1. I. Plan to Meet PLRA Threshold Requirements Phil Hinz Principal Investigator

2. Science Validation Plan Compliance This presentation discusses the tasks planned to improve the performance of LBTI to that of the PLRA threshold requirements Relationship to ORR Success Criteria: This addresses 1c, describing the plans to meet the threshold requirements Concerns: – Terms in the null uncertainty error budget are difficult to isolate and verify. Precise performance prediction and assessing impact of improvements is therefore difficult. Liens: None, though we continue to explore new detector options I-2 1.cCredible plans* documented to meet PLRA threshold performance requirements (6 zodi, 0.3 mJy) by end of science validation phase with risk that is medium or lower Green

3. Compliance Matrix PLRA Section Success Criteria March 2014 Now (ORR) End of SVP In-Guide Plan (FY17) With Lien (FY18) L04.3A: 10x better 2.8x better12x better24x better L04.3B: Inform missions 6 zodi median 1.13 zodi median 0.51 zodi median 0.50 zodi median L14.1.2C: 6 zodi, 1 σ 54 zodi12 zodi6 zodi L14.1.4D: 50 stars in 4 yrs 13183550 L24.1.4E: 0.3 mJy sens. 0.4 mJy 0.3 mJy L24.1.4F: 1.5x10 -4 null stb 1800 ppm400 ppm150 ppm L24.1.4G: 30% efficiency 30%32%40% I-3 Red = not compliant Blue = compliant, assuming in-guide completion Orange = compliant with ORR criteria, but not PLRA Green = compliant with PLRA 1 23

4. 1. Efficiency Budget Already meets requirement; sufficient to carry out HOSTS survey Setup efficiencies will improve during SV phase, providing greater margin against the number of stars that can be surveyed I-4 Automate process Yellow=areas of concern for SVP Blue=projected Improvement for SVP

5. 2. Photometric Error Budget—Current Excess background is the dominant noise term Throughput improvements will help I-5

6. Modeling Throughput and Background We have used vendor specifications and on- and off-sky testing to measure the system throughput of LBTI – Spreadsheet captures our current estimate – Throughput is 1.5x lower than expected The background dominates the noise for LBTI SNR calculation uses the photons/frame and the throughput to track our expected performance relative to the requirements I-6

7. Improve Photometric Sensitivity Reduce equivalent blackbody background emissivity to 16% from 27% (measured) – Replace poorly performing WFS dichroic and better baffling Improve throughput to 6.6% from 4.5% (measured) – Remove warm ZnSe uncoated window (used as safety between NIC and beam-combiner) – Model suggests an additional factor of 1.5 is possible Pipeline optimization during SVP – Improve data rejection to optimize null uncertainty jointly with photometric uncertainty – Implement PSF photometry I-7

8. Impact on Photometric Uncertainty Photometric requirements will be reached via straightforward improvements to the instrument during SVP I-8

9. 3. Null Uncertainty: Error Budget Areas of improvement are PWV turbulence, vibrations, and photometric bias I-9 Photometric uncertainty is incorporated into null budget

10. PWV Turbulence Low-frequency variations in the null are seen – These variations are more prominent on high-PWV nights I-10 Low PWV High PWV

11. Approach to Estimating PWV Effect NSC fits a mean (μ) and scatter (σ) to the intensity variations to distinguish these effects from the astrophysical null – The mean and scatter can only be measured to a precision given as – N is the number of independent measurements, about 60 per OB – Resulting setpoint uncertainty is 60 nm Null uncertainty given by I-11 This is consistent with phase drift calculated from NSC fits to successive OBs

12. PWV Mitigation: 1 Since PWV mitigation is the largest error budget term, several options are being developed to minimize risk: – Option A: Use group delay measurement of the K-band phase sensor. Timescale to implement: Summer 2015 Risk: Group delay metric may not encode water vapor dispersion accurately enough to improve null – Option B: Measure group delay using the 3- to 5-micron light with LMIRcam Timescale to implement: Summer 2015 Risk: Speed of LMIRcam may not be sufficient to track dispersion changes – Option C: Reconfigure K band phase sensor to more accurately measure group delay Timescale to implement: Fall 2015 Risk: More extensive change to the phasing code required I-12

13. PWV Mitigation: 2 Queue scheduling will be implemented to use driest nights for HOSTS – Most other LBTI programs don’t require dry conditions – Steward Observatory has agreed to support this – Queue will be internal to LBTI runs with clearly defined rules – Weather loss and overall allocations will still be adhered to, but may be spread over more than one semester I-13

14. Vibration We see two effects: – Vibrations at 10–20 Hz due to resonant telescope modes Removed by phase sensor Tests done to feed-forward with accelerometers – Vibrations at 100–300 Hz due to instrument Appears to be LBTI box-beam structures Cryogenic optics mounting may also contribute I-14 Telescope Vibrations Instrument Vibrations

15. Approach to Estimating Vibration Effect Assume that the residual vibration in the system (that is, whatever is not corrected by phase cam) is all high-frequency – Blurs individual frames by This is removed via phase cam telemetry, but adopt a systematic estimation error of 2%. We currently see 400 nm RMS of high-frequency vibration (f>1/DIT) I-15

16. Vibration Mitigation Reduce instrument vibration – Damping of identified resonant beams – Stiffening of identified “soft” mounts Feed-forward telescope vibration – Refine proven approach to use accelerometers and filtering for specific frequencies – Add feed-forward for tertiaries (to be implemented) as well as secondaries (currently implemented) I-16

17. Photometric Bias Excess low-frequency noise is seen in our data – This is primarily caused by our BIB detector – Thickness of the detection layer causes this (Stapelbroek et al. 1984) – A new detector could eliminate this effect I-17

18. Approach to Estimating Photometric Bias We measure a 2-mJy uncertainty per pointing from the NSC For this error budget we assume the calibrators and science object are the same I-18

19. Photometric Bias Mitigation Minimize Excess Low Frequency Noise (ELFN) by revising observing approach – Increase nod frequency (0.01 → 0.02 Hz, 1.5x improvement) – Improve background subtraction by using closest frames (1.5x improvement) Detector upgrade – Discussing/exploring options with ESO and Raytheon I-19

20. Null Uncertainty Improvements We expect a 2x improvement of null drift once PWV mitigation is implemented We expect a 2x improvement of the vibration residuals once the accelerometer feed- forward and instrument damping work is completed We expect a 2x improvement in the photometric bias after shortening the nod cycle time I-20

21. Impact on Nulling Uncertainty I-21

22. Impact on HOSTS Survey Most of the SV tasks can be carried out in parallel with executing the survey We will require dedicated engineering time at the level of approximately two nights total in FY16 for the following tasks: – Validating PWV tracking approach – Validating automated operation – Exploring increased nodding frequency sequences – Tuning and optimizing the feed-forward inputs I-22

23. SVP Mean Zodi Estimate Based on following limits: – 1 mJy photometric bias/pointing – Noise floor of 150 ppm (bright star limit) The uncertainty for a general HOSTS star is Overall sample provides mean zodi sensitivity: – 4.9 for sample of 32 stars – 6.1 for full sample of 50 stars I-23

24. Science Validation Summary We have defined a list of tasks to execute over the next 9 months – Detailed schedule developed (see supporting document on Wiki) The planned performance improvements are sufficient to meet the threshold requirements – The modeled performance is not precise, and provides some level of risk to achieving the threshold performance I-24