Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories
The proposed Laser Interferometer Space Antenna (LISA) mission features a three-satellite constellation realizing a long-arm interferometer designed to observe gravitational waves emitted by a multitude of stellar, galactic, and possibly cosmic sources not accessible to ground-based detectors. In su...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2022-06, Vol.45 (6), p.1078-1092 |
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container_title | Journal of guidance, control, and dynamics |
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creator | Houba, Niklas Delchambre, Simon Ziegler, Tobias Fichter, Walter |
description | The proposed Laser Interferometer Space Antenna (LISA) mission features a three-satellite constellation realizing a long-arm interferometer designed to observe gravitational waves emitted by a multitude of stellar, galactic, and possibly cosmic sources not accessible to ground-based detectors. In support of maximizing LISA’s scientific return, this paper presents an on-orbit excitation and estimation strategy for tilt-to-length coupling noise, a fundamental limitation of the detection sensitivity of spaceborne long-arm interferometers. Tilt-to-length coupling describes the distortion of measurements through the relative attitude jitter of the spacecraft. In operation, inevitable instrument imperfections and misalignments will cause the effect to scale proportionally with the jitter strength, the proportionality factor being referred to as the tilt-to-length coupling factor. For the first time, analytical equations are derived modeling the impact of tilt-to-length coupling on the scientific observations. These equations are shown to define the optimal on-orbit excitation needed to estimate this noise source, enabling the correction of the recorded gravitational wave signals and achievement of LISA’s required detection sensitivity. |
doi_str_mv | 10.2514/1.G006064 |
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In support of maximizing LISA’s scientific return, this paper presents an on-orbit excitation and estimation strategy for tilt-to-length coupling noise, a fundamental limitation of the detection sensitivity of spaceborne long-arm interferometers. Tilt-to-length coupling describes the distortion of measurements through the relative attitude jitter of the spacecraft. In operation, inevitable instrument imperfections and misalignments will cause the effect to scale proportionally with the jitter strength, the proportionality factor being referred to as the tilt-to-length coupling factor. For the first time, analytical equations are derived modeling the impact of tilt-to-length coupling on the scientific observations. These equations are shown to define the optimal on-orbit excitation needed to estimate this noise source, enabling the correction of the recorded gravitational wave signals and achievement of LISA’s required detection sensitivity.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G006064</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aerospace environments ; Coupling ; Excitation ; Gravitational waves ; Interferometers ; LISA (antenna) ; Noise ; Observatories ; Optimization ; Satellite constellations ; Sensitivity ; Vibration</subject><ispartof>Journal of guidance, control, and dynamics, 2022-06, Vol.45 (6), p.1078-1092</ispartof><rights>Copyright © 2021 by Airbus Defence and Space GmbH. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. 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In support of maximizing LISA’s scientific return, this paper presents an on-orbit excitation and estimation strategy for tilt-to-length coupling noise, a fundamental limitation of the detection sensitivity of spaceborne long-arm interferometers. Tilt-to-length coupling describes the distortion of measurements through the relative attitude jitter of the spacecraft. In operation, inevitable instrument imperfections and misalignments will cause the effect to scale proportionally with the jitter strength, the proportionality factor being referred to as the tilt-to-length coupling factor. For the first time, analytical equations are derived modeling the impact of tilt-to-length coupling on the scientific observations. These equations are shown to define the optimal on-orbit excitation needed to estimate this noise source, enabling the correction of the recorded gravitational wave signals and achievement of LISA’s required detection sensitivity.</description><subject>Aerospace environments</subject><subject>Coupling</subject><subject>Excitation</subject><subject>Gravitational waves</subject><subject>Interferometers</subject><subject>LISA (antenna)</subject><subject>Noise</subject><subject>Observatories</subject><subject>Optimization</subject><subject>Satellite constellations</subject><subject>Sensitivity</subject><subject>Vibration</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNotkE1LAzEYhIMoWKsH_0HAk4fUN9-7Rym1CsUerAheQnY30S1rsyZpof_ere1pLjPDzIPQLYUJk1Q80MkcQIESZ2hEJeeEF4U4RyPQnBIJJVyiq5TWAJQrqkfoc9nn9sd2eJYOmtuwwcHjVdtlkgNZuM1X_savoU0O-xDxW29rV4W4cXge7a7N_xHbkQ-7c3hZJRd3NofYunSNLrztkrs56Ri9P81W02eyWM5fpo8LUtNCZ-IVE1RY21RayMqXUjdeutICB1VLYJUQthFUaaGgrkEzJZgaXjVFCVQWjo_R3bG3j-F361I267CNw6ZkmFKsZKXWxeC6P7rqGFKKzps-Dofj3lAwB3SGmhM6_gfueF-s</recordid><startdate>20220601</startdate><enddate>20220601</enddate><creator>Houba, Niklas</creator><creator>Delchambre, Simon</creator><creator>Ziegler, Tobias</creator><creator>Fichter, Walter</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>20220601</creationdate><title>Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories</title><author>Houba, Niklas ; Delchambre, Simon ; Ziegler, Tobias ; Fichter, Walter</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c187t-f62414aadb745bf957df5e9a0306c502b44ad4167460cc0726426388d890158e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aerospace environments</topic><topic>Coupling</topic><topic>Excitation</topic><topic>Gravitational waves</topic><topic>Interferometers</topic><topic>LISA (antenna)</topic><topic>Noise</topic><topic>Observatories</topic><topic>Optimization</topic><topic>Satellite constellations</topic><topic>Sensitivity</topic><topic>Vibration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Houba, Niklas</creatorcontrib><creatorcontrib>Delchambre, Simon</creatorcontrib><creatorcontrib>Ziegler, Tobias</creatorcontrib><creatorcontrib>Fichter, Walter</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Houba, Niklas</au><au>Delchambre, Simon</au><au>Ziegler, Tobias</au><au>Fichter, Walter</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2022-06-01</date><risdate>2022</risdate><volume>45</volume><issue>6</issue><spage>1078</spage><epage>1092</epage><pages>1078-1092</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>The proposed Laser Interferometer Space Antenna (LISA) mission features a three-satellite constellation realizing a long-arm interferometer designed to observe gravitational waves emitted by a multitude of stellar, galactic, and possibly cosmic sources not accessible to ground-based detectors. In support of maximizing LISA’s scientific return, this paper presents an on-orbit excitation and estimation strategy for tilt-to-length coupling noise, a fundamental limitation of the detection sensitivity of spaceborne long-arm interferometers. Tilt-to-length coupling describes the distortion of measurements through the relative attitude jitter of the spacecraft. In operation, inevitable instrument imperfections and misalignments will cause the effect to scale proportionally with the jitter strength, the proportionality factor being referred to as the tilt-to-length coupling factor. For the first time, analytical equations are derived modeling the impact of tilt-to-length coupling on the scientific observations. 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subjects | Aerospace environments Coupling Excitation Gravitational waves Interferometers LISA (antenna) Noise Observatories Optimization Satellite constellations Sensitivity Vibration |
title | Optimal Estimation of Tilt-to-Length Noise for Spaceborne Gravitational-Wave Observatories |
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