1.3    2xL      500
Galileo      
            13     2.20-2.5    64     9.2    20      1.9      2xC      300
                   2.15-2.27   64     9.2    20      1.9      2xC      120
                   2.29-2.3    64     9.2    19      1.4      2xC       10
AT S-BAND[c]       
            13     2.2-2.5     64     9.2    79      1.9      2xL      300
AT C-BAND[c]        
             6     4.5-5.1     64     4.2    50      2.2        C      500
AT X-BAND[c]        
             3     8.1.8.7     64     2.7    54      2.1    2xL|C      500
             3/13  8.1-8.7     64     2.4    60      2.1      2xL      500
                   2.2-2.5     64     9.2   100      2.0        C      300
METH6     
                   5.9-6.3     64     3.3    50      2.2      2xC      300
                   6.4-6.8     64     3.3    50      2.2      2xC      300
METH12
             2.5 12.0-12.4     64     2.0    50      3.5      2xC      250
Mars[d]       
             3     8.0-8.9     64     2.45   25      1.7      2xC      500
13MM[e]       
             1.3  16.0-26.0    55    1-1.4   60      4.5      2xL     1000
                  21.0-22.3                                   2xC     1000
KU-BAND      
             2.2  12.0-15.0    64     1.3   140      5.8      2xL      500
K-BAND    
             1.3  21.0-24.0    55     1.5   105      3.5      2xC      500
---------------------------------------------------------------------------
[a] Calculated with typical atmospheric contribution.
[b] L = linear, C = circular, NB = narrowband.
[c] Dual linear feeds at S,C,X bands, $\lambda$/4 plates avaliable for band centers.
[d] Full bandwidth by special arrangement.
[e] See section on this receiver below.

Table 2.1: Parameters for the Parkes receiver fleet.

2.6.1 Receiver Calibration Signal

Most of the Parkes receivers including allow injection of a calibration noise signal into the receiver waveguide ahead of the ortho-mode transducer (OMT). This is generally a more satisfactory method than injecting after the OMT or after the LNAs as these elements can then be modelled using the calibration signal.

The calibration signal is generally injected through a coupler in the circular waveguide oriented at 45 degrees to the linear probes of the OMT. Thus the cal can be closely represented by a 100% linearly-polarised signal with an accurately known feed angle.

The amplitude of the cal signal is adjustable by inserting or removing fixed attenuators between the noise source and the coupler. Changing the level requires access to the receiver in the focus cabin and takes of order 30 minutes. The cal can be switched on or off remotely as required, using an observer-selectable waveform. Typically the cal is run as a continuous low-level NAR (Noise-Adding Radiometer) with the cal level approximately 10% of Tsys, for a time-averaged increase of 5%. The frequency of the switching signal is typically between a few Hz and 500Hz.

The H-OH receiver has an optional quarter-wave plate which can be inserted in the circular waveguide between the feedhorn and the OMT to achieve circular polarisation on the sky. The quarter-wave plate is inserted before the cal injection so in this case the cal signal resembles a 100% circularly-polarised signal on the sky but the cal signal alone cannot be used to model the precise properties of the quarter-wave plate.

The 13MM receiver also has an optional quarter-wave plate used with the narrow-band VLBI feed covering the 22 GHz water transition. As with the H-OH receiver, the cal injection occurs after the polariser (between the polariser and the OMT).

The MARS (8.4 GHz; X–band) receiver has a built-in (non-removable) waveguide circular polariser also with cal injection between the polariser and OMT.

The C-band and X-band receivers in the AT Multi-band receivers also have quarter-wave plates ahead of the cal injection.

The GALILEO receiver has cal injection into circular waveguide but uses a circularly-polarised OMT (cal signal resembles 100% linear on sky).

The 50cm receiver in the 1050CM package injects a cal signal using a directional coupler after each LNA (strictly, after the 4-port hybrid used to combine the signal from each pair of opposing probes and LNAs). A splitter is used to generate two identical cal signals from the same noise source.

2.7 Conversion System

The Parkes Conversion System (PCS) is summarised as follows:

An in–depth discussion of the PCS (including block diagrams) is available here.

2.8 Signal Path

An overall outline of the Parkes observing system is shown in fig:signalpath-overview.

signalpath-overview

.

Figure 2.1: Overview of the Parkes observing system.

Single-beam spectral–line observations have back-end options using 4, 8 or 64 MHz bandpass capabilities of the 2–bit Multibeam correlator, or patching in an ATCA–style bandpass filter to provide 16 or 32 MHz bandpass capability. Wider bandwidths (>64 MHz) are available using the 8–bit Digital Filterbanks (DFB3/DFB4), but it is also possible to achieve smaller bandpasses with DFB3/DFB4 (ie., 8, 16, 32 MHz).

For Pulsar observations, it is possible to switch simultaneously record data on several back ends at once.

2.9 Standing Wave Reduction

For Parkes, characteristic small-scale ripple with periodicity $\sim$5.7 MHz arises from multiple reflections in the 26m space between the vertex at one end, and the focus and/or underside of the focus cabin at the other. fig:standwave shows 22 GHz observations of a strong Ammonia source, G316.819, showing strong (1,1) and (2,2) transitions for 4 minutes (exact multiple of 60 seconds). The two observations were taken one after the other, the first (upper panel) with no special ’de-rippling’ measures, the lower taken in a mode where the receiver is moved cyclically up and down in the translator Y-axis to ’smear out’ the ripple with amplitude 6.3mm peak-to-peak ($\lambda$/2) and period 60 seconds. This technique is available for use with higher-frequency receivers only and proposers should contact Parkes Operations (parkes-operations@csiro.au) before submitting proposals.

ripple

Figure 2.2: Upper panel showing characteristic 5.7 MHz standing wave interference

with lower panel showing a cleaner spectrum obtained with receiver cycling.

2.10 Correlators

A number of correlators/backend units are available:

Please check the Parkes Correlator Guide for information on capabilities or email parkes-operations@csiro.au to ascertain requirements.

2.11 Dish Surface Quality

A 4 GHz holographic survey of the dish surface was performed prior to the 1995 upgrade of the focus cabin. Other surveys at 3.95 GHz (June 1996) and 12.75 GHz (July 1996) were performed after the installation of the new focus cabin. Details of the readjustment of the inner 44m of the Parkes reflector in December 1996 is also also available here. As part of the NASA Mars tracking contract in 2003/2004, the Parkes Telescope’s surface was upgraded to make it more reflective and sensitive at X-band ($\sim$ 8.5 GHz). The surface upgrade improved the telescope’s performance by about 1 dB (or 25%). A technical guide is available.

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