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These endeavors have been both productive and fun, in large part due to my longtime collaborator in much of this work, Paul Roche. Since then, my 5.2 years at Caltech have been made much easier by the wonderful friends I have met here.

List of Figures

List of Tables

Note on Terms, Units, and Names

Chapter 1

Accretion-Powered Pulsars and BATSE

Overview and Project History

  • Accretion-Powered Pulsars and the Role of BATSE
  • Thesis Organization

The good (1.024 s) time resolution enables coverage of most of the pulsation phase space (P > 2 s) of known accretion pulsars. Interestingly, the spin-up and spin-down magnitudes differ by only 15%, with the neutron star spin varying on a time scale of Iv /vi ~ 5000 years in both states.

Background on Accretion-Powered Pulsars

  • Early History 1
  • Observed Characteristics

The emission mechanism in these spin-powered isolated pulsars is completely different from that of accretion-powered binary pulsars. A rough correlation between orbital period and rotation period has been observed in Be-star/X-ray binary pulsars ( Corbet 1986 ; Waters & van Kerkwijk 1989 ).

Figure 1.1:  Distribution of accretion-powered binary pulsars in Galactic coordinates
Figure 1.1: Distribution of accretion-powered binary pulsars in Galactic coordinates

Chapter 2

Acquisition and Reduction of BATSE Data

The Compton Gamma Ray Observatory

Modules 0, 2, 4 and 6 are visible in this diagram. al. 1993) provides imaging observations in the 1–30 MeV range using a combined liquid/Na scintillator. The Energetic Gamma-ray Experiment Telescope (EGRET; Thompson et al. 1993) provides imaging in the 20 MeV–30 GeV range using a spark chamber detector.

The Burst and Transient Source Experiment

We also use the QUAL information to exclude intervals containing gamma-ray bursts from pulsar timing analysis. A variety of special data products are activated with high time and energy resolution when triggered by on-board identification of a gamma-ray burst in the BATSE LAD data stream.

Figure 2.2:  A BATSE  detector  module.  The  investigations  in  this  thesis  all  employ  data  from the large area detectors
Figure 2.2: A BATSE detector module. The investigations in this thesis all employ data from the large area detectors

Detector Response

The response does not drop to zero at 90° incidence due to the finite thickness of the crystal. The secondary maximum in the large-angle response for low energies is due to the geometry of the support structure at the edge of the LADs.

Figure  2.3:  Effective  area of a  BATSE  large area detector at normal incidence.  The solid  curve denotes the total response of the detector, including interactions where the incident  photon energy is  only  partially deposited
Figure 2.3: Effective area of a BATSE large area detector at normal incidence. The solid curve denotes the total response of the detector, including interactions where the incident photon energy is only partially deposited

Optimal Combination of Detectors

The best overall sensitivity is obtained by adaptively choosing the detector weight based on the altazimuth position of the source. Celestial coordinates are shown in the altazimuth system with respect to the spacecraft axes. e) singles+poirs (f) singles+poirs+quods.

Figure  2.6:  Optimal  detector  weighting  for  known  sky  positions.  Sky  coordinates  are  shown  in  the altazimuth system with  respect  to the spacecraft axes
Figure 2.6: Optimal detector weighting for known sky positions. Sky coordinates are shown in the altazimuth system with respect to the spacecraft axes

Earth Occultation

A source is obscured when the line-of-sight shock parameter relative to Earth is less than RtJJ + h. Given a position vector r = (x, y, z), the equatorial radius of the equipotential passing through that position is given by z.

Figure 2.9:  Earth occultation of Cygnus X-1,  as observed in the 20-60 keV  channel of the  BATSE large area detector facing  the source
Figure 2.9: Earth occultation of Cygnus X-1, as observed in the 20-60 keV channel of the BATSE large area detector facing the source

Detector Background

It is instructive to consider the background power spectral properties of the BATSE in the frequency domain. The bottom curve is for the raw data after subtraction by Rubin et al.

Figure  2.10:  Typical  count  spectrum  of  the  background  as  a  function  of  energy  for  a  BATSE LAD
Figure 2.10: Typical count spectrum of the background as a function of energy for a BATSE LAD

2. 7 Sensitivity to Pulsed Signals

  • General Principles
  • BATSE Sensitivity as a Function of Energy
  • Time Systems and Reference Frames
  • Standard Analysis Procedure
  • Chapter 3

The second panel shows the time series after subtraction of the ad hoc background model. The detector response matrices of the Burst and Transient Source Experiment (BATSE) at the Compton Gamma Ray Observatory.

Figure 2.14:  Typical BATSE pulsar detection sensitivity as  a function  of energy, for  1 day  of data
Figure 2.14: Typical BATSE pulsar detection sensitivity as a function of energy, for 1 day of data

Detection and Estimation of Periodic Pulsed Signals

  • Introduction
  • Detection of Periodic Pulsed Signals
    • Time Domain: Epoch Folding
    • Frequency Domain: Fourier Analysis
    • Aliasing and Pulsed Sensitivity in Binned Data
  • Estimation of Pulse Strength in Periodic Signals
  • roo 2 n2 exp(~) (-a2)
    • Flux and Spectral Estimation
  • Chapter 4

Due to the finite length of the time series T, the power spectral response in the kth Fourier frequency bin (where Vk = k/T) to a periodic signal with frequency vo is given by. This function is plotted in the top panel of Figure 3.3 for various values ​​of the true. For small values ​​of the measured amplitude (a/n;::; 2), the distribution is highly skewed towards zero signal.

Figure  3.1:  Power  spectral  response  of  a  frequency  bin  as  a  function  of frequency  offset  from  the bin  center
Figure 3.1: Power spectral response of a frequency bin as a function of frequency offset from the bin center

Discovery of the Orbit of the Accreting X-Ray Pulsar OAO 1657-415*

  • Introduction
  • Observations and Timing Analysis
  • Results
  • OAO 1 65 7 - 4 1 5 100
    • Discussion
  • Chapter 5

More recent observations have shown up-and-down rotation during the pulse period (Kamata et al. We have measured the eccentric binary orbit and eclipse duration of the accretion-driven X-ray pulsar OAO 1657-415. SIGMA observation of the pulsar OAO 1657-415: precise localization at hard X-ray energies rays and the discovery of spin down.

Figure  4.1:  Doppler  delays  for  the  pulse  arrival  times  as  a  function  of the  10.4436  day  orbit of OAO  1657-415 after  removing  our best  model  for  the  intrinsic variations  in  spin  period
Figure 4.1: Doppler delays for the pulse arrival times as a function of the 10.4436 day orbit of OAO 1657-415 after removing our best model for the intrinsic variations in spin period

Discovery of the 18.7-Second Accreting X-Ray Pulsar GRO J1948+32*

  • Introduction
  • Observations and Analysis
  • Discussion
  • Chapter 6

GRO J1948+32 was initially detected in a routine search for the Fourier power spectra of this data for 1994 April 7. correspond to the eruption. The vertical bars show the 1 a statistical uncertainties, while the horizontal bars show the widths of the energy channels.

Figure 5.1:  Pulse-phase-averaged 20-75  keV  pulsed flux  history  of GRO  J1948+32.  The  vertical bars show the  1 ()  uncertainties in  the flux  measurements
Figure 5.1: Pulse-phase-averaged 20-75 keV pulsed flux history of GRO J1948+32. The vertical bars show the 1 () uncertainties in the flux measurements
  • Introduction
  • Observations and Analysis
    • Pulse Timing
    • Phase Residual Analysis
    • Pulse Spectroscopy
  • Discussion
  • Chapter 7

The resulting power spectral density of the pulse frequency fluctuation Pq is shown in the left panel of Figure 6.3. It is therefore puzzling that the magnitudes of up-spin and down-spin in 4U 1626-67 are almost the same. These contrasts may simply reflect differences in the stability of accretion flows in these systems.

Figure 6.1:  Pulse frequency  history of 4U  1626-67, reduced  to the solar system barycen- barycen-ter
Figure 6.1: Pulse frequency history of 4U 1626-67, reduced to the solar system barycen- barycen-ter

Introduction

In the centrifugally driven wind (CDW) model of Arons et al. 1984), the magnetic field does not cross the disc but penetrates a narrow boundary layer. As an alternative, Makishima et al. suggested that the spin-down may be due to accretion from the dense, slow wind of the M giant after disruption of a previous accreting disc during spin-up. Some authors have claimed that this X-ray burst was accompanied by increased Ha emission (Manchanda et al. 1995;

7 .2 Observations and Analysis

Timing

34"red noise" component (a power spectral component that increases with decreasing frequency) in the pulse frequency fluctuations. Before calculating the power spectrum, we multiplied the pulse frequency residuals by a window function of the form Wj = cos4(j7r/N) with j = -N/2, · · ·, N/2, substantially suppressing the side response of the Fourier transform (Harris 1978) The resulting power spectral density of the pulse frequency fluctuations Pv is shown in the left panel of figure 7.5.

Figure 7.1:  Pulse frequency  history of GX  1+4 at the solar system barycenter.  Top  panel:
Figure 7.1: Pulse frequency history of GX 1+4 at the solar system barycenter. Top panel:

Pulse Profiles and Spectroscopy

A simultaneous measurement of the total (pulsed+non-pulsed) spectrum of GX 1+4 in the range 40-200 keV was performed with Compton/OSSE (Staubert et al. 1995). Furthermore, a head-to-head comparison of BATSE and OSSE observations of the Crab Nebula has shown that the BATSE fluxes are systematically::::::20% higher than the OSSE fluxes (Much et al. 1996). The dotted curve shows the best-fitting model for simultaneous OSSE observations of the total (pulsed+non-pulsed) flux, with corrections applied (see text for details).

Figure  7.6:  Left panel:  The phase-averaged pulsed  count spectrum of GX  1+4 during the  bright  spin-up  state
Figure 7.6: Left panel: The phase-averaged pulsed count spectrum of GX 1+4 during the bright spin-up state

Flux and Torque

The resulting history of the derivative of the pulse frequency (i.e. the spin-up rate), which is proportional to the net torque applied to the neutron star if we can neglect the orbital Doppler shifts, is shown in the middle panel of Figure 7.9. Clearly, most of the bright flares were accompanied by enhanced spin-down. We can formalize the correlation between torque and brightness by calculating the cross-correlation of the two time series.

Figure 7.9:  Top  panel:  BATSE 20-60 keV  pulsed flux  history for  GX  1+4, averaged at  5- 5-day intervals
Figure 7.9: Top panel: BATSE 20-60 keV pulsed flux history for GX 1+4, averaged at 5- 5-day intervals

7 .3 Discussion

Accretion

Both the MTD and CDW accretion models predict that a sufficiently increased mass transfer rate can cause a transition from spin-down to spin-up, consistent with our observations of the persistent bright state around MJD 49600. For consistency with the other data, we expect at least an initial improvement in spin-down torque. We can put a lower limit on the distance and X-ray luminosity from the steady spin-up of the source during the 1970s (see Appendix C).

Figure 7.10:  Top  panel:  Cross-correlation of  fl  and pulsed flux during spin-down
Figure 7.10: Top panel: Cross-correlation of fl and pulsed flux during spin-down

Appendix A

Spacecraft Coordinates and Sky Coordinates

The vectors for the BATSE detector normals in spacecraft coordinates are given in Table A.l. The celestial coordinates for the spacecraft axes for each of the Compton Observatory paintings are given in Table A.2. Coordinates for more recent references are available from the Compton Observatory Science Support Center via WWW (http://cossc.gsfc.nasa.gov/cossc/cossc.html).

Figure  A.l:  Spacecraft  axes  for  the  Compton  Gamma  Ray  Observatory.  The  8  BATSE  detector modules  are situated on the corners of the spacecraft
Figure A.l: Spacecraft axes for the Compton Gamma Ray Observatory. The 8 BATSE detector modules are situated on the corners of the spacecraft's main body

Appendix B

Decoherence Time Scales in Pulse Timing

Decoherence Due to Accretion Torque

For longer observations, phase coherence can be recovered by "accelerating" the time series to compensate for phase drift, essentially stretching or squeezing the size of the time bins (Middleditch 1989; Anderson et al. 1990; Wood et al. 1991; Johnston & Kulkarni 1991) .

Decoherence Due to Orbital Motion

Appendix C

Limits on Luminosity and Distance from Steady Spin-Up

Appendix D

Binary Orbits

Basic Concepts

The orientation of the line of apsides with respect to the line of sight is specified by the longitude of periastron w. By using the Doppler shifts of a binary pulsar to measure an orbit, we are only sensitive to motion projected along the line of sight. If sin i is sufficiently close to 1 to allow an eclipse of M2 at M1, then L = goo will roughly correspond to the center of the eclipse (see Deeter et al. 1g31 for some subtleties related to this point) .

Figure  D.1:  Binary geometry  for  two  masses  (M 1  >  M 2 )  orbiting  their  common  center- center-of-mass  F
Figure D.1: Binary geometry for two masses (M 1 > M 2 ) orbiting their common center- center-of-mass F

Orbit-Fitting Equations

  • Auxiliary Chain Rule Quantities
  • Pulse Frequency Measurements
  • Pulse Arrival Time Measurements

If one uses the alternative parameterization for low-eccentricity orbits, the partial derivatives with respect to T0 are replaced by those with respect to Trr ; 2,. A slightly different set of derivatives will be needed if the circuit is parameterized in terms of T1f;2 instead of To. A slightly different set of derivatives will be needed if the circuit is parameterized in terms of T1r ;2 instead of To.

Appendix E

Eclipse Constraints in OAO 1657-415

The coordinate system rotates about the z-axis in the ¢, one revolution per orbital period, so that the companion always lies on the x-axis with the neutron star at the origin. The line of sight from the neutron star to the observer will intersect the companion surface on the shown closed curve. However, because for an eccentric orbit the coordinate system no longer rotates at a uniform speed, we no longer have Oe =¢max· To relate the observed quantity Oe to equation (E.7), we can again exploit the location of periastron. halfway through the eclipse (¢ = 0).

Figure  E.1:  Eclipse  angle  geometry.  The  coordinate  system  rotates  about  the  z-axis  in  the  ¢,  with  one  revolution  per  orbital  period,  so  that  the  companion  always  lies  on  the  x-axis  with  the  neutron  star  at  the origin
Figure E.1: Eclipse angle geometry. The coordinate system rotates about the z-axis in the ¢, with one revolution per orbital period, so that the companion always lies on the x-axis with the neutron star at the origin

Appendix F

Limits on the Orbit of GRO J1948+32

By doing this for a grid of fixed parameter values, we can calculate the allowed region of parameter space corresponding to a given confidence level by excluding parameter values ​​for which x2 is also . Model with reduced x2 above this value is inconsistent with the data at the 953 confidence level. The corresponding results for eccentric orbit models are summarized in Table F.2 and shown in Figure F.3.

Figure  F.l:  Pulse  frequency  history  of  GRO  J1948+32  from  BATSE  observations
Figure F.l: Pulse frequency history of GRO J1948+32 from BATSE observations

Appendix G

BATSE Localization of Faint Pulsed Sources*

Since Wis is dominated by harmonics of the spacecraft's orbital frequency VGRO « 2vo (where 1/vGRO ~ 93 min), we can generally assume IW2kl. The factor of E in the denominator of this definition appears because a fraction 1 - E of the time series { Q j} is set to zero.). Given the strength of the signal in these data, we will adopt 0.5° as the systematic precision limit of this technique with DISCLA data.

Appendix H

Introduction

Observations

The fundamental and second harmonics of the optical pulses, seen near 0.13 Hz and 0.26 Hz, are in good agreement with the BATSE pulse frequency ephemeris. Absolute time accuracy within ± 1.5 ms UTC-NIST was maintained using a Kinemetriks/Truetime model 468-DC satellite-synchronized clock in conjunction with the GOES-West satellite operated by the National Oceanographic and Atmospheric Administration.

Results

When corrected to the barycenter of the solar system, this agrees well with the BATSE epmeheris for X-ray pulsations (see Chapter 6). In addition to the main pulsation, a significant lower frequency sidelobe is also present at the mHz topocentric frequency. The mHz main peak to sidelobe spacing is almost identical to the sidelobe spacing reported by Middleditch et al.

Figure  H.2:  Optical  power  spectrum  of 4U  1626-67  in  the  vicinity  of  the  fundamental,  normalized with  respect  to  the local  noise  power
Figure H.2: Optical power spectrum of 4U 1626-67 in the vicinity of the fundamental, normalized with respect to the local noise power

Appendix I

IAU Circulars

Position of GRO J1948+32

Appendix J

Photon spectrum and period evolution of GX 1+4 as observed at hard X-ray energies by SIGMA. Timing of X-ray pulsars from data obtained with the ART-P telescope of the Granat Space Observatory in 1990-1992.

Table  J.l.  Archival Timing Observations of GX  1+4
Table J.l. Archival Timing Observations of GX 1+4

Colophon

Gambar

Figure 1.2:  Spin  period versus  orbital period for  the accreting pulsars  with  massive  com- com-panions
Figure 2.2:  A BATSE  detector  module.  The  investigations  in  this  thesis  all  employ  data  from the large area detectors
Table 2.1.  Energy  Channels in BATSE DISCLA  and CONT  Data  Energy  Range  Background Rate
Figure 2.4:  Angular response of a BATSE large area detector to photons of various energies
+7

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