The VLBI contribution to precession (present and future)

Similar documents
Evaluation of the accuracy of the IAU 2006/2000 precession-nutation

Report of the IAU WORKING GROUP "Nomenclature for Fundamental Astronomy" (NFA)

Comparison between high precision precession models for the ecliptic and the equator

5 Transformation Between the Celestial and Terrestrial Systems

Astronomy. Astrophysics. Expressions for IAU 2000 precession quantities. N. Capitaine 1,P.T.Wallace 2, and J. Chapront 1. 1.

On the definition and use of the ecliptic in modern astronomy

THE FREE CORE NUTATION

REPORT OF THE IAU DIVISION 1 WORKING GROUP ON NOMENCLATURE FOR FUNDAMENTAL ASTRONOMY (NFA)

REPORT OF THE INTERNATIONAL ASTRONOMICAL UNION DIVISION I WORKING GROUP ON PRECESSION AND THE ECLIPTIC

High precision methods for locating the celestial intermediate pole and origin ABSTRACT

Proposed terminology for Fundamental Astronomy based on IAU 2000 resolutions

Rotation matrix from the mean dynamical equator and equinox at J to the ICRS

Definition of the Celestial Ephemeris Origin and of UT1 in the International Celestial Reference Frame

Software for Implementing the IAU 2000 Resolutions

ASTRONOMICAL REFERENCE SYSTEMS AND FRAMES, ASTROMETRIC TECHNIQUES AND CATALOGS

ROCZNIK ASTRONOMICZNY (ASTRONOMICAL ALMANAC) OF THE INSTITUTE OF GEODESY AND CARTOGRAPHY AGAINST THE IAU 2000 RESOLUTIONS

DRAFT OF NOMENCLATURE & TERMINOLOGY FOR IAU WG 1

Effects of zonal deformations and the Earth s rotation rate variations on precession-nutation

the precession-nutation parameters and Greenwich sidereal time, which Ephemeris Pole (CEP) has to be extended in order to be consistent with

The 3D representation of the new transformation from the terrestrial to the celestial system.

ESTIMATION OF NUTATION TERMS USING GPS

Nutation determination by means of GNSS

Application of the new concepts and definitions (ICRS, CIP and CEO) in fundamental astronomy. P. K. Seidelmann and J. Kovalevsky

IAU 2006 NFA GLOSSARY

COMBINING GPS AND VLBI MEASUREMENTS OF CELESTIAL MOTION OF THE EARTH S SPIN AXIS AND UNIVERSAL TIME. Jan VONDRÁK* and Cyril RON

CHAPTER 5 TRANSFORMATION BETWEEN THE CELESTIAL AND

DIVISION I WORKING GROUP on NOMENCLATURE FOR FUNDAMENTAL ASTRONOMY (NFA)

Precession, nutation, and space geodetic determination of the Earth s variable gravity field

Precise modeling of the precession-nutation of Mars

Reference system and non-rotating origin: the NRO for the rest of us Olivier de Viron, Véronique Dehant, and Nicole Capitaine

The Influence of Galactic Aberration on Precession Parameters Determined from VLBI Observations

Theory of the rotation of the rigid Earth

Determination of the lunar orbital and rotational parameters and of the ecliptic reference system orientation from LLR measurements and IERS data

Orbits. von Guochang Xu. 1. Auflage. Orbits Xu schnell und portofrei erhältlich bei beck-shop.de DIE FACHBUCHHANDLUNG

Second-order torque on the tidal redistribution and the Earth s rotation ABSTRACT

SOFA Tools for Earth Attitude

Numerical evidence for the inconsistent separation of the ITRF-ICRF transformation into precession-nutation, diurnal rotation and polar motion

National Astronomical Observatory, Mitaka, Tokyo , Japan. proper motion system of the Hipparcos frame. The analysis suggests

Towards sub-microarsecond rigid Earth nutation series in. Abstract. The nonrigid Earth nutation series adopted by the IAU (International

Earth orientation parameters: excitation by atmosphere, oceans and geomagnetic jerks

2 Conventional Celestial Reference System and Frame

Defining Sources Selection and Celestial Reference Frame Stability

Global reference systems and Earth rotation

SOFA Tools for Earth Attitude

Influence of the inner core on the rotation of the Earth revisited

Celestial Mechanics III. Time and reference frames Orbital elements Calculation of ephemerides Orbit determination

Astrodynamics (AERO0024)

Space-Time Reference Systems

THE LUNAR LIBRATION: COMPARISONS BETWEEN VARIOUS MODELS- A MODEL FITTED TO LLR OBSERVATIONS

User s Guide to NOVAS Version C3.0

The celestial reference system and its role in the epoch of global geodetic technologies

1 General Definitions and Numerical Standards

From Gaia frame to ICRF-3 3?

Analysis of the Accuracy of Prediction of the Celestial Pole Motion

USNO Circular 180 Errata Rev. A

arxiv:astro-ph/ v1 17 Jul 2003

Astrometry in Gaia DR1

Empiric Models of the Earth s Free Core Nutation

1. COMMENTS ON TERMINOLOGY: IDEAL AND CONVENTIONAL REFERENCE SYSTEMS AND FRAMES

Estimation of Geodetic and Geodynamical Parameters with VieVS

FUNDAMENTAL ASTRONOMY

Determination of the free lunar libration modes from ephemeris DE430

GOCE High Level Processing Facility. GOCE Standards. Doc. No.: GO-TN-HPF-GS-0111 Issue: 3 Revision: 1 Date: 30 / 04 / 2009

Past, present and possible updates to the IERS Conventions. J. Ray, NGS G. Petit, BIPM

Compatibility of the IERS earth rotation representation and its relation to the NRO conditions

Astrodynamics (AERO0024)

Errata in The Explanatory Supplement to the Astronomical Almanac (3rd edition, 1st printing)

Very Long Baseline Interferometry for Geodesy and Astrometry

Optical Reference Star Catalogs for Space Surveillance: Current Status and Future Plans

Implementing the IAU 2000 Resolutions in Almanacs

FREE CORE NUTATION: NEW LARGE DISTURBANCE AND CONNECTION EVIDENCE WITH GEOMAGNETIC JERKS

NGA GNSS Division Precise Ephemeris Parameters

Recent advances in modeling precession-nutation

SSM/I and SSMIS Stewardship Code Geolocation Algorithm Theoretical Basis

Very Long Baseline Interferometry for Geodesy and Astrometry

GRACE (CSR-GR-03-03)

Remaining error sources in the nutation at the submilliarc second level

The final publication is available at Springer. DOI: / _6

4sec 2xtan 2x 1ii C3 Differentiation trig

The Position of the Sun. Berthold K. P. Horn. necessary to know the position of the sun in the sky. This is particularly

Optical Reference Stars for Space Surveillance: Future Plans: Latest developments

RELATIVISTIC ASPECTS IN ASTRONOMICAL STANDARDS AND THE IERS CONVENTIONS

GRACE. Gravity Recovery and Climate Experiment. JPL Level-2 Processing Standards Document. For Level-2 Product Release 05.1

User s Guide to NOVAS Version C3.1

Astronomical Institute, Academy of Sciences of the Czech Republic, Abstract. The most recent solution of Earth orientation parameters

PRECESSION, NUTATION, AND WOBBLE OF THE EARTH

RECOMMENDATION ITU-R S Impact of interference from the Sun into a geostationary-satellite orbit fixed-satellite service link

Grupo demecanica Celeste, Facultad de Ciencias, Valladolid, Spain. Dept. Applied Mathematics, University of Alicante, Alicante, Spain

HM NAUTICAL ALMANAC OFFICE NAO TECHNICAL N OTE

M2 GLOSSARY aphelion: the point in an orbit that is the most distant from the Sun. apocenter: the point in an orbit that is farthest from the origin o

Global and local bias in the FK5 from the Hipparcos data

aberration (of light): aberration, annual: aberration, diurnal: aberration, E-terms of: aberration, elliptic: aberration, planetary:

Celestial mechanics in a nutshell

A Comparison of Radio and Optical Astrometric Reduction Algorithms

10 General Relativistic Models for Space-time Coordinates and Equations of Motion

Recent and Anticipated Changes to the International Earth Rotation and Reference Systems Service (IERS) Conventions

Geometry of Earth Sun System

Introduction Fundamental definitions Motivation

Modern Navigation. Thomas Herring

GOCE High Level Processing Facility. GOCE Standards. Doc. No.: GO-TN-HPF-GS-0111 Issue: 4 Revision: 0 Date: 14 / 05 / 2014

Transcription:

The VLBI contribution to precession (present and future) N.Capitaine (1) and P. Wallace (2) (1) Observatoire de Paris/Syrte (2) RAL, HMNAO

Precession-nutation parameters Classical: equinox-based fixed ecliptic of epoch ^ Precession of the ecliptic χ A + χ ψ A ω A ψ γ 1 1 ω A + ε 1 γ 1 γ χ A ecliptic of date ε O γ m γ O ψ ε + ε A ε A GST 90 ο - 90 ο + z A equator of date ζ A nutation of the equator α( σ) γ equinox ϖ instantaneous origin of longitude s σ CEO Σ o Σ 90 + E 90 + E Q θ mean equator of date θ A mean equator of epoch N d stellar angle Precession of the equator New: CEO based ϖ (TEO) moving equator celestial reference plane CRS Precession-nutation of the equator

VLBI estimation of celestial pole offsets w.r.t. 1976/1980 precession-nutation model VLBI provides the actual position of the pole in the GCRS -> corrections to the model + frame biases

Position of the CIP in GCRS and ITRS position of the CIP in the GCRS (OX 0 Y 0 Z 0 ) : E, d position of the CIP in the ITRS (Ox 0 y 0 z 0 ): F, g <- Celestial Intermediate Pole X=sind cose, Y=sind sine are the x, y-coordinates of the CIP unit vector provides directly where the pole is in the sky

IAU 2000 precession-nutation IAU 2000 Nutation (FCN not included) IAU 2000A : for high precision level luni-solar terms (678) + planetary terms (687) (Mathews et al. 2002) based on rigid Earth nutation (Souchay et al. 1999), MHB transfer function and VLBI data 7 basic Earth parameters (BEP) including H (dynamical flattening) IAU 2000B (its shorter version): for 1 mas level (McCarthy & Luzum 2002) Precession component of the IAU 2000 model Lieske et al. 1977 + improved rates of precession ψ Α IAU 2000(- 0.299 650 +- 0.000 400) /c ω Α IAU 2000(- 0.025 240 +- 0.000 100) /c Celestial pole offsets at J2000 in the GCRS (VLBI estimates) ξ 0 (IAU 2000) = (- 16.6170 +- 0.0100) η (IAU 2000) = (- 6.8192 +- 0.0100)

IAU 2000 expressions for X and Y (Capitaine, Chapront, Lambert, Wallace 2003, A&A 400) Σ!" # #$!"% Σ!" # #$!"% Σ!" # #$!"% & Σ # #$!"!"% Σ # #$!"!"% Σ # #$!"!"%

IAU 2000 expression for GST (Capitaine, Wallace, McCarthy 2003, A&A 406). θ' ψ ψ ω ε #χ ψ cosε Α ψ 1 cosω Α θ accumulated precession in RA (in TT) ψε Σ!α µ"!ω kinematical equation of equinoxes

Further improvement in Precession Expressions for the precession of the equator should be (i) solutions of the dynamical equations for the Earth s rotation and (ii) referred to an improved ecliptic precession w.r.t Lieske et al. 1977 -> New models compatible with IAU 2000 with improved dynamical consistency - Bretagnon P., Fienga A., Simon J.L. (2003, A&A 400): BO3 VSOP87 ecliptic + SMART 97 nutation + MHB precession rate in longitude - Fukushima (2003, A.J. 126): F03 ecliptic fitted to DE405 (1600-2200) + SF01 nutation + quadratic fit to VLBI + Harada & Fukushima (2004, A.J. 127): HF04 ecliptic - Capitaine N., Wallace P., Chapront J. (2003, A&A 412): P03 ecliptic based on both VSOP87 and fit to DE406 (2000-yr interval) + integration of dynamical equations for precession + MHB precession rates in longitude and obliquity -> IAU Division I WG on «Precession and ecliptic» established at the 2003 GA (Chair: J. Hilton) to recommend a new model - Capitaine N., Wallace P.W., Chapront J. (2004, A&A) Comparison between precession models

5 P_A : Differences with respect to IAU2000 VSOP2000 W94/B03 2.5 F03 mas 0 P03-2.5 HF04 St82-5 1 800 1 900 2 000 2 100 2 200 Year

10 Q_A : Differences with respect to IAU2000 VSOP2000 W94/B03 5 St82 mas 0 P03-5 HF04 F03-10 1 800 1 900 2 000 2 100 2 200 Year

P03 precession Capitaine, Wallace, Chapront, 2003, A&A 412 Improvement of the ecliptic precession (based on VSOP/DE406) Choice of the integration constants (non-rigid Earth model based on MHB2000, Williams 1994 and corrections for perturbing effects on the observed quantities) Improvement of the precession of the equator (based on: dynamical precession equations, improved ecliptic, updated MHB integration constants) Discussion on the precession parameters (rotation vector approach, X, Y approach)

P03 solution The derived precession in longitude is in fact the projection of the observed quantity on the conventional ecliptic with a conventional obliquity used in the current VLBI software ψ A ψ A sinε A

Comparison: equator precession solutions unit: mas Source t t 2 t 3 t 4 t 5 IAU1976 (L77) 5038778.4 1072.59 1.147 IAU2000 5038478.750 1072.59 1.147 W94 5038456.501 1078.977 1.141 0.133 B03 5038478.750 1071.9530 1.14366 0.132832 0.0000940 F03 ψ A 5038478.143 1079.1653 1.10654 0.129144 P03 prel 5038478.750 1079.0091 1.14044 0.132851 0.0000951 P03 5038481.507 1079.0069 1.14045 0.132851 0.0000951 IAU1976 (L77) 0.0 51.27 7.726 IAU2000 25.240 51.27 7.726 W94 24.4 51.268 7.727 0.000000 B03 26.501 51.2769 7.72723 0.000492 0.0003329 F03 ω A ɛ 0 21.951 53.9411 7.19621 +0.001907 P03 prel 25.240 51.2623 7.72502 0.000467 0.0003337 P03 25.754 51.2623 7.72503 0.000467 0.0003337

10 ΨA : Differences with respect to P03 5 mas 0-5 IAU 2000 B03 F03-10 1800 1900 2000 2100 2200 Year

10 ωa : Differences with respect to P03 5 mas 0-5 IAU 2000 B03 F03-10 1800 1900 2000 2100 2200 Year

P03 expressions for X and Y (Capitaine, Wallace, Chapront 2003, A&A 412) Σ!" # #$!"% Σ!" # #$!"% Σ!" # #$!"% & Σ # #$!"!"% Σ # #$!"!"% Σ # #$!"!"%

IAU 2000A minus VLBI, dx (no FCN corrections) 4000 3000 dx (microarcseconds) 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000-3000 -4000 year IAU 2000A minus VLBI, dx (i) the IAU 2000 model gives a considerably better fit to the data (ii) the data before 1990 are very noisy 4000 3000 (iii) The FCN must be corrected dx (microarcseconds) 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000-3000 -4000 year

IAU 2000A minus VLBI, dx 4000 C 0 + C 1 t+ C 2 t 2 3000 dx (microarcseconds) 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000-3000 RMS= 374 µas C 0 =(1 +- 10) µas C 1 = (-1368 +- 304) µas C 2 =(-11414 +-2579) µas Corr(C 1 C 2 )=0.9-4000 year P03 minus VLBI, dx 4000 3000 dx (microarcseconds) 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000 RMS= 374 µas C 0 =(2 +- 10) µas C 1 = (-1119 +- 304) µas C 2 =(-13296 +-2580) µas Corr(C 1 C 2 )=0.9-3000 -4000 year

IUA 2000A minus VLBI, dy 4000 3000 C 0 + C 1 t+ C 2 t 2 dy (microarcseconds) 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000-3000 -4000-5000 year P03 minus VLBI, dy RMS= 416 µas C 0 =(33 +- 11) µas C 1 = (2134 +- 338) µas C 2 =(24024 +- 2870) µas Corr(C 1 C 2 )=0.9 dy (microarcseconds) 4000 3000 2000 1000 0 1980 1985 1990 1995 2000 2005-1000 -2000-3000 -4000 RMS= 416 µas C 0 =(33 +- 11) µas C 1 = (1620 +- 338) µas C 2 =(23991 +- 2870) µas Corr(C 1 C 2 )=0.9-5000 year

Summary VLBI is potentially the most powerful technique to estimate the motion of the celestial equator w.r.t. GCRS (and consequently the precession of the equator) but not the ecliptic precession The IAU 2000A precession-nutation which consists only on corrections to the precession rates in longitude and obliquity of the IAU 1976 precession is not dynamically consistent but gives a very good fit to VLBI Improvement in the precession model for the ecliptic is necessary (few mas in the t term): the resulting effect on the precession of the equator is at a level of 100 µ as for one century (on the t 2 term in ψ Α ) Improvement in the precession model for the equator is necessary. However, the possible improvement in the model is dependent on the model for some parameters of the non-rigid Earth as the J2 rate Observations covering a longer period of time are necessary to separate - the precession rates and amplitudes of long-period nutations - the precession rates and the t 2 terms in the developments (indirect access to the motion of the ecliptic).

Conclusion What is required from VLBI in the future in order it can be powerful at the present level of accuracy for discriminating between various precession models: - Refined ICRF (without any global rotation + the largest number of sources) - longest interval of celestial pole offsets with low noise level and no systematic error (FCN) - Adopt IAU 2000 precession-nutation model in order than the celestial pole offsets can be considered as being first order quantities - Adopt the X, Y representation that is close to the parameters to which VLBI is sensitive - Adopt the CEO instead of the equinox to avoid possible risks of inconsistencies in the terrestrial to celestial transformation (for microarcsecond accuracy) In parallel: Models for contribution (t term and t 2 term) to precession of a non-rigid Earth have to be improved ( improved MHB)