PIONIER Overview

The PIONIER instrument can be operated both on the Unit Telescopes (UTs) and on the Auxiliary telescopes (ATs). The UT adaptive optics MACAO guarantees diffraction-limited image quality on PIONIER for targets brighter than V=15 (please refer to the latest version of the VLTI User Manual). Starting from Period 104 the ATs have been equipped with NAOMI adaptive optics. The top performances are guaranteed for targets with R = 11 mag. The performances degrade down to R = 15 mag. For details we refer to the latest version of the VLTI User Manual. Off-axis guiding is possible if the target does not meet the above limits. The presence of an appropriate guide star must then be checked and indicated in the proposal in the target notes. The VLTI is considered non-operational at seeing values worse than 1.5" because of operational limit for the adative optics above. PIONIER is offered on various sets of baselines: please look at the VLTI News webpage to get the list of the UT and AT baselines available. The Spectrograph optics are either dispersed (GRISM, 6 pixel over H-band), or undispersed (FREE, 1 pixel). As a rule, Visitor Mode is discouraged and will only be accepted for observations that are well justified to require real-time decisions or non-standard operational procedures in order to achieve the proposed science goal.

Limiting Visibility and Magnitudes

PIONIER is tracking its own fringes. Due to the limited dynamic range of the detector, the fringe tracking requires a minimum visibility of V = 0.05, or 5%. This requirement must, however, be met only on the short and intermediate baselines in a given quadruplet, since the fringe position on the longest (or most resolved) baselines can be calculated from the information obtained from the less resolved, fringe tracking baselines. Depending on the geometry of the baselines that can track fringes, two or three remaining baselines can be bootstrapped. If bootstrapping the fringe position is possible in this way, the limit at which fringes can be reduced and calibrated is much lower, namely V = 0.01, or 1%.

The bright limit is given by the high detector sensitivity vs. its limited dynamic range. Targets cannot be observed in service mode if they are brighter than H = -1 mag. Brighter targets can in principle be observed by inserting a vignetting optics into the beam or defocussing the telescopes (only possible with ATs), but this special operation is limited to visitor mode observations. In any case, the above visibility limits apply, which more typically will be the reason why these targets cannot be observed, rather than the brightness as such. 

The faint limit depends on the observing conditions. After the installation of the NAOMI adaptive optics the limit values have been assessed and are modified for observing proposals from P105 onwards. Starting from P105 a new atmospheric turbulence constraint replaces the current seeing constraint. There is no need to ask for photometric conditions while using PIONIER, usually CLEAR is reccomended for faintest sources, while THIN conditions are sufficient for all the other cases. The execution times depending on the brightness of the source are:

Dispersion Limit (H mag) Conditions to be used in phase 1
FREE 8.6 to 9.0  T ≤ 10%, seeing ≤ 0.6", τ0 > 5.2 ms 45 min (2700 sec) 75 min (4500 sec)
GRISM 7.6 to 8.5  T ≤ 10%, seeing ≤ 0.6", τ0 > 5.2 ms 45 min (2700 sec) 75 min (4500 sec)
 6.1 to 7.5  T ≤ 30%, seeing ≤ 0.8", τ0 > 4.1 ms 40 min (2400 sec) 60 min (3600 sec)
GRISM  -1.0 to 6.0  T ≤ 70%, seeing ≤ 1.15", τ0 > 2.2 ms 30 min (1800 sec) 45 min (2700 sec)

the H-band magnitude listed above are correlated magnitudes, to be calculated using the formula Hcorr = Htot - 2.5 * log10 (Visibility)

Calibrators should be similarly bright as the target. Large magnitude differences will lead to considerably lower signal in the fainter object, and hence to lower precision. For optimal precision of the calibration, the magnitude difference should not be more than 1 magnitude. Differences of more than 3 magnitudes become operationally difficult to secure with the same setup of the detector, thus not only diminish the chance of an observation to be carried out, but will introduce a slight and systematic mis-calibration of a few percent. In particular, for targets brighter than H=2.5 also the calibrator needs to be brighter than H=2.5, and fainter targets should have fainter calibrators, as around H=2.5 a different detector gain value will be set under normal conditions by the operator. Finally, there is some evidence that for large magnitude differences between SCI and CAL the calibration is systematically worse in the blueward channels.

It is of greatest importance that the coordinates of all objects in a concatenation are taken from a consistent source. Coordinate offsets lead to offsets in optical path difference, which may prevent the fringes to be found and cause the execution to fail.

Tests of PIONIER on the UTs have shown that, although fringes can be detected up to H ~ 11 mag, the data turned out to be very difficult to calibrate. In particular, no observation beyond H = 9 mag (which is as well the AT limiting magnitude) could yet be verified as scientifically valid. The exact issues are possibly related to injection instabilities, to which PIONIER, designed for the ATs and never optimised for the UTs, is particularly sensitive. Therefore, UTs should only be used when other issues (such as availability of guide stars or need for small interferometric FoV) prohibit the use of ATs.

Typical Calibration Precision

Applying the normal observation and calibration scheme offered in service mode, the accuracy of PIONIER observables (squared visibility and closure phase) is limited by calibration systematics related to the separation between calibrators and science target. To minimize these systematics, calibrators should be selected within a few degrees from the science target. For a separation of 3 degree between the calibrators and the science target, the typical accuracy reached is 3% on the squared visibility and 2 degree on the closure phase measured. The use of different calibrators distributed around the science target is advisable. Further reducing this uncertainty is possible applying a more complex calibration scheme that can only be offered in visitor mode (see the PIONIER user manual for details).

Other Instrument and Detector Parameters

Other parameters, such as detector gain and integration times, will be chosen by the operator based on conditions vs. target parameters, as they will not affect the scientific results. In service mode we ensure that a given concatenation is observed with a single set of parameters only, except for very bright targets, where suitable calibrators may be to faint and the have to be observed with a higher detector gain. The calibratatablity of this procedure was tested and results are within the typical precision. In any case, we do not guarantee to use identical parameters across several concatenations, since they may be observed on different dates under different conditions.This is not waiverable in service mode, and users who can solidly justify the scientific need for consistent instrument and detector parameters across their program (such as the need to achieve exceptionally high calibration precision) should apply for visitor mode.

Operation Sequences

In service mode, two operation sequences are offered, namely three OBs (in a CAL-SCI-CAL concatenation, depending on the brightness of the source mostly suitable for snapshot observations) or five OBs (in a CAL-SCI-CAL-SCI-CAL concatenation, suitable for imaging programs). 

Visitor mode observers are advised to plan with about 10 to 12 minutes per OB, to allow some additional time for inter-OB decision making or special operation procedures, which typically will be the reason why VM would be accepted..

Data Reduction

Data reduction software PNDRS is available from the JMMC dedicated webpage. Additionally, all SM data will be routinely processed at IPAG and calibrated OIFITS data can be retrieved from the OIDB database.