Implications of Atmospheric Differential Refraction for Adaptive Optics Observations1 Henry G. Roe,2 PASP, in press. ABSTRACT Many adaptive optics systems operate by measuring the distortion of the wavefront in one wavelength range and performing the scientific observations in a second, different wavelength range. Onecommontechniqueistomeasurewavefrontdistortionsatwavelengths<∼1µmwhile operatingthescienceinstrumentatwavelengths>∼1µm. Theindexofrefractionofairdecreases sharply from shorter visible wavelengths to near-infrared wavelengths. Therefore, because the 2 adaptive optics system is measuring the wavefront distortion in one wavelength range and the 0 scienceobservationsareperformedatadifferentwavelengthrange,residualimagemotionoccurs 0 and the maximum exposure time before smearing of the image can be significantly limited. We 2 demonstratetheimportanceofatmosphericdifferentialrefraction,presentcalculationstopredict n theeffectofatmosphericdifferentialrefraction,andfinallydiscusstheimplicationsofatmospheric a differential refraction for several current and proposed observatories. J Subject headings: atmospheric effects — instrumentation: adaptiveoptics 6 1 1. Introduction as the beamsplitter in order to send visible light 1 (<∼ 1µm) to the wavefront sensor and infrared v Adaptive Optics (AO) has been used for astro- light(>∼1µm)to the science instrument. Exam- 3 nomical observations for more than a decade and ples oftelescopes with AO systems that canoper- 7 numerous medium-to-large telescopes around the ateinthiswayinclude the3-mShanetelescopeat 2 world are now equipped with AO systems. If an Lick Observatory (Gavel et al. 2000), the CFHT 1 AO system’s wavefront sensor operates at differ- 0 3.6-m telescope (Rigaut et al. 1998), the Gem- 2 ent wavelengths than are being observed by the ini North 8-m telescope (Graves et al. 2000), and 0 science instrument, and no correction is made for / atmospheric differential refraction, the target ob- h p jectwillappeartodriftwithrespecttothescience - instrument. An example of the problem this phe- o nomenon can introduce is shown in Fig. 1 which r t is the difference of two images of Saturn’s moon s a Titan taken just 2.5 minutes apart while contin- : uously tracking and correcting on Titan with the v i KeckIItelescope’sAOsystem. Themaximumex- X posuretimepossiblewithoutdegradingthespatial r resolution of the data is significantly restricted if a no correction for atmospheric differential refrac- tion is made. Adaptive optics systems for astronomical ob- servingoperatebysplittingtheincominglightinto Fig. 1.— The difference between two raw images of twobeams,oneofwhichgoestothewavefrontsen- Titan taken just 153 seconds apart with NIRSPEC’s sor of the AO system and the goes to the science SCAM detector on the Keck II telescope while con- instrument. Inmanycasesadichroicopticisused tinuously guiding/correcting with the AO system on Titan. Each image is the result of three 10 second 1DatapresentedhereinwereobtainedattheW.M.Keck exposures. At the start of the first sequence of expo- Observatory, which is operated as a scientific partnership sures Titan was at an elevation of 57◦.86 and an hour among the California Institute of Technology, the Univer- angleof2.25; 153secondslaterwhenthesecondsetof sityofCalifornia,andtheNationalAeronauticsandSpace exposures started Titan was at an elevation of 57◦.26. Administration. The Observatory was made possible by Titan’s declination was 16◦.73. The 1-pixel wide slit the generous financial support of the W.M. Keck Founda- ofNIRSPEC’sspectrometerisacrossTitan’sdiskand tion. the apparent motion of Titan due to the effect of at- 2Department of Astronomy, 601 Campbell Hall, mospheric differential refraction is obvious along the University of California, Berkeley, CA 94720-3411. elevation vector. ([email protected]) 1 both of the W.M. Keck Observatory’s 10-m tele- scopes (Wizinowich et al. 2000). The wavefront sensor measures the distortions to the wavefront anda correctionis calculatedandappliedtoade- formablemirror. Thefirstorderofdistortionthat an AO system is called upon to correct is simply image motion, commonly known as ‘tip/tilt’. If significant tip/tilt residuals remain after AO cor- rection then the resulting data will be of lower spatial resolution, regardless of how well the AO system corrects for the higher order terms of fo- cus, astigmatism,coma, and so forth. Minimizing tip/tilt residuals is critical to achieving optimum Fig. 2.— The refractive index of air as a function of wavelength across the visible and near-infrared spec- performance from an AO system. The effect of trumatstandardtemperatureandpressureintheab- atmospheric differential refraction is to introduce sence of water vapor. a systematic tip/tilt errorthat anAO system will not correct for unless specifically accounted for in theAOcontrolsoftware. Foreaseintheremainder ADRforAOobservingwithcurrentandcurrently of this report we will refer to atmospheric differ- proposed telescopes. The code used in these cal- ential refraction as “ADR”. culationsisavailablewiththeelectronicversionof this paper or by request from the author. While Problems due to ADR arise when the AO sys- thecodeiswritteninthecommonlyusedIDLpro- tem is correcting on visible wavelength light and gramming language, it could easily be translated the science instrument is observing at infrared to otherlanguages. We encourageothers toinves- wavelengths. Fromvisibletoinfraredwavelengths tigate the implications of ADR for their favourite the refractive index of air decreases sharply, as telescope, site, target, observing strategy, etc.. shown in Fig. 2. A star’s visible pointing center always appears at higher elevation than a star’s 2. Theoretical Calculations infrared pointing center, except when the star is at the zenith. That the two pointing centers do The equations necessary for calculating the ef- not coincide is not unto itself a problem for the fectofADRaregivenbySchubert&Walterscheid typical AO system, however the offset between (2000). FromSchubert&Walterscheid(2000)the the two pointing centers is not constant. With- refractive index of air n at pressure p millibar, out some consideration for the effect of ADR, a temperature T Kelvin, partial pressure of water properly performing AO system will hold the vis- vapor p millibar3, and wavelength λ microns is w ible pointing center of the star fixed, relative to boththewavefrontsensorandthesciencecamera. n(λ,p,T,p )=1+ (1) w However as time progresses and the star moves 29498.1 255.4 pT in elevation, the infraredpointing center will drift 64.328+ + s 10−6 (cid:20) 146−λ−2 41−λ−2(cid:21)(cid:20)p T(cid:21) with respect to the visible pointing center, and s thus in the infrared the star appears to drift with −43.49 1− 7.956×10−3 pw10−6, respecttothescienceinstrument. Observersmust (cid:20) λ2 (cid:21) ps consider this effect in determining the maximum where p is 1013.25 millibar and T is 288.15 K. exposure times in order to avoid ‘trailed’ images, s s For a given refractive index n the angle between unless some other compensation is made. thetruezenithdistancez andtheapparentzenith In this paper we present calculations demon- t distance z is well approximated by strating when and how much of a problem ADR a can be for an AO system. Using data taken with n2−1 the AO system on the Keck II telescope we show R≡zt−za ≃206265(cid:18) 2n2 (cid:19)tanzt arcsec that in a long exposure, or sequence of exposures, (2) the most significant uncorrected tip-tilt motion is due to the effect of ADR. We further show that 3Schubert & Walterscheid (2000) contains a typo that re- the effect of ADR is dependent on the spectral sultedinamissingfactorof10−6 forthewatervaporcor- type, or color, of the star being used as a refer- rection. Equation2hereiscorrect. encesource. Finally,wediscusstheimplicationsof 2 ◦ Y forzenithdistanceslessthanabout80 . Observers East typically work at much more modest zenith dis- tancesofz <40◦−50◦ wherethis approximation t is extremely good. g Atmosphericdifferentialrefractionbetweentwo An s to Zenith wavelengths (e.g. λ of an AO wavefront sensor o vis P and λ of a science instrument) is then ir R −R = (3) X vis ir n2 −1 n2 −1 ParAng 206265 vis − ir tanz arcsec (cid:18) 2n2vis 2n2ir (cid:19) t North Note that equation 4 is written to give a posi- Fig. 3.— Schematic clarifying definition of position tive angular distance since the zenith distance of angle and parallactic angle. The parallactic angle the visible pointing center, z , will be less than (ParAng) is defined as the angle measured from the vis that of the infrared pointing center, z . The true vector pointing north on thesky counter-clockwise to ir the vector pointing to the zenith. The position angle zenithdistance(z )isrelatedtolatitudeoftheob- t (PosAng) is defined as the angle measured from the server (φ), declination of the target (δ), and hour positiveY-directiononthedetectorarrayclockwiseto angle of the target (H) by thevector pointing north on thesky. cos(z )=sin(φ)sin(δ)+cos(φ)cos(δ)cos(H) t (4) suchthatinstrumentcoordinatesremainfixedrel- ativetorightascensionanddeclination. Therefore To relate the ADR offset of equation 4 to the the instrument coordinate system rotates relative (x,y)coordinatesofadetectorarrayorientedarbi- to elevation and azimuth. The important point trarily with respect to the sky, we introduce sev- is that the instrument coordinate system rotates eral angles. As shown in Fig. 3 the parallactic about the visible pointing center. Thus, the ef- angle (ParAng) is the angle from the sky North fective motion of the infrared pointing center in vector counter-clockwise to the elevation-up vec- instrument coordinates is not along the elevation tor. Position angle (PosAng) is the angle from vector except when the parallactic angle is un- the increasing Y-direction of the detector array changing. In the images of Titan differenced in clockwisetotheskyNorthvector. Finally,thedif- Fig. 1 the parallactic angle was nearly unchang- ference of PosAng minus ParAng gives the angle ingandthereforethe motiondue toADRappears from the increasing Y-direction clockwise to the along the elevation vector. In later examples the elevation up vector. In the (x,y) coordinates of parallactic angle is changing rapidly and then the the detector array the offset from visible pointing apparentmotionis notalongthe elevationvector. center to infrared pointing center is then Equation 4 gives the instantaneous offset be- R −R X = ir vis sin(PosAng−ParAng) tween visible and infrared pointing centers, but it offset PlateScale is the first derivative of R −R with respect ir vis (5) R −R to time that causes the problem addressed in this Y = ir vis cos(PosAng−ParAng), paper. In the extreme case of an AO equipped offset PlateScale telescope atthe SouthPole,ADR, asdescribedin (6) this current report, is not a problem since targets wherePlateScaleisarcsecondsperpixelofthear- do not move in elevation angle. ray. The parallactic angle (ParAng) is a function of hour angle, declination, and latitude, Inordertofindtheinstantaneousrateofimage motion due to ADR we define the constant sin(H) tan(ParAng)= cos(δ)tan(φ)−sin(δ)cos(H). β = 206265 n2ir −1 − n2vis−1 (8) (7) PlateScale(cid:18) 2n2 2n2 (cid:19) ir vis In the coordinate system of elevation and az- and take the partial derivative of X and offset imuth, the motion of the infrared pointing center Y with respect to hour angle. offset relativeto the visible pointing center due to ADR is always along the elevation vector. However, most observations are made using a field rotator 3 ∂ X = (9) offset ∂H ∂z βsin(PosAng−ParAng)sec2(z ) t t ∂H ∂ParAng −βtan(z )cos(PosAng−ParAng) t ∂H ∂ Y = (10) offset ∂H ∂z βcos(PosAng−ParAng)sec2(z ) t t ∂H ∂ParAng +βtan(z )sin(PosAng−ParAng) t ∂H The partialderivativesofz andParAng with re- t spect to H are ∂ z = (11) t ∂H cos(δ)cos(φ)sin(H) Fig. 4.— (a) predicted image motion and (b) maxi- 1−(cos(H)cos(δ)cos(φ)+sin(δ)sin(φ))2 mumexposuretimesforanobservationat1.65µm(H- q band) of a target at declination +30◦ with the Keck 10-meter telescope assuming an effective wavelength ∂ of 0.65 µm for the wavefront sensor of the AO sys- ParAng = (12t)em. Each hourangleis markedbyacircle anda line ∂H pointing toward the zenith at that moment. The mo- cos(H)cos(δ)tan(φ)−sin(δ) tionduetoADRisnotnecessarilyalongtheelevation sin2(H)+(cos(H)sin(δ)−cos(δ)tan(φ))2 vector. Note that (a) does not depend on telescope aperture,butdoesdependonwavelengthsofobserva- The combination of eqns. 8, 12, and 13 with tion,declinationoftarget,andlatitudeofobservatory. The origin of the coordinate system in (a) lies at the d π radian visiblewavelength pointingcenter,which theAOsys- H = (13) temisholdingsteady. Maximumexposuretimein(b) dt 1800 minute iscalculatedfora10-meterdiametertelescopeandas- into eqns. 10 and 11 gives the instantaneous rate sumingmaximumallowedimagemotionof0.25ofthe FWHM of the diffraction limited point spread func- of image motion in the x/y-plane of the detector. tion. The IDL routine adr rateofmotion.pro included in the electronic version of this paper calculates this instantaneous rate of image motion. Output from these calculations for an observa- Finding the maximum exposure time allowed tion with the Keck telescope is shown in Fig. 4. before the image motion exceeds some givenlimit The predicted motion shown in Fig. 4a depends is not as straightforward as simply dividing the on site, but not diameter of telescope, while the desired image motion limit by the instantaneous maximum exposure times shown in Fig. 4b are rate of image motion at the start of the expo- based on the 10-meter diameter of the Keck tele- sure. This is because the image motion is usu- scopes. A smaller telescope has a coarser diffrac- ally curved in the x/y-plane and because the tionlimitandthereforeislessaffectedbytheissue second partial derivatives of X and Y ofdriftduetodifferentialrefraction,howeversome offset offset with respect to time are not constants. There- smallertelescopesareatlowersites(e.g.theShane fore, the most direct method of determining the 3-mofLickObservatory)wheredifferentialrefrac- maximum exposure time is to calculate X tion is greater. A smaller telescope ata higher al- offset and Y with fine time sampling and simply titude, higher latitude site suffers less from ADR offset search for the point at which the maximum de- than a larger telescope at a lower altitude, lower sired image motion has been exceeded. The IDL latitude site. The implications ofADR for several routine adr maxexptime.pro, included in the elec- current and proposed telescopes are discussed in tronic version of this paper, calculates the maxi- section 4. mum allowed exposure time. 4 Acriticalparameterincalculating the implica- tions of ADR is the effective wavelength of the reference source on the wavefront sensor. The wavefrontsensorof an AO systemis often photon limited and therefore designed to have as broad a wavelength bandpass as possible. In the case of a broad wavefront sensor bandpass, the effective wavelength of the reference source on the wave- front sensor depends on the color of source, as we will show in section 3 using observed data. Usu- ally of less importance is the effective wavelength of the target on the science instrument since the variation of air’s refractive index with wavelength is much less in the near-infrared than in the visi- ble. 3. Data Reduction and Analysis All the data presented here were taken using the W.M. Keck Observatory’s near-infrared spec- trographNIRSPEC behind the AO systemonthe Keck II 10-meter telescope. NIRSPEC contains two infrared arrays: a 1024 × 1024 InSb AL- ADDINforspectroscopyanda256×256HgCdTe PICNIC array as a slit-viewing camera (SCAM). The images of Titan shown in Fig. 1 were taken 2001 January 11 (UT) during high-spectral reso- lution long-exposure spectroscopy for a project of Eliot Young’s. This observing run was the first time we noticed the problems presented by atmo- Fig. 5.— Example images of HIP 110 and HIP sphericdifferentialrefractionwhenobservingwith 13117. These images have been processed using stan- dard near-infrared techniques of sky-subtraction and AO.TheimagesshowninFig.1are30-secondex- flat-fielding. Bad pixels have been replaced with the posures taken just 2.5 minutes apart and clearly median of their nearest 4 to 8 good neighbors. show a movement of ∼1 pixel, or ∼1/2 the full width at half maximum (fwhm) of the diffraction limit. 3.1. CalibrationofPlatescale andPosition Angle During the nights of 2001 August 20 and 21 (UT) James Lloyd and James Graham observed The platescale of SCAM behind AO was de- several binary stars as part of an ongoing search signed to well sample the core of a diffraction for low-mass companions. Images were taken of limited point spread function (PSF) in the near- eachfieldnearlycontinuouslyfor30to60minutes infrared with a pixel size of approximately 0′.′017. while neither adjusting the parameters of the AO InordertodeterminethetrueplatescaleofSCAM systemnoroffsettingthepointingofthetelescope. behind AO and confirm the accuracy of the We first discuss platescale and position angle cal- instrument-reported position angle, four Hippar- ibration using several Hipparcos binary star sys- cos binary systems chosen for their small uncer- tems. We then focus on data on two of Lloyd & tainty in separation and small parallax were ob- Graham’sstars(HIP110andHIP13117)toshow served earlier on the evenings of 2001 August 20 that on multi-minute time scales atmospheric dif- and 21 (UT) by de Pater et al.. The details of ferentialrefractionisthedominantimageblurring these plate scale calibrations are givenin Table 1. effect that is uncorrectedby the AO system. Fur- Each Hipparcos field was imaged at a number of ther, we use these data to show that the spectral positions aroundSCAM’s field-of-view in orderto type or color of the star is important when con- check for distortions. As noted in Table 1, three sidering how to correct for ADR. of the four fields were imaged a second time af- ter a 90◦ rotation of SCAM’s field-of-view. All 5 Table 1 Details of plate-scale calibration. Coadds× Assumed SCAM Hipparcos Measured Derived Star #of Exposure P.A.of Reported Measured Binary Separation PlateScale Name images Time Binarya P.A.b P.A.c Separation (pixels) (mas/pixel) HIP83634 14 10×0.1s 306◦.4 92◦.0 92◦.13±0◦.23 1′.′436±0′.′007 87.03±0.51 16.50±0.013 HIP83634 17 10×0.1s 306◦.4 2◦.0 1◦.95±0◦.29 1′.′436±0′.′007 87.24±0.49 16.46±0.012 HIP89947 6 50×0.2s 340◦.1 92◦.0 92◦.33±0◦.53 1′.′642±0′.′006 98.67±0.30 16.64±0.008 HIP91362 10 50×0.2s 223◦.2 82◦.0 82◦.63±0◦.35 1′.′050±0′.′009 61.88±0.52 16.97±0.020 HIP91362 10 50×0.2s 223◦.2 -8◦.0 -7◦.21±0◦.34 1′.′050±0′.′009 62.29±0.31 16.86±0.017 HIP100847 10 10×1.0s 129◦. -8◦.0 -8◦.28±0◦.24 0′.′871±0′.′010 51.59±0.23 16.88±0.021 HIP100847 10 10×1.0s 129◦. -98◦.0 -97◦.87±0◦.55 0′.′871±0′.′010 51.93±0.36 16.77±0.022 aPositionangleofsecondarystarrelativetoprimarystarasreportedintheHipparcoscatalog(ESA 1997). bPositionangleoftheSCAMdetectorreportedbytheinstrumenthardware. SeeFig.3fordefinition. cPosition angle of the SCAM detectordeterminedfromthe data assumingthe position angleof thebinary pair givenin ESA (1997)isperfect. of these data were taken in the H-band filter and 3.2. Measurement of Differential Refrac- wereprocessedusingstandardinfraredtechniques tion of sky subtraction and flat-field correction using The relevant ephemeris data and details of the data taken on the twilight sky. To measure the observationsofHIP110andHIP13117areshown x,yoffsetbetweentwostarsonthesameimagewe in Tables 2 and 3. Note that two separate se- rebinnedthe imageby afactorof8 (64newpixels quencesofdataweretakenonHIP110. Allofthe for each original pixel) using sampling and then stellar data were taken in the K-prime filter, each calculated the autocorrelationfunction image containing 100 coadds of 0.40 second ex- A=FFT−1(FFT(R)Conjugate(FFT(R))), posure. Each pair of binary stars were aligned on thechiptoavoidregionsofbadpixels. Theimages (14) wereprocessedusingstandardinfraredtechniques where R is the rebinned image, FFT represents a forward fast fourier transform, and FFT−1 repre- of bias subtraction and flat-field correction using data taken on the twilight sky. Those pixels that sents an inverse fast fourier transform. The posi- tion of the secondary maxima in A gives the x,y were flagged as bad were replaced with the me- dianoftheirnearest4-8goodneighbors. Example offset between the two stars. Table 1 gives the frames from both fields are shown in Fig. 5. Hipparcos measured position angle (PA) of each binarypair,the PAofthe detector asreportedby The goal of this exercise is to track the motion theinstrumenthardware,andthePAofthedetec- ofastaracrosstheseveraldozenimagesthatmake tor measured from the data assuming no motion up an exposure sequence. To do this we extract a of the stars since the epoch of the Hipparcos ob- regionof roughly±50pixels aroundthe starfrom servations. Further, Table 1 gives the Hipparcos each image of the sequence. In essence we then measurement of angular separation for each pair, oversample by a factor of 4 and find the peak of ourmeasuredseparationinpixels,andtheimplied the cross-correlationfunctionfor everypairofim- plate scale for our detector. For the current work ages in this extracted stack. From this matrix of weadoptaplatescaleof0′.′0167±0′.′0002perpixel, quarter-pixelresolutionoffsets betweeneverypair although we note that most of the uncertainty in of images we calculate a least-squares fit for the thisdeterminationofplatescaleappearstobedue relativeoffsetsoftheimages. Sinceeachfieldcon- to inaccuracies in the ‘known’ separation of the tains two stars we can do this for each star and binaries in the Hipparcos catalog,suggesting that obtain an internal cross-check on our method of these binaries have moved slightly in separation tracking image motion. Figure 6 shows the im- since the epoch of Hipparcos (1991.25). The posi- agemotionduringthesecondsequenceofHIP110 tionangledeterminationshowninTable1demon- observations as measured from each of the com- strates that the instrument-reported position an- ponents of HIP 110, which agree well with each gle is accurate to better than ∼0◦.5. other. This good agreement gives us confidence that our method of detecting image motion is not 6 Table 2 Binary stars used for fitting for the effects of ADR. Parallax Separationa Spectral Star mV (milliarcsec) B−Va V −Ia ∆HIPmaga,b (arcsec) Typec HIP110 8.61 20.42±1.91 0.787±0.003 0.820±0.007 0.64±0.03 1.197 GV HIP13117 11.69 29.67±9.34 1.460±0.022 1.85±0.10 0.64±0.22 1.679 MV aFromtheHipparcoscatalog(ESA 1997). bMagnitudedifferencebetweenthetwostarsofthebinaryintheESA (1997)definedpassband. cSpectraltypeandclassestimatedfromthetablesofDrilling& Landolt(2000) usingmV,parallax,B−V,and V −I. length of the star on SCAM. The parameter of interest being fit for is the effective wavelength of the reference star on the wavefront sensor. Also allowed to vary is the (x,y) position where the starwouldappearonSCAMattheeffectivewave- lengthofthewavefrontsensor. This(x,y)position is constant within an observing sequence. The re- sultsofthesefitsareshownwiththeircorrespond- ing observations in Fig. 7 and are summarized in Table 3. For the purposes of this fitting we as- sumed a typical atmospheric pressure and tem- perature for Mauna Kea of 456 mm Hg and 2◦C (Cohen&Cromer1988). Wealsoassumedawater vapor partial pressure of zero, although we found novariationinourresultsoverareasonablerange of watervapor partialpressuresfor the summit of Mauna Kea. Athoroughexaminationofthe uncertaintiesin our determination of effective wavelength on the Fig. 6.— Image motion during second sequence of wavefrontsensorisdifficult,primarilybecausethe HIP 110 observations as derived independently from residuals of the fits (dashed lines in Fig. 7) are each component of theHIP110 binary. clearly not randomly distributed. While most of theresidualimagemotionisattributabletoADR, affectedby issues suchasbadpixels, residualflat- thereappeartobeotherphenomenacausingresid- field noise, read-noise, etc. that would differ be- ual image motion at the several pixel level. tween the two stars. One method for better understanding the un- For each of the six observed sequences (2 com- certaintiesinbest-fitλ istorefitλ toaran- eff eff ponents of HIP 110 observed in two separate se- domly chosen fraction of the observations. For quences and 2 components of HIP 13117) we use each observational sequence we randomly chose the downhill simplex method ‘amoeba’ of Press, one half of the observations and refit for λ . eff Teukolsky, Vetterling, & Flannery (1992) as im- By repeating this procedure 1000 times for each plemented in the IDL software package to fit for observational sequence we made the error esti- the effect of ADR. The fixed parameters are: the mates shownin Table 3. The majorsource ofsys- zenithdistanceofeachobservation,theparallactic tematic uncertainty in λ is the uncertainty in eff angle of each observation, the relative (x,y) off- platescale, which adds an additional ±0.004 µm set of each observation, the platescale, the posi- uncertainty to the values of λ in Table 3. This eff tion angle of the SCAM array, the atmospheric is not a truly rigorous exercise in error analysis, pressure and temperature, the partial pressure of howeveritdoesshowthattheuncertaintiesinλ eff atmospheric water vapor, and the effective wave- for HIP 110 and HIP 13117 (∼<0.025 µm) are 7 Fig. 7.— Image motion for the brighter component of each binary pair. (a) is the first sequence of HIP 110 observations, (b)is thesecond sequenceof HIP110, and (c) is HIP13117. Thetriangles mark therelative positions of thestar from image to image. The solid line is the best-fit for themotion dueto ADR.The dashed lines connect each observation (triangle) with its corresponding point along the best-fit solid line. As shown in Fig. 6 the image motion derived from each binary component is nearly identical and therefore the fits to the secondary components are not shown in this figure, but the resulting best-fit effective wavelengths are included in Table 3. Also shown on (a),(b),and(c)aregrayarrowspointingtothezenithatthestartandendofeachsequenceofobservations. (d),(e), and (f) show the image motion residuals of the observations in (a), (b), and (c) after subtracting themotion due to ADR.NotetheasymmetryoftheresidualsinthecaseofHIP110in(d)and(e). Thisisduetothecloseseparationof HIP110influencingtheAOcorrectionasdescribedinthetext. Theorientationofthebinarypairineachobservation sequenceis indicated by an arrow. 8 muchlessthanthedifferencebetweenλ forHIP implemented this type of correction. However, eff 110andHIP13117(∼0.11µm). As expected, we in some cases for practical reasons implementing find that HIP 13117, an MV star, has a redder this correctionmaybe difficult, or λ ofthe ref- eff λ than HIP 110, which is a GV star. Our de- erence source on the wave-front sensor may not eff tection of the color difference between these two be well known. Knowing λ of the science tar- eff starsisrealandshowsthattofullycorrectforthe get on the science instrument is less critical since effectofADRthecoloroftheAOcalibratorsource the index of refraction of air varies much more must be taken into account. gradually at near-infrared wavelengths than visi- Figure 7 shows that the largestsource of resid- ble wavelengths. In the following sections we in- ual image motion is accounted for by ADR, how- vestigate both of these cases for several existing ever residuals of up to 1 to 2 pixels (0′.′017 − andproposedtelescopes. Analternativetechnique −0′.′034) remain, which are significant given that forADRcorrectionistoinsertanatmosphericdis- the diffraction limit resolution is 0′.′046 at 2.15 persion corrector between the telescope and AO µm. The source of the largest remaining resid- system. Thisapproachwouldbeeffectiveinmany uals is most likely due to the binary nature of situations, although it does invariably lead to at these stars. The AO system uses light from the leastsomelossofthroughputandincreaseinther- brighterofthetwostarstomeasurethewavefront mal background. Any increase in thermal back- distortion. In these observations a 1” field stop is ground is detrimental to observations at longer employed in front of the wavefront sensor in or- near-infraredwavelengths. Wealsodiscusstheim- der to block the light of the dimmer star from portance of considering the effect of ADR when reaching the sensor. With binaries of closer sep- attempting slit-spectroscopy with an AO system. aration, moments of worse seeing can cause light 4.1. Maximum Exposure Times from the dimmer star to leak in through the field stop. During these moments the AO correction Inthefollowingweadoptthemaximumaccept- is worse and the residual tip-tilt error in the di- abledriftinasingleexposuretobe0.25ofthefull rection of the position angle of the binary will be width half maximum (FWHM) of the diffraction larger. Insupportofthisargumentthatthelarger limitedcoreofthescienceinstrumentpointspread tip-tilt residualswe observearedue to this binary function (PSF), i.e. 1.04 λ/D radian, where λ is effect, we show in Fig. 7d-f the residuals of tip- the wavelength of the science observation and D tilt image motion after subtracting the effect of is the diameter of the telescope aperture. These ADR.ForbothobservationsofHIP110theseresid- calculationswereperformedforaλ ofthewave- eff uals are extremely asymmetrical in the x-y plane, front sensor of 0.65 µm and a science wavelength with the larger residuals parallel to the position of 1.65 µm, which is roughly the middle of H- angle of HIP110. In these data the position an- band. Foralloftheseexamplesweusethelatitude gle of HIP110 is approximately orthogonal to the of Mauna Kea observatory in Hawaii (19◦.826 N), direction of motion due to ADR. The residuals in but clearly if the sign of the target declination is the direction of motion due to ADR are approx- reversed then these figures would be correct for imately gaussian distributed with σ = 0.3 pixels. an observatory at 19◦.826 S latitude. In general, The stars of HIP13117are more widely separated an observer closer to the equator will be affected andthus the AO correctionis less affected by this morebyADRthananobserveratoneofthepoles, binary star issue. This is apparent in that the who will not have to contend with the problems residuals ofimage motion measuredfor HIP13117 discussed here. All of these calculations assumed are roughly symmetrically distributed in the x-y zero water vapor. In generalreasonablevalues for plane with a standard deviation of 0.3 pixels. the partial pressureof water have little impact on these calculations,but the implications ofvarying 4. Implications for Observing watervaporshouldbeconsideredifextremelyhigh precision is sought. See Section 2 for further de- Ideally one would know λ of the reference eff scriptionofthesecalculations. We aremakingthe source on the WFS and λ of the science target eff IDL code used in this work publicly available for on the science instrument. The AO system could anyone to use to examine the implications of at- then continuously correct for the calculated effect mospheric differential refraction for their favorite of differential refraction by inserting tip-tilt mo- telescopeandtarget. Afinalnoteisthatnearlyall tions inorderto keepthe sciencetargetsteadyon modern telescopes are built on altitude-azimuth the science instrument. Some AO systems have mounts which often have a zenith 9 Table 3 Details of observations and results of fitting for atmospheric differential refraction. Star UTTime Elevation #of Best-fitλeff Name Range Range images (µm)a HIP110a(#1b) 12:28-13:06 70◦.27-68◦.68 40 0.611±0.016 HIP110b(#1b) 12:28-13:06 70◦.27-68◦.68 40 0.608±0.014 HIP110a(#2b) 13:16-13:55 67◦.71-62◦.84 41 0.623±0.008 HIP110b(#2b) 13:16-13:55 67◦.71-62◦.84 41 0.623±0.007 HIP13117a 14:07-14:46 64◦.15-68◦.98 31 0.735±0.018 HIP13117b 14:07-14:46 64◦.15-68◦.98 31 0.730±0.019 aSeetextfordetailsoffitting. Thisistheeffectivewavelengthofthewave- frontsensoroftheAObenchwhenobservingthisstar. bThesenumbersrefertothefirstorsecondsequenceofobservationsonHIP 110. Fig. 8.— Maximum exposure time due to the effect of atmospheric differential refraction. All calculations assume λ of the wavefront sensor is 0.65 µm, science observations are at 1.65 µm, observatory latitude is 19◦.826 N, eff maximum allowed image motion is one quarterthe FWHM of the diffraction limited PSF at the science wavelength of1.65µm,andthatthereisnowatervapor. (a)isforthecaseofa4-metertelescopeatsealevel. (b)isforthecase of a 4-meter telescope on Mauna Kea, similar to NASA’sIRTF3-meter telescope or theCFHT 3.6-meter telescope. (c) is for the case of a 10-meter telescope on Mauna Kea, such as the Keck 10-meter telescopes. (d) is for the case of a 30-meter telescope on the summit of Mauna Kea. Note that maximum exposure time is not symmetric about transit. 10