On the extension of Helmert transform

The article deals with the method of comparison of the coordinate systems used by two quite different scientific disciplines: stellar astronomy and the geodesy. Geodesic Helmert transform is analysed along with a series of stellar astronomy kinematic models: Kovalsky-Airy, Lindbladt-Oort and Ogorodn...

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Datum:2014
1. Verfasser: Choliy, V.Ya.
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Veröffentlicht: Головна астрономічна обсерваторія НАН України 2014
Schriftenreihe:Advances in Astronomy and Space Physics
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spelling irk-123456789-1198022017-06-10T03:03:09Z On the extension of Helmert transform Choliy, V.Ya. The article deals with the method of comparison of the coordinate systems used by two quite different scientific disciplines: stellar astronomy and the geodesy. Geodesic Helmert transform is analysed along with a series of stellar astronomy kinematic models: Kovalsky-Airy, Lindbladt-Oort and Ogorodnikov-Milne. An analogy was built allowing us to propose an extension to the Helmert transform. In the second part of the article, three different approaches to the solution of the correlation problem are compared, and the results of the numerical experiment are presented. 2014 Article On the extension of Helmert transform / V.Ya. Choliy // Advances in Astronomy and Space Physics. — 2014. — Т. 4., вип. 1-2. — С. 15-19. — Бібліогр.: 12 назв. — англ. 2227-1481 DOI: 10.17721/2227-1481.4.15-19 http://dspace.nbuv.gov.ua/handle/123456789/119802 en Advances in Astronomy and Space Physics Головна астрономічна обсерваторія НАН України
institution Digital Library of Periodicals of National Academy of Sciences of Ukraine
collection DSpace DC
language English
description The article deals with the method of comparison of the coordinate systems used by two quite different scientific disciplines: stellar astronomy and the geodesy. Geodesic Helmert transform is analysed along with a series of stellar astronomy kinematic models: Kovalsky-Airy, Lindbladt-Oort and Ogorodnikov-Milne. An analogy was built allowing us to propose an extension to the Helmert transform. In the second part of the article, three different approaches to the solution of the correlation problem are compared, and the results of the numerical experiment are presented.
format Article
author Choliy, V.Ya.
spellingShingle Choliy, V.Ya.
On the extension of Helmert transform
Advances in Astronomy and Space Physics
author_facet Choliy, V.Ya.
author_sort Choliy, V.Ya.
title On the extension of Helmert transform
title_short On the extension of Helmert transform
title_full On the extension of Helmert transform
title_fullStr On the extension of Helmert transform
title_full_unstemmed On the extension of Helmert transform
title_sort on the extension of helmert transform
publisher Головна астрономічна обсерваторія НАН України
publishDate 2014
url http://dspace.nbuv.gov.ua/handle/123456789/119802
citation_txt On the extension of Helmert transform / V.Ya. Choliy // Advances in Astronomy and Space Physics. — 2014. — Т. 4., вип. 1-2. — С. 15-19. — Бібліогр.: 12 назв. — англ.
series Advances in Astronomy and Space Physics
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first_indexed 2025-07-08T16:38:03Z
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fulltext On the extension of Helmert transform V.Ya.Choliy1,2∗ Advances in Astronomy and Space Physics, 4, 15-19 (2014) © V.Ya.Choliy, 2014 1Faculty of Physics, Taras Shevchenko National University of Kyiv, Glushkova ave., 4, Kyiv 03127, Ukraine 2Main Astronomical Observatory of the NAS of Ukraine, Akademika Zabolotnoho Str. 27, Kyiv 03680, Ukraine The article deals with the method of comparison of the coordinate systems used by two quite di�erent scienti�c disciplines: stellar astronomy and the geodesy. Geodesic Helmert transform is analysed along with a series of stellar astronomy kinematic models: Kovalsky-Airy, Lindbladt-Oort and Ogorodnikov-Milne. An analogy was built allowing us to propose an extension to the Helmert transform. In the second part of the article, three di�erent approaches to the solution of the correlation problem are compared, and the results of the numerical experiment are presented. Key words: stellar astronomy, geodesy, mathematical methods introduction Let us state several de�nitions �rst. The con- struction of a coordinate systems for the sky (galax- ies, quasars) or for the Earth (cities, geodetic mark- ers, GPS navigators) leads to a catalogue of coordi- nates of objects. Thus, the word �catalogue� in this article always refers to a set of object coordinates, while catalogue objects are referred as points. An essential method for building catalogues is through observations and subsequent processing. There are no possibilities to build absolute cata- logues, as objects tend to change their positions. There are individual object velocities, due to galactic rotation in the case of celestial coordinate systems, and due to tectonic movements and secular tidal ef- fects in the case of Earth coordinate systems. That is why one should always specify the catalogue epoch and precision, meaning its systematic (averaged over all objects) and random (every object has own error) precisions. The only way to determine such errors is through the comparison of di�erent catalogues. Furthermore, a catalogue should not be inter- preted as just a list of point coordinates. Every cata- logue de�nes its own coordinate system. This should be kept in mind when using the catalogue. Through- out the years, geodesy has constructed of numerous catalogues of terrestrial objects, and has de�ned nu- merous Terrestrial Reference Frames (TRF). Astron- omy has done the same with respect to catalogues of celestial bodies, and has similarly de�ned numerous Celestial Reference Frames (CRF). Space geodynam- ics makes use of both types of catalogues. Determi- nation of the transformation between CRF and TRF is its main task. In this article we will not anal- yse geodynamic transformations, but the TRFs and CRFs themselves only. Let ~ri be the coordinate of some object given in i-th xRF (x might be C or T, but C and T may never be present simultaneously in the same for- mula). Spherical coordinates in TRF are λ � longi- tude, and ϕ � lattitude. If ri if the distance from the centre, then: ~ri = ri (cosλ cosϕ, sinλ cosϕ, sinϕ) T . For TRF ri ≈ R⊕, the Earth' radius. Spherical coordinates in CRF are α � right as- cension and δ � declination. Following the spherical astronomy de�nition where all sources are placed on the same celestial sphere of any useful radius R� we will have the same coordinate de�nitions: ~ri = ri (cosα cos δ, sinα cos δ, sin δ)T . For CRF ri = R�, usually 1. Helmert transform was proposed for the compar- ison of di�erent geodesic catalogues (read: TRFs) by Friedrich Robert Helmert (1843�1917), director of Potsdam geodetic institute and Professor at the University of Berlin [11]. He introduced shift plus rotation transform. It is widely used until now, see for example [2, 3, 10], and not only for TRF/CRF comparison [4]. But there are other possibilities to be analysed. shifted centres, parallel axes In this case for any point: ~r2 = ~r1 +~b, (1) ∗ charlie@univ.kiev.ua 15 Advances in Astronomy and Space Physics V.Ya.Choliy where ~b is the shift of the centres. In stellar astron- omy we may suppose that ~r1 and ~r2 are coordinates in catalogues built for two distinct epochs with time interval ∆t between them. That is: ~b = ~V∆t = ~r2 − ~r1. Point coordinates may change: ~r2 = ~r1 + d~r dt ∣∣∣∣ 1 ∆t = ~r1 + ~µ∆t, where ~µ is a proper motion vector. In spherical coordinates: ~V∆t = d~r dt ∣∣∣∣ 1 ∆t, or ~V =  ṙ cosα cos δ − r sinαα̇ cos δ − r cosα sin δδ̇ ṙ sinα cos δ + r cosαα̇ cos δ − r sinα sin δδ̇ ṙ sin δ + r cos δδ̇  . In matrix notations: ~V = ( X Y Z ) = = ( r cosα cos δ −r sinα −r cosα sin δ r sinα cos δ r cosα −r sinα sin δ r sin δ 0 r cos δ ) × × ( ṙ/r α̇ cos δ δ̇ ) . (2) With generally used stellar astronomy designations: ṙ = Vr, α̇ cos δ = µα, δ̇ = µδ having in mind ∆t = 1 year and after inverting the matrix in (2):( Vr/r µα µδ ) = ( cosα cos δ sinα cos δ sin δ sinα − cosα 0 − cosα sin δ sinα sin δ cos δ ) × × ( X/r Y/r Z/r ) . (3) Or without matrices:{ Vr/r = X/r cosα cos δ + Y/r sinα cos δ + Z/r sin δ, µα = X/r sinα− Y/r cosα, µδ = −X/r cosα sin δ + Y/r sinα sin δ + Z/r cos δ, (4) which is more essential for classical classroom pre- sentation. The two last equations in (4) are identical to the Kovalsky-Airy model. The �rst one is used to deter- mine the Sun's velocity from radial stellar velocities only [9], here (X,Y, Z)T = ~V�. In geodesy we may use (1), or the Kovalsky-Airy model (3), for exam- ple for comparison of geocentre positions determined from VLBI and SLR. Both relations are identical and di�er only in mathematical writing style. shifted centres, non-parallel axes Following Helmert we imply that two RFs have di�erent centres and their axes might coincide through three rotations around three coordinate axes: ~r2 = B~r1 +~b = R(n)Q(m)P(l)~r1 +~b, (5) where P,Q,R are three elementary rotation matrices around x, y, z axes respectively. In the general case, angles l,m, n are small and their cosines might be re- placed with unity, and sinuses with their arguments. It gives us: B = ( 1 l 0 −l 1 0 0 0 1 )( 1 0 −m 0 1 0 m 0 1 )( 1 0 0 0 1 n 0 −n 1 ) , and: ~r2 = ( 1 l −m −l 1 n m −n 1 ) ~r1 +~b. (6) While the angles remain small, the result does not depend upon the order of multiplications. For the next step, let us extract a unity matrix from the right side, move it to the left side: ~r2 − ~r1 = ( 0 l −m −l 0 n m −n 0 ) ~r1 +~b = A~r1 +~b, which may be rewritten in yet another form (here x1, y1, z1 are components of the vector ~r1): ~r2 − ~r1 = ( ly1 −mz1 nz1 − lx1 mx1 − ny1 ) +~b = [~ω × ~r1] +~b, (7) where ~ω = (n,m, l)T = (ω1, ω2, ω3) T is an angular velocity vector which is generally used to explain ro- tation from RF1 to RF2. It is a well-known result, as any rotations around the main coordinate axes can be replaced with only one around some specially selected axis. Inserting sphericals into (7) gives: ( r cosα cos δ −r sinα −r cosα sin δ r sinα cos δ r cosα −r sinα sin δ r sin δ 0 r cos δ ) × × ( Vr/r µα µδ ) = ( ω2z − ω3y ω3x− ω1z ω1y − ω2x ) + ( X Y Z ) , 16 Advances in Astronomy and Space Physics V.Ya.Choliy or after matrix inversion, rewriting without matrices: Vr/r = X/r cosα cos δ + Y/r sinα cos δ + Z/r sin δ, µα = −X/r sinα+ Y/r cosα− ω1 cosα sin δ− −ω2 sinα sin δ + ω3 cos δ, µδ = −X/r cosα sin δ − Y/r sinα sin δ + Z/r cos δ+ +ω1 sinα− ω2 cosα. (8) Thus, starting from (5) and supposing that rota- tions are small, we came to the Lindblat-Oort model of stellar astronomy [8]. Let us have a look at (6) again, where [~ω × ~r1] = A~r1, A is an antisymmetric matrix, and A~r1 or al- ternatively [~ω × ~r1] de�nes the velocity �eld essential for the �rst catalogue. That velocity �eld moves the points of the �rst catalogue to the positions of the second one in full analogy with liquid �ow, with the points immersed into that liquid. The points are the partices �owing from the �rst catalogue positions to the second catalogue positions. This analogy lead us to the third model. deformable velocity field with shifted centres and non-parallel axes If the velocity �led is de�ned by matrix (or ten- sor)A, can we add another part to that tensor? Since the transformation matrix (or velocity �eld tensor) A is antisymmetric, let us add the symmetric part S as well. A new model arises: ~r2 − ~r1 = [~ω × ~r1] +~b+ S~r1. (9) A symmetric matrix explains additional deforma- tions of the velocity �eld. Interpretation of these values are as follows: diagonal elements explain scal- ing along their axes, while non-diagonal elements ex- plain the pressure e�ects within their planes. Substitution of stellar astronomy formulas into (9) leads to the classical Ogoridnikov-Milne model [6, 7] in matrix form: ( r cosα cos δ −r sinα −r cosα sin δ r sinα cos δ r cosα −r sinα sin δ r sin δ 0 r cos δ ) × × ( Vr/r µα µδ ) = ( ω2z − ω3y ω3x− ω1z ω1y − ω2x ) + ( X Y Z ) + + ( S11x+ S12y + S13z S12x+ S22y + S23z S13x+ S23y + S33z ) , or without matrices: Vr/r = X/r cosα cos δ + Y/r sinα cos δ+ +Z/r sin δ + S12 sin 2α cos2 δ+ +S13 cosα sin 2δ + S23 sinα sin 2δ+ +S11 cos 2 α cos2 δ + S22 sin 2 α cos2 δ+ +S33 sin 2 δ, µα = −X/r sinα+ Y/r cosα− −ω1 cosα sin δ − ω2 sinα sin δ+ +ω3 cos δ + S12 cos 2α cos δ− −S13 sinα+ S23 cosα sin δ− −(S11 − S22)/2 sin 2α cos δ, µδ = −X/r cosα sin δ − Y/r sinα sin δ+ +Z/r cos δ + ω1 sinα− ω2 cosα− −S12 sin 2α sin 2δ/2+ +S13 cosα cos 2δ + S23 sinα cos 2δ− −(S11 − S22)/2 cos 2 α sin 2δ+ +(S33 − S22)/2 sin 2δ. A geodesic transformation of type (9) is an ex- tended Helmert transform. We should understand �deformation� in a very weak sense. There is no real deformation of the space with embedded sources. The only deformed �eld is the virtual �eld of velocities, which moves the ob- jects of the catalogue to their positions in another catalogue, in the best way. case of correlated random errors Typically, the Helmert transform is used as the �rst step of a multiple-step procedure of constructing the combined catalogue. Parameters of (9) together form the model of systematic errors between RFi and RFj . Random errors might be estimated as a total residual error after removing of the systematic one. There is some probability that the combined cata- logue will have a lower level of random errors, as compared with the raw ones. Let us de�ne RF0 as a combined catalogue. The classical method of build- ing them from M raw ones postulates that [12]: ~r0 = M∑ i=1 pi~ri M∑ i=1 pi , σ2 0 = 1 M∑ i=1 pi , where ~r0 is the best position, estimated with error σ2 0, pi are weights. To estimate the random errors let us suppose that all numbers in (9) are already determined with Least Squares procedure applied to N shared points of RFi and RF0. It means that now we are able to trans- form all the shared points from RFi to RF0 applying (9) to points coordinates in RFi. It leads us to: ~r (∗) i = [ω × ~ri] + ~ri +~b+ S~ri. (10) 17 Advances in Astronomy and Space Physics V.Ya.Choliy The total residual dispersion is then: σ2 i0 = ∑( ~r (∗) i − ~r0 )2 /N, (11) and it is the mean random error of the RFi and RF0. According to statistics for any two RFi and RFj : σ2 ij = σ2 i + σ2 j − 2ρijσiσj , (12) where σ2 i is the dispersion of random errors of the RFi, and ρij is the correlation of random errors of two RF ′s. There are numerous unknowns in (12) which make the equation system underdetermined. In the case of comparison of M di�erent RF ′s, there are M(M − 1) equations with M(M − 1) unknown cor- relation coe�cients ρij and M unknown σi. The so- lution of these equations is possible only with addi- tional assumptions. To solve (12) one needs to determine the correla- tions ρij in some way. It might be done directly: ρij = ∑( ~ri − ~̂ri )( ~rj − ~̂rj ) σiσj , (13) or by the method proposed in [1], where ρij are the solutions of a linear equation system, built on (RFi−RFj) and (RFi+RFj) dispersions. Here ~r (∗) i are points of RFi after applying systematic correc- tion between RFi and combined RF0. If d2ij is the estimation of the di�erence between the dispersions of the catalogues (RFi −RFj), and s2ij is an estima- tion of the sum of the dispersions of the catalogues (RFi+RFj). For three catalogues [1] gives the linear equations: σ2 1 = (s212 + s213 − s223 − σ2 12 − σ2 13 + σ2 23)/4, σ2 2 = (s223 + s212 − s213 − σ2 23 − σ2 12 + σ2 13)/4, σ2 3 = (s223 + s213 − s212 − σ2 23 − σ2 13 + σ2 12)/4, (14) and ρij = s2ij − d2ij 2σiσj . Yet another solution method of (13) uses the op- timization procedure in the space of ρ′s. For the case of M = 3 let us build a three-dimensional space (~ρ- space) where ρ12, ρ23, ρ31 are coordinates. Then, let us rewrite (12) as a 3-dimensional vector equation: ~f =  σ2 1 + σ2 2 − 2ρ12σ1σ2 − σ2 12 σ2 2 + σ2 3 − 2ρ23σ2σ3 − σ2 23 σ2 3 + σ2 1 − 2ρ31σ3σ1 − σ2 31  = ~0, (15) and proceed with the solution of (15) for σ′s on the lattice of ρ′s in ~ρ-space. Newton method of tangents: ~σnew = ~σold − J−1 ~f(~σold), is fully su�cient with starting value ~σ0 and Jakobi matrix J: ~σ0 = ( σ12 σ23 σ31 ) , J = [ ∂ ~f ∂~σ ] . Unfortunately, the proposed method generates a large number of solutions. For example, if we built a lattice in ~ρ-space with 0.1 step, we will have 213 = 9261 solutions. Since the Newton method is unrestricted, some solutions have negative σi and therefore should be dropped. Other solutions demonstrate known be- haviour: the greater negative ρ′s are, the lower σ′s are as a result. This is why we apply an additional restriction: the solution of (12) in ~ρ−space should be a minimum-length positive component vector ~σ corresponding to the minimum value of ρ′s modules. shifted correlated random errors Let us return to (12) and (10), which are the def- inition of σij . If one estimates Helmert parameters from (11), then calculates σij for transformation RFi to RFj , and then calculates σ2 ji for transformation from RFj to RFi, then one will have σ2 ij 6= σ2 ji and even ρij 6= ρji in general. Our explanation of this fact is that there is an uncompensated systematic error still present in the data (but not accounted with (9)) which distorts and shifts the dispersion estimation (12). If we suppose that the systematic part is not correlated with ran- dom one, we can rewrite (12) in an another form: { σ2 ij = σ2 i + σ2 j + kij − 2ρijσiσj , σ2 ji = σ2 i + σ2 j − kij − 2ρijσiσj , (16) where kij is an additional member, while the dis- persion of a portion of the systematic errors is still present in random residuals. It is thus evident that: kij = ( σ2 ij − σ2 ji ) /2. This term is absolutely arti�cial and its inclusion in (16) still needs mathematical approvement, however its value might serve as goodness-of-�t criteria of the applicability of Helmert transform. 18 Advances in Astronomy and Space Physics V.Ya.Choliy numerical experiment The specially assigned software was created for the purpose of numerical experiments with the Helmert transform. The software builds three ar- ti�cial catalogues consisting of points on the Earth's surface, equally distributed along longitude and lat- itude with 5◦ steps; each catalogue containing 2664 points. Then Gaussian correlated random noise was added to each points in the catalogues. To generate Gaussian random noise values, the following well- known transformation was used: (u1, u2) → → (n1 = u1 √ −2 log s/s, n2 = u2 √ −2 log s/s), where s = u21 + u22, and 0 < s < 1 with u1 and u2 are random values uniformly distributed on [−1, 1]. Before they were applied, the values of (n1, n2) were correlated with one another according to the rule: (n1, n2) → (n1, n1ρ+ n2 √ 1− ρ2) with prede�ned ρ. Generation of uniformly dis- tributed values was conducted with x128() algorithm [5]. After comparison of the catalogues, building the combined one, values of errors and correlations were calculated using three di�erent approaches. These are a) standard formulae (11) and (13); b) linear so- lution from [1]; c) optimization in ~ρ-space. The most interesting for us are values of correla- tions, calculated through di�erent methods. In most cases the correlations according to (14) are 5%�10% less than correlations according to (13). In contrary to this, values of σ do not show any similarities. The following example might show the correla- tion di�erences: (0.261, 0.677, 0.383) from (14) and (0.331, 0.700, 0.442) from (13), whilst sigmas are (7.68, 1.16, 4.79) with (14) correlations and (3.72, 4.72, 0.89) with (13) ones. The most surprising third method, as it can converge to both of the results de- pending of starting conditions. conclusion Extended Helmert transform was used for the comparison of model TRF catalogues, and it was shown that systematic errors are accounted for in a more precise way than with the classical Helmert transform. Can the extended transform be extended once again? We may add spherical functions to the right side of (9), like in many astrometric texts on cata- logue comparison, e. g. [12]. However, as we used throughout the article the analogy between geodesy and stellar astronomy, we can suppose that there is a time to start searching for �tectonic plates� in the sky, like it was done in geodesy years ago. references [1] Bolotin S. L. & Lytvyn S.O. 2010, Kinematika i Fizika Nebesnykh Tel, 26, 1, 31 [2] CholiyV.Ya. 1987, Kinematika i Fizika Nebesnykh Tel, 3, 4, 75 [3] CholiyV.Ya. 2013, BUEOP, 8, 92 [4] CholiyV.Ya. 1989, Kinematika i Fizika Nebesnykh Tel, 5, 2, 7 [5] CholiyV.Ya. 2012, �Numerical methods�, Kyivskyi Uni- versytet, Kyiv [6] MilneE.A. 1935, MNRAS, 95, 560 [7] OgorodnikovK.F. 1958, �Dynamics of the stellar sys- tems�, Fizmatgiz, Moskov [8] Oort J.H. 1927, Bull. Astronomical Institutes of the Netherlands, 3, 120, 275 [9] ParenagoP.P. 1954, �Stellar Astronomy�, TechGiz, Moskov [10] TkachukV.V. & CholiyV.Ya. 2013, Advances in As- tronomy and Space Physics, 3, 141 [11] WatsonG.A. 2006, J. Comput. Appl. Mathem., 197, 387 [12] ZverevM. 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