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Dive into the research topics where D. I. Robertson is active.

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Featured researches published by D. I. Robertson.


Classical and Quantum Gravity | 2002

The GEO 600 gravitational wave detector

B. Willke; P. Aufmuth; Carsten Aulbert; S. Babak; R. Balasubramanian; B. Barr; Steven J. Berukoff; S. Bose; G. Cagnoli; M. M. Casey; D. Churches; D. Clubley; Carlo Nicola Colacino; D. R. M. Crooks; Curt Cutler; Karsten Danzmann; R. Davis; E. J. Elliffe; Carsten Fallnich; Andreas Freise; S. Gossler; A. Grant; H. Grote; Gerhard Heinzel; A. Heptonstall; M. Heurs; J. Hough; Keita Kawabe; Karsten Kötter; V. Leonhardt

The GEO 600 laser interferometer with 600 m armlength is part of a worldwide network of gravitational wave detectors. Due to the use of advanced technologies like multiple pendulum suspensions with a monolithic last stage and signal recycling, the anticipated sensitivity of GEO 600 is close to the initial sensitivity of detectors with several kilometres armlength. This paper describes the subsystems of GEO 600, the status of the detector by September 2001 and the plans towards the first science run.


Applied Optics | 1994

Automatic alignment of optical interferometers

Euan Morrison; Brian J. Meers; D. I. Robertson; H. Ward

We present a description of a system for automatic alignment of optical interferometers. The technique relies on using differential phase modulation to permit the detection of the phase difference between two fundamental-mode Gaussian beams at the output of an interferometer. Measurements of the spatially varying phase difference between the two beams by use of one or more multielement photodiodes permits information to be derived about the mismatch in overlap between the phase fronts at the output of the interferometer.


Classical and Quantum Gravity | 2005

Hydroxide-catalysis bonding for stable optical systems for space

E. J. Elliffe; J. Bogenstahl; A. Deshpande; J. Hough; Christian J. Killow; S. Reid; D. I. Robertson; S. Rowan; H. Ward; G. Cagnoli

Space-based optical systems must be made from lightweight materials which can withstand significant acceleration and temperature changes. Materials such as ZERODUR®, ULE® (Ultra Low Expansion material) and silica are all potentially suitable. Depending on the specific requirements of the optical system and the transmissive or reflective nature of the optical layout these materials can be used by themselves or together to fabricate optical benches. The geometrical layouts of these optical systems are often very complicated and the requirements for mechanical stability very stringent, thus jointing components presents a challenge. In this paper we present developments of a novel chemical bonding process, originally invented at Stanford University for bonding silica components for the optical telescope for the Gravity Probe B mission. Colloquially called silicate bonding, this process utilizes hydroxide catalysis to join optical components to optical mounts to obtain high stability whilst accommodating the requirement for precise alignment procedures.


Applied Optics | 1994

Experimental demonstration of an automatic alignment system for optical interferometers

Euan Morrison; Brian J. Meers; D. I. Robertson; H. Ward

An automatic alignment system, based on a differential phase-sensing technique described in a companion paper [Appl. Opt.33, 0000, (1994)], has been experimentally demonstrated on the 10-m prototype laser interferometric gravitational wave detector in Glasgow. The alignment system developed was used to control the orientations of two mirrors in a 10-m-long suspended Fabry-Perot cavity with respect to the direction defined by the input laser beam. The results of the test and a discussion of the performance of the system are given.


Classical and Quantum Gravity | 2004

The LTP interferometer and phasemeter

Gerhard Heinzel; V. Wand; Antonio Garcia; Oliver Jennrich; Claus Braxmaier; D. I. Robertson; Kevin Middleton; D. Hoyland; Albrecht Rüdiger; R. Schilling; Ulrich Johann; Karsten Danzmann

The LISA Technology Package (LTP), to be launched by ESA in 2006/2007, is a technology demonstration mission in preparation for the LISA space-borne gravitational wave detector. A central part of the LTP is the optical metrology package (heterodyne interferometer with phasemeter) which monitors the distance between two test masses with a noise level of 10 pm Hz−1/2 between 3 mHz and 30 mHz. It has a dynamic range of >100 µm without any actuators for the pathlength. In addition to the longitudinal measurements, it provides alignment measurements with an expected noise level of <10 nrad Hz−1/2. While the basic design has been described previously by Heinzel et al (2003 Class. Quantum Grav. 20 S153–61), this paper gives new details on the laser stabilization, the phasemeter and recent prototype results.


Classical and Quantum Gravity | 2005

The LTP experiment on the LISA Pathfinder mission

S. Anza; M Armano; E. Balaguer; M. Benedetti; C. Boatella; P. Bosetti; D. Bortoluzzi; N. Brandt; Claus Braxmaier; Martin E. Caldwell; L. Carbone; A. Cavalleri; A. Ciccolella; I. Cristofolini; M. Cruise; M. Da Lio; Karsten Danzmann; D. Desiderio; R. Dolesi; N. Dunbar; Walter Fichter; C. Garcia; E. Garcia-Berro; A. F. Garcia Marin; R. Gerndt; Alberto Gianolio; Domenico Giardini; R. Gruenagel; A. Hammesfahr; Gerhard Heinzel

We report on the development of the LISA Technology Package (LTP) experiment that will fly onboard the LISA Pathfinder mission of the European Space Agency in 2008. We first summarize the science rationale of the experiment aimed at showing the operational feasibility of the so-called transverse–traceless coordinate frame within the accuracy needed for LISA. We then show briefly the basic features of the instrument and we finally discuss its projected sensitivity and the extrapolation of its results to LISA.


Classical and Quantum Gravity | 2006

Status of the GEO600 detector

H. Lück; M. Hewitson; P. Ajith; B. Allen; P. Aufmuth; C. Aulbert; S. Babak; R. Balasubramanian; B. Barr; Steven J. Berukoff; Alexander Bunkowski; G. Cagnoli; C. A. Cantley; M. M. Casey; S. Chelkowski; Y. Chen; D. Churches; T. Cokelaer; C. N. Colacino; D. R. M. Crooks; Curt Cutler; Karsten Danzmann; R. J. Dupuis; E. J. Elliffe; Carsten Fallnich; A. Franzen; A. Freise; I. Gholami; S. Goßler; A. Grant

Of all the large interferometric gravitational-wave detectors, the German/British project GEO600 is the only one which uses dual recycling. During the four weeks of the international S4 data-taking run it reached an instrumental duty cycle of 97% with a peak sensitivity of 7 × 10−22 Hz−1/2 at 1 kHz. This paper describes the status during S4 and improvements thereafter.


Classical and Quantum Gravity | 2009

LISA Pathfinder: the experiment and the route to LISA

M. Armano; M. Benedetti; J. Bogenstahl; D. Bortoluzzi; P. Bosetti; N. Brandt; A. Cavalleri; G. Ciani; I. Cristofolini; A. M. Cruise; Karsten Danzmann; I. Diepholz; G. Dixon; R. Dolesi; J. Fauste; L. Ferraioli; D. Fertin; Walter Fichter; M. Freschi; Antonio Garcia; C. Garcia; A. Grynagier; F. Guzman; E. Fitzsimons; Gerhard Heinzel; M. Hewitson; D. Hollington; J. Hough; M. Hueller; D. Hoyland

LISA Pathfinder (LPF) is a science and technology demonstrator planned by the European Space Agency in view of the LISA mission. As a scientific payload, the LISA Technology Package on board LPF will be the most precise geodesics explorer flown as of today, both in terms of displacement and acceleration sensitivity. The challenges embodied by LPF make it a unique mission, paving the way towards the space-borne detection of gravitational waves with LISA. This paper summarizes the basics of LPF, and the progress made in preparing its effective implementation in flight. We hereby give an overview of the experiment philosophy and assumptions to carry on the measurement. We report on the mission plan and hardware design advances and on the progress on detailing measurements and operations. Some light will be shed on the related data processing algorithms. In particular, we show how to single out the acceleration noise from the spacecraft motion perturbations, how to account for dynamical deformation parameters distorting the measurement reference and how to decouple the actuation noise via parabolic free flight.


Proceedings of SPIE | 2004

The status of GEO 600

K. A. Strain; B. Allen; P. Aufmuth; Carsten Aulbert; S. Babak; R. Balasubramanian; B. Barr; Steven J. Berukoff; Alexander Bunkowski; G. Cagnoli; C. A. Cantley; M. M. Casey; S. Chelkowski; D. Churches; T. Cokelaer; Carlo Nicola Colacino; D. R. M. Crooks; Curt Cutler; Karsten Danzmann; R. Davies; R. J. Dupuis; E. J. Elliffe; Carsten Fallnich; A. Franzen; Andreas Freise; S. Goßler; A. Grant; H. Grote; S. Grunewald; J. Harms

The GEO 600 laser interferometer with 600m armlength is part of a worldwide network of gravitational wave detectors. GEO 600 is unique in having advanced multiple pendulum suspensions with a monolithic last stage and in employing a signal recycled optical design. This paper describes the recent commissioning of the interferometer and its operation in signal recycled mode.


Nuclear Physics | 2002

LISA and its in-flight test precursor SMART-2

S. Vitale; P. L. Bender; A. Brillet; Saps Buchman; A. Cavalleri; Massimo Cerdonio; M. Cruise; Curt Cutler; Karsten Danzmann; R. Dolesi; William M. Folkner; Alberto Gianolio; Y Jafry; G. Hasinger; Gerhard Heinzel; Craig J. Hogan; M. Hueller; J. Hough; S. Phinney; T. Prince; D. Richstone; D. I. Robertson; M. Rodrigues; Albrecht Rüdiger; M. Sandford; R. Schilling; D. H. Shoemaker; Bernard F. Schutz; Robin T. Stebbins; Christopher W. Stubbs

LISA will be the first space-home gravitational wave observatory. It aims to detect gravitational waves in the 0.1 MHz+1 Hz range from sources including galactic binaries, super-massive black-hole binaries, capture of objects by super-massive black-holes and stochastic background. LISA is an ESA approved Cornerstone Mission foreseen as a joint ESA-NASA endeavour to be launched in 2010-11. The principle of operation of LISA is based on laser ranging of test-masses under pure geodesic motion. Achieving pure geodesic motion at the level requested for LISA, 3×10^(−15) ms^(−2)/√Hz at 0.1 mHz, is considered a challenging technological objective. To reduce the risk, both ESA and NASA are pursuing an in-flight test of the relevant technology. The goal of the test is to demonstrate geodetic motion within one order of magnitude from the LISA performance. ESA has given this test as the primary goal of its technology dedicated mission SMART-2 with a launch in 2006. This paper describes the basics of LISA, its key technologies, and its in-flight precursor test on SMART-2.

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H. Ward

University of Glasgow

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J. Hough

University of Glasgow

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E. Fitzsimons

Airbus Defence and Space

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