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Implementation of an \mathcal{F}-statistic all-sky search for continuous gravitational waves in Virgo VSR1 data

LIGO Scientific Collaboration and Virgo Collaboration    J. Aasi1, B. P. Abbott1, R. Abbott1, T. Abbott2, M. R. Abernathy1, T. Accadia3, F. Acernese4,5, K. Ackley6, C. Adams7, T. Adams8, P. Addesso5, R. X. Adhikari1, C. Affeldt9, M. Agathos10, N. Aggarwal11, O. D. Aguiar12, A. Ain13, P. Ajith14, A. Alemic15, B. Allen9,16,17, A. Allocca18,19, D. Amariutei6, M. Andersen20, R. Anderson1, S. B. Anderson1, W. G. Anderson16, K. Arai1, M. C. Araya1, C. Arceneaux21, J. Areeda22, S. M. Aston7, P. Astone23, P. Aufmuth17, C. Aulbert9, L. Austin1, B. E. Aylott24, S. Babak25, P. T. Baker26, G. Ballardin27, S. W. Ballmer15, J. C. Barayoga1, M. Barbet6, B. C. Barish1, D. Barker28, F. Barone4,5, B. Barr29, L. Barsotti11, M. Barsuglia30, M. A. Barton28, I. Bartos31, R. Bassiri20, A. Basti18,32, J. C. Batch28, J. Bauchrowitz9, Th. S. Bauer10, B. Behnke25, M. Bejger33, M. G. Beker10, C. Belczynski34, A. S. Bell29, C. Bell29, G. Bergmann9, D. Bersanetti35,36, A. Bertolini10, J. Betzwieser7, 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California Institute of Technology, Pasadena, CA 91125, USA 2Louisiana State University, Baton Rouge, LA 70803, USA 3Laboratoire d’Annecy-le-Vieux de Physique des Particules (LAPP), Université de Savoie, CNRS/IN2P3, F-74941 Annecy-le-Vieux, France 4INFN, Sezione di Napoli, Complesso Universitario di Monte S.Angelo, I-80126 Napoli, Italy 5Università di Salerno, Fisciano, I-84084 Salerno, Italy 6University of Florida, Gainesville, FL 32611, USA 7LIGO - Livingston Observatory, Livingston, LA 70754, USA 8Cardiff University, Cardiff, CF24 3AA, United Kingdom 9Albert-Einstein-Institut, Max-Planck-Institut für Gravitationsphysik, D-30167 Hannover, Germany 10Nikhef, Science Park, 1098 XG Amsterdam, The Netherlands 11LIGO - Massachusetts Institute of Technology, Cambridge, MA 02139, USA 12Instituto Nacional de Pesquisas Espaciais, 12227-010 - São José dos Campos, SP, Brazil 13Inter-University Centre for Astronomy and Astrophysics, Pune - 411007, India 14Tata Institute for Fundamental Research, Mumbai 400005, India 15Syracuse University, Syracuse, NY 13244, USA 16University of Wisconsin–Milwaukee, Milwaukee, WI 53201, USA 17Leibniz Universität Hannover, D-30167 Hannover, Germany 18INFN, Sezione di Pisa, I-56127 Pisa, Italy 19Università di Siena, I-53100 Siena, Italy 20Stanford University, Stanford, CA 94305, USA 21The University of Mississippi, University, MS 38677, USA 22California State University Fullerton, Fullerton, CA 92831, USA 23INFN, Sezione di Roma, I-00185 Roma, Italy 24University of Birmingham, Birmingham, B15 2TT, United Kingdom 25Albert-Einstein-Institut, Max-Planck-Institut für Gravitationsphysik, D-14476 Golm, Germany 26Montana State University, Bozeman, MT 59717, USA 27European Gravitational Observatory (EGO), I-56021 Cascina, Pisa, Italy 28LIGO - Hanford Observatory, Richland, WA 99352, USA 29SUPA, University of Glasgow, Glasgow, G12 8QQ, United Kingdom 30APC, AstroParticule et Cosmologie, Université Paris Diderot, CNRS/IN2P3, CEA/Irfu, Observatoire de Paris, Sorbonne Paris Cité, 10, rue Alice Domon et Léonie Duquet, F-75205 Paris Cedex 13, France 31Columbia University, New York, NY 10027, USA 32Università di Pisa, I-56127 Pisa, Italy 33CAMK-PAN, 00-716 Warsaw, Poland 34Astronomical Observatory Warsaw University, 00-478 Warsaw, Poland 35INFN, Sezione di Genova, I-16146 Genova, Italy 36Università degli Studi di Genova, I-16146 Genova, Italy 37San Jose State University, San Jose, CA 95192, USA 38Faculty of Physics, Lomonosov Moscow State University, Moscow 119991, Russia 39LAL, Université Paris-Sud, IN2P3/CNRS, F-91898 Orsay, France 40NASA/Goddard Space Flight Center, Greenbelt, MD 20771, USA 41University of Western Australia, Crawley, WA 6009, Australia 42Department of Astrophysics/IMAPP, Radboud University Nijmegen, P.O. Box 9010, 6500 GL Nijmegen, The Netherlands 43Université Nice-Sophia-Antipolis, CNRS, Observatoire de la Côte d’Azur, F-06304 Nice, France 44Institut de Physique de Rennes, CNRS, Université de Rennes 1, F-35042 Rennes, France 45Laboratoire des Matériaux Avancés (LMA), IN2P3/CNRS, Université de Lyon, F-69622 Villeurbanne, Lyon, France 46Centre for Astronomy, Nicolaus Copernicus University, 87-100 Toruń, Poland 47Washington State University, Pullman, WA 99164, USA 48INFN, Sezione di Perugia, I-06123 Perugia, Italy 49INFN, Sezione di Firenze, I-50019 Sesto Fiorentino, Firenze, Italy 50Università degli Studi di Urbino ’Carlo Bo’, I-61029 Urbino, Italy 51University of Oregon, Eugene, OR 97403, USA 52Laboratoire Kastler Brossel, ENS, CNRS, UPMC, Université Pierre et Marie Curie, F-75005 Paris, France 53VU University Amsterdam, 1081 HV Amsterdam, The Netherlands 54University of Maryland, College Park, MD 20742, USA 55University of Massachusetts - Amherst, Amherst, MA 01003, USA 56Universitat de les Illes Balears, E-07122 Palma de Mallorca, Spain 57Università di Napoli ’Federico II’, Complesso Universitario di Monte S.Angelo, I-80126 Napoli, Italy 58Canadian Institute for Theoretical Astrophysics, University of Toronto, Toronto, Ontario, M5S 3H8, Canada 59Tsinghua University, Beijing 100084, China 60University of Michigan, Ann Arbor, MI 48109, USA 61Rochester Institute of Technology, Rochester, NY 14623, USA 62INFN, Sezione di Roma Tor Vergata, I-00133 Roma, Italy 63National Tsing Hua University, Hsinchu Taiwan 300 64Charles Sturt University, Wagga Wagga, NSW 2678, Australia 65Caltech-CaRT, Pasadena, CA 91125, USA 66Pusan National University, Busan 609-735, Korea 67Australian National University, Canberra, ACT 0200, Australia 68Carleton College, Northfield, MN 55057, USA 69INFN, Gran Sasso Science Institute, I-67100 L’Aquila, Italy 70Università di Roma Tor Vergata, I-00133 Roma, Italy 71Università di Roma ’La Sapienza’, I-00185 Roma, Italy 72University of Brussels, Brussels 1050 Belgium 73Sonoma State University, Rohnert Park, CA 94928, USA 74Embry-Riddle Aeronautical University, Prescott, AZ 86301, USA 75The George Washington University, Washington, DC 20052, USA 76University of Cambridge, Cambridge, CB2 1TN, United Kingdom 77Northwestern University, Evanston, IL 60208, USA 78University of Minnesota, Minneapolis, MN 55455, USA 79The University of Texas at Brownsville, Brownsville, TX 78520, USA 80The University of Sheffield, Sheffield S10 2TN, United Kingdom 81Wigner RCP, RMKI, H-1121 Budapest, Konkoly Thege Miklósút 29-33, Hungary 82University of Sannio at Benevento, I-82100 Benevento, Italy 83NCBJ, 05-400Świerk-Otwock, Poland 84INFN, Gruppo Collegato di Trento, I-38050 Povo, Trento, Italy 85Università di Trento, I-38050 Povo, Trento, Italy 86Montclair State University, Montclair, NJ 07043, USA 87The Pennsylvania State University, University Park, PA 16802, USA 88MTA Eötvös University, ‘Lendulet’ A. R. G., Budapest 1117, Hungary 89Università di Perugia, I-06123 Perugia, Italy 90Rutherford Appleton Laboratory, HSIC, Chilton, Didcot, Oxon, OX11 0QX, United Kingdom 91Perimeter Institute for Theoretical Physics, Waterloo, Ontario, N2L 2Y5, Canada 92American University, Washington, DC 20016, USA 93University of Adelaide, Adelaide, SA 5005, Australia 94Raman Research Institute, Bangalore, Karnataka 560080, India 95Korea Institute of Science and Technology Information, Daejeon 305-806, Korea 96Białystok University, 15-424 Białystok, Poland 97University of Southampton, Southampton, SO17 1BJ, United Kingdom 98IISER-TVM, CET Campus, Trivandrum Kerala 695016, India 99Institute of Applied Physics, Nizhny Novgorod, 603950, Russia 100Seoul National University, Seoul 151-742, Korea 101Hanyang University, Seoul 133-791, Korea 102IM-PAN, 00-956 Warsaw, Poland 103Institute for Plasma Research, Bhat, Gandhinagar 382428, India 104The University of Melbourne, Parkville, VIC 3010, Australia 105INFN, Sezione di Padova, I-35131 Padova, Italy 106Monash University, Victoria 3800, Australia 107SUPA, University of Strathclyde, Glasgow, G1 1XQ, United Kingdom 108ESPCI, CNRS, F-75005 Paris, France 109Argentinian Gravitational Wave Group, Cordoba Cordoba 5000, Argentina 110Università di Camerino, Dipartimento di Fisica, I-62032 Camerino, Italy 111The University of Texas at Austin, Austin, TX 78712, USA 112Southern University and A&M College, Baton Rouge, LA 70813, USA 113College of William and Mary, Williamsburg, VA 23187, USA 114IISER-Kolkata, Mohanpur, West Bengal 741252, India 115National Institute for Mathematical Sciences, Daejeon 305-390, Korea 116Hobart and William Smith Colleges, Geneva, NY 14456, USA 117Gjøvik videregående skole, P.b. 534, N-2803 Gjøvik, Norway 118RRCAT, Indore MP 452013, India 119SUPA, University of the West of Scotland, Paisley, PA1 2BE, United Kingdom 120Institute of Astronomy, 65-265 Zielona Góra, Poland 121Indian Institute of Technology, Gandhinagar Ahmedabad Gujarat 382424, India 122Instituto de Física Teórica, Univ. Estadual Paulista/International Center for Theoretical Physics-South American Institue for Research, São Paulo SP 01140-070, Brazil 123Andrews University, Berrien Springs, MI 49104, USA 124Trinity University, San Antonio, TX 78212, USA 125University of Washington, Seattle, WA 98195, USA 126Southeastern Louisiana University, Hammond, LA 70402, USA 127Abilene Christian University, Abilene, TX 79699, USA
Abstract

We present an implementation of the \mathcal{F}-statistic to carry out the first search in data from the Virgo laser interferometric gravitational wave detector for periodic gravitational waves from a priori unknown, isolated rotating neutron stars. We searched a frequency f0f_{0} range from 100 Hz to 1 kHz and the frequency dependent spindown f1f_{1} range from 1.6(f0/100Hz)×109-1.6\,(f_{0}/100\,{\rm Hz})\times 10^{-9}\, Hz/s to zero. A large part of this frequency - spindown space was unexplored by any of the all-sky searches published so far. Our method consisted of a coherent search over two-day periods using the \mathcal{F}-statistic, followed by a search for coincidences among the candidates from the two-day segments. We have introduced a number of novel techniques and algorithms that allow the use of the Fast Fourier Transform (FFT) algorithm in the coherent part of the search resulting in a fifty-fold speed-up in computation of the \mathcal{F}-statistic with respect to the algorithm used in the other pipelines. No significant gravitational wave signal was found. The sensitivity of the search was estimated by injecting signals into the data. In the most sensitive parts of the detector band more than 90% of signals would have been detected with dimensionless gravitational-wave amplitude greater than 5×10245\times 10^{-24}.

pacs:
04.80.Nn, 95.55.Ym, 97.60.Gb, 07.05.Kf

1 Introduction

This paper presents results from a wide parameter search for periodic gravitational waves from spinning neutron stars using data from the Virgo detector [1]. The data used in this paper were produced during Virgo’s first science run (VSR1) which started on May 18, 2007 and ended on October 1, 2007. The VSR1 data has never been searched for periodic gravitational waves from isolated neutron stars before. The innovation of the search is the combination of the efficiency of the FFT algorithm together with a nearly optimal grid of templates.

Rotating neutron stars are promising sources of gravitational radiation in the band of ground-based laser interferometric detectors (see [2] for a review). In order for these objects to emit gravitational waves, they must exhibit some asymmetry, which could be due to imperfections of the neutron star crust or the influence of strong internal magnetic fields (see [3] for recent results). Gravitational radiation also may arise due to the r-modes, i.e., rotation-dominated oscillations driven unstable by the gravitational emission (see [4] for discussion of implications of r-modes for GW searches). Neutron star precession is another gravitational wave emission mechanism (see [5] for a recent study). Details of the above mechanisms of gravitational wave emission can be found in [6, 7, 8, 9, 10, 11].

A signal from a rotating neutron star can be modeled independently of the specific mechanism of gravitational wave emission as a nearly periodic wave the frequency of which decreases slowly during the observation time due to the rotational energy loss. The signal registered by an Earth-based detector is both amplitude and phase modulated because of the motion of the Earth with respect to the source.

The gravitational wave signal from such a star is expected to be very weak, and therefore months-long segments of data must be analyzed. The maximum deformation that a neutron star can sustain, measured by the ellipticity parameter ϵ\epsilon (Eq. (7)), ranges from 5×1065\times 10^{-6} for ordinary matter [7, 12] to 10410^{-4} for strange quark matter [10, 11]. For unknown neutron stars one needs to search a very large parameter space. As a result, fully coherent, blind searches are computationally prohibitive. To perform a fully coherent search of VSR1 data in real time (i.e., in time of 136 days of duration of the VSR1 run) over the parameter space proposed in this paper would require a 1.4×1041.4\times 10^{4} petaflop computer [13].

A natural way to reduce the computational burden is a hierarchical scheme, where first short segments of data are analyzed coherently, and then results are combined incoherently. This leads to computationally manageable searches at the expense of the signal-to-ratio loss. To perform the hierarchical search presented in this paper in real time a 2.82.8 teraflop computer is required. One approach is to use short segments of the order of half an hour long so that the the signal remains within a single Fourier frequency bin in each segment and thus a single Fourier transform suffices to extract the whole power of the gravitational wave signal in each segment. Three schemes were developed for the analysis of Fourier transforms of the short data segments and they were used in the all-sky searches of ground interferometer data: the “stack-slide” [14], the “Hough transform” [15, 14], and the “PowerFlux” methods [14, 16, 17].

Another hierarchical scheme involves using longer segment duration for which signal modulations need to be taken into account. For segments of the order of days long, coherent analysis using the popular \mathcal{F}-statistic [18] is computationally demanding, but feasible. For example the hierarchical search of VSR1 data presented in this paper requires around 1900 processor cores for the time of 136 days which was the duration of the VSR1 run. In the hierarchical scheme the first coherent analysis step is followed by a post-processing step where data obtained in the first step are combined incoherently. This scheme was implemented by the distributed volunteer computing project Einstein@Home [19]. The E@H project performed analysis of LIGO S4 and S5 data, leading to results published in three papers. In the first two, [20, 21], the candidate signals from the coherent analysis were searched for coincidences. In the third paper [22] the results from the coherent search were analyzed using a Hough-transform scheme.

The search method used here is similar to the one used in the first two E@H searches: it consists of coherent analysis by means of the \mathcal{F}-statistic, followed by a search for coincidences among the candidates obtained in the coherent analysis. There are, however, important differences: in this search we have a fixed threshold for the coherent analysis, resulting in a variable number of candidates from analysis of each of the data segments. Moreover, for different bands we have a variable number of two-day data segments (see Section 3 for details). In E@H searches the number of candidates used in coincidences from each data segment was the same, as was the number of data segments for each band. In addition, the duration of data segments for coherent analysis in the two first E@H searches was 30h (48h in this case).

In this analysis we have implemented algorithms and techniques that considerably improve the efficiency of this search. Most importantly we have used the FFT algorithm to evaluate the \mathcal{F}-statistic for two-day data segments. Also we were able to use the FFT algorithm together with a grid of templates that was only 20% denser than the best known grid (i.e., the one with the least number of points).

Given that the data we analyzed (Virgo VSR1) had a higher noise and the duration was shorter than the LIGO S5 data we have achieved a lower sensitivity than in the most recent E@H search [22]. However due to very good efficiency of our code we were able to analyze a much larger parameter space. We have analyzed a large part of the ff˙f-\dot{f} plane that was previously unexplored by any of the all-sky searches. For example in this analysis the ff˙f-\dot{f} plane searched was 6.56.5 larger than that in the full S5 E@H search [22] (see Figure 5). In addition, the data from the Virgo detector is characterized by different spectral artifacts (instrumental and environmental) from these seen in LIGO data. As a results, certain narrow bands excluded from LIGO searches because of highly non-Gaussian noise can be explored in this analysis.

The paper is organized as follows. In Section 2 we describe the data from the Virgo detector VSR1 run, in Section 3 we explain how the data were selected. In Section 4 the response of the detector to a gravitational wave signal from a rotating neutron star is briefly recalled. In Section 5 we introduce the \mathcal{F}-statistic. In Section 6 we describe the search method and present the algorithms for an efficient calculation of the \mathcal{F}-statistic. In Section 7 we describe the vetoing procedure of the candidates. In Section 8 we present the coincidence algorithm that is used for post-processing of the candidates. Section 9 contains results of the analysis. In Section 10 we determine the sensitivity of this search, and we conclude the paper by Section 11. In A we present a general formula for probability that is used in the estimation of significance of the coincidences.

2 Data from the Virgo’s first science run

The VSR1 science run spanned more than four months of data acquisition. This run started on May 18, 2007 at 21:00 UTC and ended on October 1, 2007 at 05:00 UTC. The detector was running close to its design sensitivity with a duty cycle of 81.0% [23]. The data were calibrated, and the time series of the gravitational wave strain h(t)h(t) was reconstructed. In the range of frequencies from 10Hz to 10kHz the systematic error in amplitude was 6% and the phase error was 70 mrad below the frequency of 1.9 kHz [24]. A snapshot of the amplitude spectral density of VSR1 data in the Virgo detector band is presented in Figure 1.

Refer to caption
Figure 1: Strain amplitude spectral density Sh\sqrt{S_{h}} of Virgo data taken on May 25, 2007 during the VSR1 run.

3 Data selection

The analysis input consists of narrow-band time-domain data segments. In order to obtain these sequences from VSR1 data, we have used the software described in [25], and extracted the segments from the Short Fourier Transform Database (SFDB). The time domain data sequences were extracted with a certain sampling time Δt\Delta t, time duration Tobs{T_{\mathrm{obs}}} and offset frequency fofff_{\rm off}. Thus each time domain sequence has the band [foff,foff+B][f_{\rm off},f_{\rm off}+B], where B=1/2×1/ΔtB=1/2\times 1/\Delta t. We choose the segment duration to be exactly two sidereal days and the sampling time equal to 1/21/2 s, i.e., the bandwidth B=1B=1 Hz. As a result each narrow band time segment contains N=344 656N=344\,656 data points. We have considered 67 two-day time frames for the analysis. The starting time of the analysis (the time of the first sample of the data in the first time frame) was May 19, 2007 at 00:00 UTC. The data in each time frame d=1,,67d=1,\dots,67 were divided into narrow band sequences of 1Hz band each. The bands overlap by 252^{-5} Hz resulting in 929 bands numbered from 0 to 928. The relation between the band number bb and the offset frequency fofff_{\rm off} is thus given by

foff[Hz]=100+(125)b.f_{\rm off}\mbox{[Hz]}=100+(1-2^{-5})\,b. (1)

Consequently, we have 62 243 narrow band data segments. From this set we selected good data using the following conditions. Let N0N_{0} be the number of zeros in a given data segment (data point set to zero means that at that time there was no science data). Let [foff,foff+B][f_{\rm off},f_{\rm off}+B] be the band of a given data segment. Let SminS_{min} and SmaxS_{max} be the minimum and the maximum of the amplitude spectral density in the interval [foff+0.05B,foff+B0.05B][f_{\rm off}+0.05B,f_{\rm off}+B-0.05B]. Spectral density was estimated by dividing the data of a given segment into short stretches and averaging spectra of all the short stretches. We consider the data segment as good data and use it in this analysis, if the following two criteria are met:

  1. 1.

    N0/N<1/4N_{0}/N<1/4,

  2. 2.

    Smax/Smin1.1S_{max}/S_{min}\leq 1.1.

20 419 data segments met the above two criteria. Figure 2 shows a time-frequency distribution of the good data segments.

Refer to caption
Figure 2: A map of the VSR1 data. Grey - good data selected for the analysis, white - data not analyzed because of large number of missing data or a strong variation of the spectrum, black - bad data where number of missing data is greater than 50% or there are strong lines from mirror wires, electronics, etc.

The good data appeared in 50 out of 67 two-day time frames and in 785 out of 929 bands. The distribution of good data segments in time frames and in bands is given in Figure 3.

Refer to caption
Refer to caption
Figure 3: Number of good data segments. Left panel - distribution of data segments in frequency bands. The number of data segments chosen for the analysis in a given frequency band varies from 1 to 50. Right panel - distribution of data segments time frames. The number of data segments in a given time frame varies from 54 to 520. The smallest, outlying number of bands of 54 is in the 5th time frame. In the remaining frames the number of good bands is greater than 300.

In Figure 4 we plot a snapshot spectral density of VSR1 data presented in Figure 1 and an estimate of the spectral density of the data that was used in the analysis. We estimate the spectral density in each band by a harmonic mean of the spectral densities of each of the two-day time segments chosen for the analysis in the band. As the data spectrum in each band is approximately white, we estimate the spectral density in each time segment by 2σ2Δt2\sigma^{2}\Delta t, where σ2\sigma^{2} is the variance of the data in a segment and Δt\Delta t is the 1/21/2s sampling time. We plot the band from 100Hz to 1 kHz which we have chosen for this search.

Refer to caption
Figure 4: A snapshot of strain amplitude spectral density Sh\sqrt{S_{h}} of the VSR1 data (grey curve) in comparison with the spectral density estimated from the data used in the analysis (black dots). The spectrum in each band is obtained from a harmonic mean of the spectral densities of the data in each segment chosen for the analysis in the band.

4 The response of the detector

The dimensionless noise-free response hh of a gravitational-wave detector to a weak plane gravitational wave in the long wavelength approximation, i.e., when the characteristic size of the detector is much smaller than the reduced wavelength λ/(2π)\lambda/(2\pi) of the wave, can be written as the linear combination of the two independent wave polarizations h+h_{+} and h×h_{\times},

h(t)=F+(t)h+(t)+F×(t)h×(t),h(t)=F_{+}(t)h_{+}(t)+F_{\times}(t)h_{\times}(t), (2)

where F+F_{+} and F×F_{\times} are the detector’s beam-pattern functions,

F+(t)=a(t)cos2ψ+b(t)sin2ψ,\displaystyle F_{+}(t)=a(t)\cos 2\psi+b(t)\sin 2\psi, (3)
F×(t)=b(t)cos2ψa(t)sin2ψ.\displaystyle F_{\times}(t)=b(t)\cos 2\psi-a(t)\sin 2\psi. (4)

The beam-patterns F+F_{+} and F×F_{\times} are linear combinations of sin2ψ\sin 2\psi and cos2ψ\cos 2\psi, where ψ\psi is the polarization angle of the wave. The functions a(t)a(t) and b(t)b(t) are the amplitude modulation functions, that depend on the location and orientation of the detector on the Earth and on the position of the gravitational-wave source in the sky, described in the equatorial coordinate system by the right ascension α\alpha and the declination δ\delta angles. They are periodic functions of time with the period of one and two sidereal days. The analytic form of the functions a(t)a(t) and b(t)b(t) for the case of interferometric detectors is given by Eqs. (12) and (13) of [18]. For a rotating nonaxisymmetric neutron star, the wave polarization functions are of the form

h+(t)=h0+cos(ϕ(t)+ϕ0),h×(t)=h0×sin(ϕ(t)+ϕ0),h_{+}(t)=h_{0+}\cos(\phi(t)+\phi_{0}),\\ h_{\times}(t)=h_{0\times}\sin(\phi(t)+\phi_{0}), (5)

where h0+h_{0+} and h0×h_{0\times} are constant amplitudes of the two polarizations and ϕ(t)+ϕ0\phi(t)+\phi_{0} is the phase of the wave, ϕ0\phi_{0} being the initial phase of the waveform. The amplitudes h0+h_{0+} and h0×h_{0\times} depend on the physical mechanism responsible for the gravitational radiation, e.g., if a neutron star is a triaxial ellipsoid rotating around a principal axis with frequency ff, then these amplitudes are

h0+=12h0(1+cos2ι),h0×=h0cosι,h_{0+}=\frac{1}{2}h_{0}(1+\cos^{2}\iota),\\ h_{0\times}=h_{0}\cos\iota, (6)

where ι\iota is the angle between the star’s angular momentum vector and the direction from the star to the Earth, and the amplitude h0h_{0} is given by

h0=16π2Gc4ϵIf2r.h_{0}=\frac{16\pi^{2}G}{c^{4}}\frac{\epsilon If^{2}}{r}. (7)

Here II is the star’s moment of inertia with respect to the rotation axis, rr is the distance to the star, and ϵ\epsilon is the star’s ellipticity defined by ϵ=|I1I2|/I\epsilon=|I_{1}-I_{2}|/I, where I1I_{1} and I2I_{2} are moments of inertia with respect to the principal axes orthogonal to the rotation axis. We assume that the gravitational waveform given by Eqs. (2)–(5) is almost monochromatic around some angular frequency ω0\omega_{0}, which we define as instantaneous angular frequency evaluated at the solar system barycenter (SSB) at t=0t=0, and we assume that the frequency evolution is accurately described by one spindown parameter ω1\omega_{1}. Then the phase ϕ(t)\phi(t) is given by

ϕ(t)=ω0t+ω1t2+𝐧𝐫d(t)c(ω0+2ω1t),\phi(t)=\omega_{0}t+\omega_{1}t^{2}+\frac{{\bf n}\cdot{\bf r}_{d}(t)}{c}(\omega_{0}+2\omega_{1}t), (8)

where, neglecting the relativistic effects, 𝐫d(t){\bf r}_{d}(t) is the vector that joins the SSB with the detector, and 𝐧{\bf n} is the unit vector pointing from SSB to the source. In equatorial coordinates (δ(\delta, α)\alpha) we have 𝐧=(cosδcosα,cosδsinα,sinδ){\bf n}=(\cos\delta\cos\alpha,\cos\delta\sin\alpha,\sin\delta).

5 The \mathcal{F} - statistic

A method to search for gravitational wave signals from a rotating neutron star in a detector data x(t),t=1,,Nx(t),t=1,...,N uses the \mathcal{F}-statistic, described in [18]. The \mathcal{F}-statistic is obtained by maximizing the likelihood function with respect to the four unknown parameters - h0h_{0}, ϕ0\phi_{0}, ι\iota, and ψ\psi. This leaves a function of only the remaining four parameters - ω0\omega_{0}, ω1\omega_{1}, δ\delta, and α\alpha. Thus the dimension of the parameter space that we need to search decreases from 8 to 4. In this analysis we shall use an observation time Tobs{T_{\mathrm{obs}}} equal to the integer multiple of sidereal days. Since the bandwidth of the signal over our coherent observation time of two days is very small, we can assume that over this band the spectral density of the noise is white (constant). Under these assumptions the \mathcal{F}-statistic is given by [26, 27]

2σ2(|Fa|2a2+|Fb|2b2),\mathcal{F}\approx\frac{2}{\sigma^{2}}\left(\frac{|F_{a}|^{2}}{\left\langle a^{2}\right\rangle}+\frac{|F_{b}|^{2}}{\left\langle b^{2}\right\rangle}\right), (9)

where σ2\sigma^{2} is the variance of the data, and

Fa:=t=1Nx(t)a(t)exp[iϕ(t)],\displaystyle F_{a}:=\sum^{N}_{t=1}x(t)\,a(t)\exp[-\mathrm{i}\phi(t)], (10)
Fb:=t=1Nx(t)b(t)exp[iϕ(t)].\displaystyle F_{b}:=\sum^{N}_{t=1}x(t)\,b(t)\exp[-\mathrm{i}\phi(t)].
a2=t=1Na(t)2,b2=t=1Nb(t)2.\left\langle a^{2}\right\rangle=\sum^{N}_{t=1}a(t)^{2},\,\,\,\left\langle b^{2}\right\rangle=\sum^{N}_{t=1}b(t)^{2}. (11)

6 Description of the search

The search consists of two parts; the first part is a coherent search of two-day data segments, where we search a 4-parameter space defined by angular frequency ω0\omega_{0}, angular frequency derivative ω1\omega_{1}, declination δ\delta, and right ascension α\alpha. The search is performed on a 4-dimensional grid in the parameter space described in Section 6.2. We set a fixed threshold of 20 for the \mathcal{F}-statistic for each data segment. This corresponds to a threshold of 6 for the signal-to-noise ratio. All the threshold crossings are recorded together with corresponding 4 parameters of the grid point and the signal-to-noise ratio ρ\rho. The signal-to-noise is calculated from the value of the \mathcal{F}-statistic at the threshold crossing as

ρ=2(2).\rho=\sqrt{2(\mathcal{F}-2)}. (12)

In this way for each narrow band segment we obtain a set of candidates. The candidates are then subject to the vetoing procedure described in Section 7. The second part of the search is the post-processing stage involving search for coincidences among the candidates. The coincidence procedure is described in Section 8.

6.1 Choice of the parameter space

We have searched the frequency band from 100 Hz to 1 kHz over the entire sky. We have followed [13] to constrain the maximum value of the parameter ω1\omega_{1} for a given frequency ω0\omega_{0} by |ω1|ω0/(2τmin)|\omega_{1}|\leq\omega_{0}/(2\tau_{min}), where τmin\tau_{min} is the minimum spindown age111The factor of two in this formula appears here because the spindown parameter f˙\dot{f} used in [13] is twice the spindown parameter used in this work.. We have chosen τmin=1000\tau_{min}=1000yr for the whole frequency band searched. Also, in this search we have considered only the negative values for the parameter ω1\omega_{1}, thus assuming that the rotating neutron star is spinning down. This gives the frequency-dependent range of the spindown parameter f1f_{1} where f1=ω1/(2π)f_{1}=\omega_{1}/(2\pi):

|f1|1.6×109f100Hz1000yrτmin[Hzs1]|f_{1}|\leq 1.6\times 10^{-9}\frac{f}{100{\mbox{H}z}}\frac{1000{\mbox{y}r}}{\tau_{min}}[{\mbox{H}zs}^{-1}] (13)

We have considered only one frequency derivative. Estimates taking into account parameter correlations (see [13] Figure 6 and Eqs. (6.2) - (6.6)) show that even for the minimum spindown age of 4040yr and for two days coherent observation time that we consider here, it is sufficient to include just one spindown parameter.

In Figure 5 we have compared the parameter space searched in this analysis in the ff˙f-\dot{f} plane with that of other recently published all-sky searches: Einstein@Home early S5 search [21], Einstein@Home full S5 [22], PowerFlux early S5 [28], PowerFlux full S5 [17].

Refer to caption
Figure 5: Comparison of the parameter space in ff˙f-\dot{f} plane searched in VSR1 analysis presented in this paper (area enclosed by a thick black line) and recently published PowerFlux and E@H searches of the LIGO S5 data.

6.2 Efficient calculation of the \mathcal{F}-statistic on the grid in the parameter space

Calculation of the \mathcal{F}-statistic (Eq. (9)) involves two sums given by Eqs. (10). By introducing a new time variable called the barycentric time tbt_{b} ([29, 18, 27])

tb:=t+𝐧𝐫d(t)c.t_{b}:=t+\frac{{\bf n}\cdot{\bf r}_{d}(t)}{c}. (14)

we can write these sums as discrete Fourier transforms in the following way

Fa=tb=1Nx(t(tb))a(t(tb))exp[iϕs(t(tb))]exp[iω0tb],\displaystyle F_{a}=\sum^{N}_{t_{b}=1}x(t(t_{b}))\,a(t(t_{b}))\exp[-\mathrm{i}\phi_{s}(t(t_{b}))]\exp[-\mathrm{i}\omega_{0}t_{b}], (15)
Fb=tb=1Nx(t(tb))b(t(tb))exp[iϕs(t(tb))]exp[iω0tb],\displaystyle F_{b}=\sum^{N}_{t_{b}=1}x(t(t_{b}))\,b(t(t_{b}))\exp[-\mathrm{i}\phi_{s}(t(t_{b}))]\exp[-\mathrm{i}\omega_{0}t_{b}],

where

ϕs(t)=ω1t2+2𝐧𝐫d(t)cω1t.\phi_{s}(t)=\omega_{1}t^{2}+2\frac{{\bf n}\cdot{\bf r}_{d}(t)}{c}\omega_{1}t. (16)

Written in this form, the two sums can be evaluated using the Fast Fourier Transform (FFT) algorithm thus speeding up their computation dramatically. The time transformation described by equation (14) is called resampling. In addition to the use of the FFT algorithm we apply an interpolation of the FFT using the interbinning procedure (see [27] Section VB). This results in the \mathcal{F}-statistic sampled twice as fine with respect to the standard FFT. This procedure is much faster than the interpolation of the FFT obtained by padding the data with zeroes and calculating a FFT that is twice as long. With the approximations described above for each value of the parameters ω1\omega_{1}, δ\delta, and α\alpha, we calculate the \mathcal{F}-statistic efficiently for all the frequency bins in the data segment of bandwidth 1Hz.

In order to search the 4-dimensional parameter space, we need to construct a 4-dimensional grid. To minimize the computational cost we construct a grid that has the smallest number of points for a certain assumed minimal match MMMM [30]. This problem is equivalent to the covering problem [31, 32] and it has the optimal solution in 4-dimensions in the case of a lattice i.e., a uniformly spaced grid. In order that our parameter space is a lattice, the signals’ reduced Fisher matrix must have components that are independent of the values of the parameters. This is not the case for the signal given by Eqs. (2) - (8); it can be realized however for an approximate signal called the linear model described in Section IIIB of [27]. The linear model consists of neglecting amplitude modulation of the signal and discarding the component of the vector 𝐫d(t){\bf r}_{d}(t) joining the detector and the solar system barycenter that is perpendicular to the ecliptic. This approximation is justified because the amplitude modulation is very slow compared to the phase modulation and the discarded component in the phase is small compared to the others. As a result the linear model signal hlin(t)h_{lin}(t) has a constant amplitude A0A_{0}, and one can find parameters such that the phases are linear functions of them. We explicitly have (see Section IIIB of [27] for details):

hlin(t)=A0cos[ϕlin(t)+ϕ0],h_{lin}(t)=A_{0}\cos[\phi_{lin}(t)+\phi_{0}], (17)

where

ϕlin(t)=ω0t+ω1t2+α1μ1(t)+α2μ2(t).\phi_{lin}(t)=\omega_{0}t+\omega_{1}t^{2}+\alpha_{1}\mu_{1}(t)+\alpha_{2}\mu_{2}(t). (18)

The parameters α1\alpha_{1} and α2\alpha_{2} are defined by

α1:=ω0(sinαcosδcosε+sinδsinε),\displaystyle\alpha_{1}:=\omega_{0}(\sin\alpha\cos\delta\cos\varepsilon+\sin\delta\sin\varepsilon), (19)
α2:=ω0cosαcosδ,\displaystyle\alpha_{2}:=\omega_{0}\cos\alpha\cos\delta, (20)

where ε\varepsilon is the obliquity of the ecliptic, and μ1(t)\mu_{1}(t) and μ2(t)\mu_{2}(t) are known functions of the detector ephemeris.

In order that the grid is compatible with application of the FFT, its points should be constrained to coincide with Fourier frequencies at which the FFT is calculated. Moreover, we observed that a numerically accurate implementation of the interpolation to the barycentric time (see Eq. (14)) is so computationally demanding that it may offset the advantage of the FFT. Therefore we introduced another constraint in the grid such that the resampling is needed only once per sky position for all the spindown values. Construction of the constrained grid is described in detail in Section IV of [27]. In this search we have chosen the value of the minimal match MM=3/2MM=\sqrt{3}/2. The workflow of the coherent part of the search procedure is presented in Figure 6.

Refer to caption
Figure 6: Workflow of the \mathcal{F}-statistic search pipeline.

7 Vetoing procedure

We apply three vetoing criteria to the candidates obtained in the coherent part of the search - line width veto, stationary line veto and polar caps veto. Data from the detector always contain some periodic interferences (lines) that are detector artifacts. An important part of our vetoing procedure was to identify the lines in the data. We have therefore performed a Fourier search with frequency resolution of 1/(2 days) 5.8×106\simeq 5.8\times 10^{-6} Hz for periodic signals of each of the two-day data segments. We compared the frequencies of the significant periodic signals identified by our analysis with the line frequencies obtained by the Virgo LineMonitor and we found that all the lines from the LineMonitor were detected by our Fourier search.

7.1 Line width veto

We veto all the candidates with frequency ff around every known line frequency flf_{l} according to the following criterion

|ffl|<Δfmax,|f-f_{l}|<\Delta f_{max}, (21)

where the width Δfmax\Delta f_{max} is estimated as

Δfmax=fl|v|max/c+2|f1|max(Tobs+Tobs|v|max/c+|r|max/c),\Delta f_{max}=f_{l}|v|_{max}/c+2|f_{1}|_{max}({T_{\mathrm{obs}}}+{T_{\mathrm{obs}}}|v|_{max}/c+|r|_{max}/c), (22)

where vmaxv_{max} is the maximum value of the velocity of the detector with respect to the SSB during the observation time, rmaxr_{max} is the maximum distance to the SSB during the coherent observation time Tobs{T_{\mathrm{obs}}}, and |f1|max|f_{1}|_{max} is the maximum of the absolute value of the frequency derivative. Eq. (22) determines the maximum smearing of the frequency on each side of the line due to frequency modulation induced by the filters applied in the \mathcal{F}-statistic.

7.2 Stationary line veto

Let us consider the instantaneous frequency finstf_{\rm inst} of the signal, i.e., the time derivative of the phase:

finst:=12πdϕ(t)dt=f0+2f1t+𝐧𝐯d(t)c(f0+2f1t)+2𝐧𝐫d(t)cf1,f_{\rm inst}:=\frac{1}{2\pi}\frac{d\phi(t)}{dt}=f_{0}+2f_{1}t+\frac{{\bf n}\cdot{\bf v}_{d}(t)}{c}(f_{0}+2f_{1}t)+2\frac{{\bf n}\cdot{\bf r}_{d}(t)}{c}f_{1}, (23)

where 𝐯d(t)=d𝐫d(t)/dt{\bf v}_{d}(t)={d{\bf r}_{d}(t)}/{dt}. The frequency derivative of the instantaneous frequency is given by

dfinst(t)dt=2f1+𝐧𝐚d(t)c(f0+2f1t)+4𝐧𝐯d(t)cf1,\frac{df_{\rm inst}(t)}{dt}=2f_{1}+\frac{{\bf n}\cdot{\bf a}_{d}(t)}{c}(f_{0}+2f_{1}t)+4\frac{{\bf n}\cdot{\bf v}_{d}(t)}{c}f_{1}, (24)

where 𝐚d(t)=d𝐯d(t)/dt{\bf a}_{d}(t)={d{\bf v}_{d}(t)}/{dt}. Eq. (24) is the rate of change of detector response frequency for a source whose SSB frequency and spindown are f0f_{0} and f1f_{1}. An instrumental line has a constant detector frequency and mimics a source for which the r.h.s of Eq. (24) vanishes. In practice, we veto candidates with

|2f1+𝐧𝐚d(t)cf0+2𝐧d2(𝐫d(t)t)/dt2cf1|<ϵSL\left|2f_{1}+\frac{{\bf n}\cdot{\bf a}_{d}(t)}{c}f_{0}+2\frac{{\bf n}\cdot{d^{2}({\bf r}_{d}(t)t)}/{dt^{2}}}{c}f_{1}\right|<\epsilon_{SL} (25)

for some ϵSL>0\epsilon_{SL}>0. In the search we choose ϵSL=1/Tobs2\epsilon_{SL}=1/{T_{\mathrm{obs}}}^{2}, where Tobs{T_{\mathrm{obs}}} is the observation time. The above stationary line veto was introduced in reference [14] and refined in [33]; it was used in the first two E@H searches [20, 21].

7.3 Polar caps veto

We observe that many of the detected lines cluster around the poles where declination δ\delta is close to ±π/2\pm\pi/2. An interference originating from a detector will correlate well with our templates if the frequency modulation in Eq. (23) is minimized. Assuming that f1=0f_{1}=0 and that the diurnal motion of the Earth averages to 0 over two days observation time, this happens when the quantity |𝐧𝐯d(t)||{\bf n}\cdot{\bf v}_{d}(t)| is minimized. We find that this quantity is close to minimum independently of the value of α\alpha when δ=±π/2\delta=\pm\pi/2. Thus we veto candidates that are too close to the poles; we discard all candidates with the declination angle δ\delta within three grid cells from the poles.

8 Coincidences

In order to find coincidences among the candidates, we applied a method similar to the one used in the first two E@H searches [20, 21]. For each band we have searched for coincidences among candidates in different time frames. We are able to search for coincidences only in those bands where there were two or more time frames with data selected for the analysis. If we search for a real gravitational wave signal, we must take into account frequency evolution due to spindown of the rotating neutron star. Thus the first step in the coincidence analysis was to transform all frequencies ω0(tl)\omega_{0}(t_{l}) of the candidates to a common fiducial reference time tft_{f}. We have chosen the fiducial time to be the time of the first sample of the latest time frame that we analyzed i.e., the 67th time frame. We have

ω(tf)=ω0(tl)+2ω1(tl)[67Tobstl],\omega(t_{f})=\omega_{0}(t_{l})+2\,\omega_{1}(t_{l})[67\,{T_{\mathrm{obs}}}-t_{l}], (26)

where tlt_{l} is the time of the first sample of the llth time frame. The next step was to divide the parameter space into cells. This construction of the coincidence cell was different from that in the E@H analysis. To construct the cells in the parameter space we have used the reduced Fisher matrix Γ~\tilde{\Gamma} for the linear signal model defined by Eqs. (17) and (18). The reduced Fisher matrix is the projected Fisher matrix on the 4-dimensional space spanned by parameters κ=(ω𝟎,ω𝟏,α𝟏,α𝟐)\bf{\kappa}=(\omega_{0},\omega_{1},\alpha_{1},\alpha_{2}). We define the cell in the parameter space by the condition:

k,lΓ~klκkκl2.\sum_{k,l}\tilde{\Gamma}_{kl}\kappa_{k}\kappa_{l}\leq 2. (27)

Because the ephemeris of the detector is different in each of the time frames, the reduced Fisher matrix is different in each time frame. To have a common coincidence grid we have chosen the grid defined by the latest frame i.e., the frame no. 67 as the coincidence grid. After the transformation of the candidate frequencies to a reference time and construction of the coincidence grid, the coincidence algorithm for each of the bands proceeded in the following steps:

  1. 1.

    Transform angles α\alpha and δ\delta to α1\alpha_{1} and α2\alpha_{2} coordinates (see Eq.(19))

  2. 2.

    Transform candidate parameters to xlx_{l} coordinates defined by

    xl=k=14κkVklel,x_{l}=\sum_{k=1}^{4}\kappa_{k}V_{kl}\sqrt{e_{l}}, (28)

    where Vkl,k=1,..,4V_{kl},k=1,..,4 are eigenvectors of the matrix Γ~\tilde{\Gamma}, and ele_{l} are its eigenvalues. In these coordinates the Fisher matrix is proportional to the unit matrix.

  3. 3.

    Coordinates xlx_{l} are rounded to the nearest integer. In this way we sort candidates efficiently into adjacent 4-dimensional hypercubes. If there are more than one candidates from a given data segment in a hypercube we select the candidate that has the highest SNR. We do sorting for each time frame in the band. If there is more than one candidate in a given hypercube we register a coincidence.

  4. 4.

    We shift cubes by 1/2 of their size in all possible 242^{4} directions, and for each shift we search for coincidences.

This last step of the algorithm takes into account cases for which the candidate events are located on opposite sides of cell borders, edges, and corners and consequently coincidences that could not be found just by packing candidates into adjacent cells.

The most significant coincidence in each band is the one which has the highest multiplicity. For each most significant coincidence we have calculated the false alarm probability i.e., the probability that such a coincidence can occur purely by chance. The false alarm probability is calculated using the formula explained in A and given by Eq. (35). This general formula applies to a variable number of candidates in various time slots and also takes into account the 242^{4} shifts of the cells in the parameter space.

9 The search

In this analysis we have searched coherently 20 419 two-day time segments of data narrowbanded to 11 Hz. In the coherent part of the search described in Section 6 we have used 9.10×10169.10\times 10^{16} templates which is the number of \mathcal{F}-statistic values computed. This resulted in 20 419 candidate files containing 4.21×10104.21\times 10^{10} candidates. The candidates were subject to the vetoing using the three veto criteria: line veto, polar caps veto, and stationary line veto described in Section 7. As a result of vetoing around 24% of the candidates were discarded leaving 3.19×10103.19\times 10^{10} candidates. Nearly all candidates were vetoed by the line veto, whereas 0.20% were vetoed by the stationary line criterion and only 3.2×1023.2\times 10^{-2}% by the polar caps veto. In Figure 7 we present an example of the candidate distribution obtained from the coherent search of one narrow band data segment and after the vetoing procedure.

Refer to caption
Figure 7: Distribution of candidates after vetoing obtained in the coherent \mathcal{F}-statistic search of two-day data segment 3008930-089 i.e., a segment with the time frame number d=30d=30 and the band number b=89b=89. The left top panel shows data and its spectrum. The right top panel shows the distribution of 22\mathcal{F} values of the candidates in comparison to the χ2\chi^{2} distribution with 4 degrees of freedom. The bottom left panel shows the distribution of signal-to-noise ratios ρ\rho (see Eq. (12)) of the candidates as a function of the frequency. The vertical black line is the periodic interference identified in the data. The candidates in the band around the line are vetoed (see Eq. (22)). The right bottom panel shows the distribution of the candidates on the sky in equatorial coordinates α\alpha and δ\delta. The distribution shows singularity at the ecliptic. This is a consequence of the grid construction from the approximate linear signal model given by Eqs.(17) - (19).

In the next step we have searched for the significant coincidences among the candidates. We have searched for coincidences in all the frequency bands where there were two or more data segments analyzed. In Figure 8 we have plotted the highest coincidence multiplicity for each of the bands. The highest multiplicity was 6, and it occurred in 10 bands. The multiplicity tends to grow with the frequency, because the size of the parameter space grows as f3f^{3}.

Refer to caption
Figure 8: Coincidences among the candidates. Top panel: maximum multiplicity of coincidence as function of frequency. Bottom panel: corresponding coincidence false alarm probability.

For each band we have calculated the false alarm probability corresponding to the most significant coincidence using Eq. (35). The most significant coincidence occurred in band no. 401, corresponding to the frequency range of [488.4,489.4]\sim[488.4,489.4] Hz. It was a coincidence of multiplicity = 5, and its false alarm probability was 14.5%. Note that a coincidence with the highest multiplicity is not the most significant. This is because the significance depends on the number of time frames with candidates in a given band and also on the number of candidates in the time frames. By adopting a criterion used by E@H searches that the background coincidences correspond to false alarm probability of 0.1% or greater, we conclude that we have found no significant coincidence and thus no viable gravitational wave candidate. Considering the significance of the coincidences, we could adopt even a 10% false alarm probability as a background. Consequently, we proceed to the final stage of our analysis - estimation of sensitivity of the search.

10 Sensitivity of the search

The sensitivity of the search is taken to be the amplitude h0h_{0} of the gravitational wave signal that can be confidently detected. To estimate the sensitivity we use a procedure developed in [20]. We determine the sensitivity of the search in each of the 785 frequency bands that we have searched. To determine the sensitivity, we perform Monte Carlo simulations in which, for a given amplitude h0h_{0}, we randomly select the other seven parameters of the signal: ω0,ω1,α,δ,ϕ0,ι,\omega_{0},\omega_{1},\alpha,\delta,\phi_{0},\iota, and ψ\psi. We choose frequency and spindown parameters uniformly over their range, and source positions uniformly over the sky. We choose angles ϕ0\phi_{0} and ψ\psi uniformly over the interval [0,2π][0,2\pi] and we choose cosι\cos\iota uniformly over the interval [1,1][-1,1]. For each band we add the signal to all the data segments chosen for the analysis in that band. Then we process the data through our pipeline. First, we perform a coherent \mathcal{F}-statistic search of each of the data segments where the signal was added, and store all the candidates above our \mathcal{F}-statistic threshold of 20. In this coherent analysis, to make the computation manageable, we search over only parameter space consisting of ±\pm 2 grid points around the nearest grid point where the signal was added. Then we apply our vetoing procedure to the candidates obtained as explained in Section 7. Finally, we perform coincidence analysis of the candidates that survive vetoing which is described in Section 8. We define a detectable signal if it is coincident in more than 70% of the time frames in a given band. This condition is similar to the condition used in the two E@H searches, where a coincidence method was used [20, 21]. For bands with only one frame available the coherent search over one 22-day data segment was performed. In this case the injected signal is declared detected if its signal-to-noise ratio obtained in the coherent search is larger than the signal-to-noise ratio of the loudest signal in that data segment without an injection. For each band we inject signals with 5 different amplitude values, and perform 100 randomized injections for each amplitude. For each amplitude we calculate how many signals were detected, and by interpolation we determine the amplitude corresponding to 90% of signals detected. This amplitude was defined as the 90% confidence sensitivity. Sometimes even for the highest amplitude we have not reached the 90%90\% detection probability. In this case we performed injections for higher amplitudes until the desired level of detectability was achieved. In Figure 9, as an example, we present an estimation of the sensitivity in the band b=369b=369 corresponding to the frequency range of [457.47,458.44]\sim[457.47,458.44] Hz. The errors in the sensitivity estimates originate from calibration errors in the amplitude and errors due to a finite number of Monte Carlo injections. We use 100 injections; hence from a binomial statistic, one σ\sigma is equivalent to 3% fluctuation. Thus the estimated amplitude sensitivity corresponds to confidence in the range from 87% to 93%. To estimate how this uncertainty in confidence translates into uncertainty in the amplitude we have performed an additional set of injections for a range of amplitudes close to the estimated sensitivity and from the slope of the confidence vs. amplitude we determined the uncertainty in the amplitude. To increase the accuracy of the error estimate, we have performed 1000 injections for each amplitude. The uncertainty in the amplitude was not more than 5%. The calibration errors in VSR1 data are 6% (see Section 2). Adding these two types of errors in quadrature results in the total error in sensitivity estimate to be around 7%.

Refer to caption
Figure 9: Estimation of sensitivity in the band no. 369. In this band there are 20 time frames. Thus the signal is detected if it is coincident in more than 14 frames. The black dots are amplitudes of the injected signals and the corresponding detection probabilities estimated from the injections. The red circle is the interpolated amplitude corresponding to 90%90\% detection probability. This is the 90%90\% confidence sensitivity for this band.

The sensitivity of this search obtained through Monte Carlo simulations for the whole band searched is presented in Figure 10.

Refer to caption
Figure 10: The 90%90\% confidence sensitivity of the all-sky search of Virgo VSR1 data in the band from 100 Hz to 1 kHz. The dots show the source strain amplitude h0h_{0} for which 90%90\% of sources are confidently detected by this pipeline. The thin line is the rescaled instrumental noise curve, see Eq. (29).

We see from Figure 10 that the sensitivity essentially reflects the instrumental noise curve given in Figure 4. We have made a fit of the sensitivity h090%h^{90\%}_{0} to the one-sided spectral density Sh(f)S_{h}(f) of detector noise described by the following relation:

h090%=R𝒟Sh(f)48hours.h^{90\%}_{0}=R_{\cal D}\sqrt{\frac{S_{h}(f)}{48~\mbox{hours}}}. (29)

We find that the prefactor R𝒟R_{\cal D} is in the range from 15.6 to 22.4 and it depends on the frequency band and the number of the data segments in the band.

11 Conclusions

The sensitivity of this search was 50% to 2 times better, depending on the bandwidth, than that of the LIGO S4 search [20] and comparable to the sensitivities obtained in the early LIGO S5 data [21], but 22 to 55 times worse than the upper limits in the E@H full LIGO S5 data search [22]. This was due to the lower noise and longer observation time for the LIGO S5 data w.r.t the Virgo VSR1 data. However, for the first time in an all-sky search we have estimated the sensitivity in the frequency band from 400Hz to 1kHz and the frequency spindown range from 7.2(f0/400Hz)×109-7.2\,(f_{0}/400\,{\rm Hz})\times 10^{-9}\, Hz/s to 6.0×109-6.0\times 10^{-9}\, Hz/s, which is a previously unexplored region in the parameter space.

The next step is to test the search method described in this paper in the Mock Data Challenge (MDC) designed by the LIGO and Virgo projects to validate and compare pipelines that are proposed to be used in the analysis of the forthcoming data from the advanced detectors. It is also planned to further test the pipeline presented here with other data sets collected by the LIGO and Virgo detectors.

The authors gratefully acknowledge the support of the United States National Science Foundation for the construction and operation of the LIGO Laboratory, the Science and Technology Facilities Council of the United Kingdom, the Max-Planck-Society, and the State of Niedersachsen/Germany for support of the construction and operation of the GEO600 detector, and the Italian Istituto Nazionale di Fisica Nucleare and the French Centre National de la Recherche Scientifique for the construction and operation of the Virgo detector. The authors also gratefully acknowledge the support of the research by these agencies and by the Australian Research Council, the International Science Linkages program of the Commonwealth of Australia, the Council of Scientific and Industrial Research of India, the Istituto Nazionale di Fisica Nucleare of Italy, the Spanish Ministerio de Economía y Competitividad, the Conselleria d’Economia Hisenda i Innovació of the Govern de les Illes Balears, the Foundation for Fundamental Research on Matter supported by the Netherlands Organisation for Scientific Research, the Polish Ministry of Science and Higher Education, the FOCUS Programme of Foundation for Polish Science, the PL-Grid Infrastructure, the Royal Society, the Scottish Funding Council, the Scottish Universities Physics Alliance, The National Aeronautics and Space Administration, the Carnegie Trust, the Leverhulme Trust, the David and Lucile Packard Foundation, the Research Corporation, and the Alfred P. Sloan Foundation. This document has been assigned LIGO Laboratory document number LIGO-P1300133.

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Appendix A False alarm coincidence probability

Let us assume that for a given frequency band we analyze LL non-overlapping time segments. Suppose that the search of the llth segment produces NlN_{l} candidates. Let us assume that the size of the parameter space for each time segment is the same, and it can be divided into the number NcellN_{\rm cell} of independent cells. We would like to test the null hypothesis that coincidences among candidates from LL segments are accidental. The probability for a candidate event to fall into any given coincidence cell is equal to 1/Ncell1/N_{\rm cell}. Thus probability ϵl\epsilon_{l} that a given coincidence cell is populated with one or more candidate events is given by

ϵl=1(11Ncell)Nl.\epsilon_{l}=1-\Big{(}1-\frac{1}{N_{\rm cell}}\Big{)}^{N_{l}}. (30)

We may also consider independent candidates only, i.e., such that there is no more than one candidate within one cell. If we obtain more than one candidate within a given cell we choose the one which has the highest signal-to-noise ratio. In this case

ϵl=NlNcell.\epsilon_{l}=\frac{N_{l}}{N_{\rm cell}}. (31)

The probability pF(Ncell)p_{F}(N_{\rm cell}) that any given coincidence cell out of the total of NcellN_{\rm cell} cells contains candidate events from CmaxC_{max} or more distinct data segments is given by a generalized binomial distribution

pF(Ncell)\displaystyle p_{F}(N_{\rm cell}) =\displaystyle= n=CmaxL1n!(Ln)!×\displaystyle\sum_{n=C_{max}}^{L}\frac{1}{n!(L-n)!}\times (32)
×\displaystyle\times σΠ(L)ϵσ(1)ϵσ(n)(1ϵσ(n+1))(1ϵσ(L)),\displaystyle\sum_{\sigma\in\Pi(L)}\epsilon_{\sigma(1)}\ldots\epsilon_{\sigma(n)}(1-\epsilon_{\sigma(n+1)})\ldots(1-\epsilon_{\sigma(L)}),

where σΠ(L)\sum_{\sigma\in\Pi(L)} is the sum over all the permutations of the LL data sequences. Finally the probability PFP_{F} that there is 𝒞max{\mathcal{C}}_{max} or more coincidences in one or more of the NcellN_{\rm cell} cells is

PF=1(1pF(Ncell))Ncell.P_{F}=1-(1-p_{F}(N_{\rm cell}))^{N_{\rm cell}}. (33)

The above formula for the false alarm coincidence probability does not take into account the case when candidate events are located on opposite sides of cell borders, edges, and corners. In order to find these coincidences the entire cell coincidence grid is shifted by half a cell width in all possible 24=162^{4}=16 combinations of the four parameter-space dimensions, and coincidences are searched in all the 16 coincidence grids. This leads to a higher number of accidental coincidences, and consequently Eq. 33 underestimates the false alarm probability. Let us consider the simplest one-dimensional case. In this case we have 21=22^{1}=2 possible shifts (the original coincidence grid and the one shifted by half). This increases probability pF(Ncell)p_{F}(N_{\rm cell}) by a factor of 22 if the two cell coincidence grids were independent. However the cells overlap by half and some coincidences would be counted twice. To account for this we divide the cells in the coincidence grid by half resulting in 2Ncell2N_{\rm cell} cells and define the false alarm probability pF(2Ncell)p_{F}(2N_{\rm cell}) that any given half of the coincidence cell out of the total of 2Ncell2N_{\rm cell} half cells contains candidate events from CmaxC_{max} or more distinct data segments. These are coincidences that were already counted, and consequently the false alarm probability with the cell shift is 2pF(Ncell)pF(2Ncell)2p_{F}(N_{\rm cell})-p_{F}(2N_{\rm cell}). This results in the false alarm probability

PF=1(1(2pF(Ncell)pF(2Ncell)))Ncell.P_{F}=1-(1-(2p_{F}(N_{\rm cell})-p_{F}(2N_{\rm cell})))^{N_{\rm cell}}. (34)

To generalize the above formula to higher dimensions we need to consider further shifts and divisions of the cells. In the four dimension case this leads to the formula for the probability PFshiftsP^{\rm shifts}_{F} that there are 𝒞max{\mathcal{C}}_{\mathrm{max}} or more independent coincidences in one or more of the NcellN_{\rm cell} cells in all 16 grid shifts given by

PFshifts=1[1(24pF(Nc)\displaystyle P^{\rm shifts}_{F}=1-\Big{[}1-\Big{(}2^{4}p_{F}(N_{c}) (35)
((41)pF(2Nc)+(42)pF(22Nc)+(43)pF(23Nc)+(44)pF(24Nc))\displaystyle-\big{(}{4\choose 1}p_{F}(2N_{c})+{4\choose 2}p_{F}(2^{2}N_{c})+{4\choose 3}p_{F}(2^{3}N_{c})+{4\choose 4}p_{F}(2^{4}N_{c})\big{)}
((42)pF(22Nc)+(43)pF(23Nc)+(44)pF(24Nc))\displaystyle-\big{(}{4\choose 2}p_{F}(2^{2}N_{c})+{4\choose 3}p_{F}(2^{3}N_{c})+{4\choose 4}p_{F}(2^{4}N_{c})\big{)}
((43)pF(23Nc)+(44)pF(24Nc))\displaystyle-\big{(}{4\choose 3}p_{F}(2^{3}N_{c})+{4\choose 4}p_{F}(2^{4}N_{c})\big{)}
(44)pF(24Nc))]Nc\displaystyle-{4\choose 4}p_{F}(2^{4}N_{c})\Big{)}\Big{]}^{N_{c}}

By choosing a certain false alarm probability PFP_{F}, we can calculate the threshold number 𝒞max{\mathcal{C}}_{\mathrm{max}} of coincidences. If we obtain more than 𝒞max{\mathcal{C}}_{\mathrm{max}} coincidences in our search we reject the null hypothesis that coincidences are accidental only at the significance level of PFP_{F}.