A Sub-Hertz, Low-Frequency Vibration Isolation Platform

One of the major technical problems deep-space optical communication (DSOC) systems need to solve is the isolation of the optical terminal from vibrations produced by the spacecraft navigational control system and by the moving parts of onboard instruments. Even under these vibration perturbations, the DSOC transceivers (telescopes) need to be pointed l000 fs of times more accurately than an RF communication system (parabolic antennas). Mechanical resonators have been extensively used to provide vibration isolation for groundbased, airborne, and spaceborne payloads. The effectiveness of these isolation systems is determined mainly by the ability of designing a mechanical oscillator with the lowest possible resonant frequency. The Low-Frequency Vibration Isolation Platform (LFVIP), developed during this effort, aims to reduce the resonant frequency of the mechanical oscillators into the sub-Hertz region in order to maximize the passive isolation afforded by the 40 dB/decade roll-off response of the resonator. The LFVIP also provides tip/tilt functionality for acquisition and tracking of a beacon signal. An active control system is used for platform positioning and for dampening of the mechanical oscillator. The basic idea in the design of the isolation platform is to use a passive isolation strut with an approximately equal to 100-mHz resonance frequency. This will extend the isolation range to lower frequencies. The harmonic oscillator is a second-order lowpass filter for mechanical disturbances. The resonance quality depends on the dissipation mechanisms, which are mainly hysteretic because of the low resonant frequency and the absence of any viscous medium. The LFVIP system is configured using the well-established Stewart Platform, which consists of a top platform connected to a base with six extensible struts (see figure). The struts are attached to the base and to the platform via universal joints, which permit the extension and contraction of the struts. The struts ends are connected in pairs to the base and to the platform, forming an octahedron. The six struts provide the vibration isolation due to the properties of mechanical oscillators that behave as second-order lowpass filters for frequencies above the resonance. At high frequency, the ideal second-order low-pass filter response is spoiled by the distributed mass and the internal modes of membrane and of the platform with its payload

New Seismic Attenuation System (SAS) for the Advanced LIGO Configurations (LIGO2)

A new passive seismic attenuation system is being developed to replace the current passive attenuation stacks in LIGO 2, it is expected to drive the seismic contribution to the interferometer noise below any other noise source. The SAS will be effective completely starting at about 5 Hz, well inside the (uncompensated) gravity gradient noise wall

Overview of Advanced LIGO Adaptive Optics

This is an overview of the adaptive optics used in Advanced LIGO (aLIGO), known as the thermal compensation system (TCS). The TCS was designed to minimize thermally induced spatial distortions in the interferometer optical modes and to provide some correction for static curvature errors in the core optics of aLIGO. The TCS is comprised of ring heater actuators, spatially tunable CO_2 laser projectors, and Hartmann wavefront sensors. The system meets the requirements of correcting for nominal distortion in aLIGO to a maximum residual error of 5.4 nm rms, weighted across the laser beam, for up to 125 W of laser input power into the interferometer

Overview of Advanced LIGO Adaptive Optics

This is an overview of the adaptive optics used in Advanced LIGO (aLIGO), known as the thermal compensation system (TCS). The thermal compensation system was designed to minimize thermally-induced spatial distortions in the interferometer optical modes and to provide some correction for static curvature errors in the core optics of aLIGO. The TCS is comprised of ring heater actuators, spatially tunable CO$_{2}$ laser projectors and Hartmann wavefront sensors. The system meets the requirements of correcting for nominal distortion in Advanced LIGO to a maximum residual error of 5.4nm, weighted across the laser beam, for up to 125W of laser input power into the interferometer

The linear variable differential transformer (LVDT) position sensor for gravitational wave interferometer low-frequency controls

Low-power, ultra-high-vacuum compatible, non-contacting position sensors with nanometer resolution and centimeter dynamic range have been developed, built and tested. They have been designed at Virgo as the sensors for low-frequency modal damping of Seismic Attenuation System chains in Gravitational Wave interferometers and sub-micron absolute mirror positioning. One type of these linear variable differential transformers (LVDTs) has been designed to be also insensitive to transversal displacement thus allowing 3D movement of the sensor head while still precisely reading its position along the sensitivity axis. A second LVDT geometry has been designed to measure the displacement of the vertical seismic attenuation filters from their nominal position. Unlike the commercial LVDTs, mostly based on magnetic cores, the LVDTs described here exert no force on the measured structure

Current status of Japanese detectors

Current status of TAMA and CLIO detectors in Japan is reported in this article. These two interferometric gravitational-wave detectors are being developed for the large cryogenic gravitational wave telescope (LCGT) which is a future plan for detecting gravitational wave signals at least once per year. TAMA300 is being upgraded to improve the sensitivity in low frequency region after the last observation experiment in 2004. To reduce the seismic noises, we are installing new seismic isolation system, which is called TAMA Seismic Attenuation System, for the four test masses. We confirmed stable mass locks of a cavity and improvements of length and angular fluctuations by using two SASs. We are currently optimizing the performance of the third and fourth SASs. We continue TAMA300 operation and R&D studies for LCGT. Next data taking in the summer of 2007 is planned. CLIO is a 100-m baseline length prototype detector for LCGT to investigate interferometer performance in cryogenic condition. The key features of CLIO are that it locates Kamioka underground site for low seismic noise level, and adopts cryogenic Sapphire mirrors for low thermal noise level. The first operation of the cryogenic interferometer was successfully demonstrated in February of 2006. Current sensitivity at room temperature is close to the target sensitivity within a factor of 4. Several observation experiments at room temperature have been done. Once the displacement noise reaches at thermal noise level of room temperature, its improvement by cooling test mass mirrors should be demonstrated.Comment: 6 pages, 5 figures, Proceedings of GWDAW-1

Overview of Advanced LIGO Adaptive Optics

This is an overview of the adaptive optics used in Advanced LIGO (aLIGO), known as the thermal compensation system (TCS). The TCS was designed to minimize thermally induced spatial distortions in the interferometer optical modes and to provide some correction for static curvature errors in the core optics of aLIGO. The TCS is comprised of ring heater actuators, spatially tunable CO_2 laser projectors, and Hartmann wavefront sensors. The system meets the requirements of correcting for nominal distortion in aLIGO to a maximum residual error of 5.4 nm rms, weighted across the laser beam, for up to 125 W of laser input power into the interferometer

Le système d'alignement du banc de détection de l'expérience VIRGO de recherche d'ondes gravitationnelles

LE BUT DE L'EXPERIENCE FRANCO-ITALIENNE VIRGO, EST LA DETECTION DES ONDES GRAVITATIONNELLES AVEC UN INTERFEROMETRE DE MICHELSON-MORLEY, AYANT DES BRAS DE 3 KM DE LONG. CETTE ETUDE EST FOCALISEE SUR LE BANC DE DETECTION DE VIRGO, DONT LES FONCTIONS PRINCIPALES SONT DE FOURNIR LE SIGNAL D'ONDE GRAVITATIONNELLE ET D'AMELIORER SON RAPPORT SIGNAL SUR BRUIT EN UTILISANT UNE CAVITE OPTIQUE RESONNANTE. C'EST UN ENSEMBLE FORME DE COMPOSANTS OPTIQUES (UN CAVITE OPTIQUE FABRY-PEROT), MECANIQUES (MOTEURS SOUS VIDE), ELECTRONIQUES (PHOTODIODES, AMPLIFICATEURS) ET INFORMATIQUES (LECTURE, CONTROLE). PLACE DANS UNE ENCEINTE A VIDE POUR L'ISOLER DU BRUIT ACOUSTIQUE, IL EST AUSSI ACCROCHE A UNE SUSPENSION QUI L'ISOLE DU BRUIT SISMIQUE. L'OBJET DE CETTE THESE, EST L'ETUDE, LA REALISATION ET LE TEST DES SYSTEMES DE CONTROLE AUTOMATIQUE DE POSITION DU BANC : LE SYSTEME DE POSITIONNEMENT LOCAL CONTROLE PAR UNE CAMERA CCD ET LE SYSTEME GLOBAL, COMPRENANT UNE OPTIQUE D'ADAPTATION (TELESCOPE), DES CAPTEURS DE POSITION INSTALLES SUR LE BANC, AINSI QUE L'ELECTRONIQUE ET L'INFORMATIQUE ASSOCIEES. LE BRUIT RESIDUEL DU SYSTEME LOCAL, QUI CONTROLE LES SIX DEGRES DE LIBERTE DU BANC, EST DE 5RAD#R#M#S EN ANGLE ET DE 4M#R#M#S EN POSITION. LE SYSTEME GLOBAL QUI SUIT UN DES DEUX FAISCEAUX DE SORTIE DE L'INTERFEROMETRE, REDUIT LE BRUIT ANGULAIRE D'UN ORDRE DE GRANDEUR, CE QUI EST SUFFISANT POUR L'ALIGNEMENT CORRECT DE LA CAVITE RESONNANTE. L'ENSEMBLE DU SYSTEME DE POSITIONNEMENT DU BANC DE DETECTION PRESENTE DANS CE MEMOIRE SERA INSTALLE SUR LE SITE AU DEBUT DE L'ANNEE 1999 EN MEME TEMPS QUE LE RESTE DE LA PARTIE CENTRALE DE L'EXPERIENCE VIRGO.NI