Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba
Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba
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In our eReader you can find the full English version of the book. Read Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba Online - link to read the book on full screen. Our eReader also allows you to upload and read Pdf, Txt, ePub and fb2 books. In the Mini eReder on the page below you can quickly view all pages of the book - Read Book Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba
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111. IV. V. VI. X 40. 668778 +0. 6697OO +0. 669871 4-0. 668780 +0. 669562 +0, 669853 a Y* -0. 565036 -0. 564561 *0. 564782 -0. 365000 -0. 564584 -0. 564489 Z +0. 125224 +0. 125908 +0. 125589 +0. 125217 +O. 125793 +0. 125997 X^ +0. 446200 +0. 443864 +0. 445037 +0. 446198 -0. 443721 +0. 443432 Y' +0. 347541 +0. 347166 +0. 347367 +0. 347548 +0. 347165 +0. 347085 Zl +1. 393368 +1. 393785 +1. 393542 +1. 393387 +1. 393897 +1. 393841 The following comparison* are of particular interest.
VI -V VI -IV 1...-1V X, + 291 + 1073 - 2 Y^ + 101 +517 +36 2 +204 +760 +7 X ' -289 - 276S + 2 . - T' - 85 - 463 - i 2' + 216 + 454 - 19 The differences between Orbit IV and Orbit vl show that Orbit IV is correct only to two places. In the comparison of Orbit 1 and Orbit IV where the parallax is entirely neglected the differences are so small and at the same tine are within the errors of computation that it is quits evident that the partial elimination has no decided effect upon the orbit.
The differences between Orbit V and Vl where parallax - 13 is completely eliminated show that Orbit VI is correct to three places.
What to read after Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba?
You can find similar books in the "Read Also" column, or choose other free books by Sarah De Camp Morgan to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
111. IV. V. VI. X 40. 668778 +0. 6697OO +0. 669871 4-0. 668780 +0. 669562 +0, 669853 a Y* -0. 565036 -0. 564561 *0. 564782 -0. 365000 -0. 564584 -0. 564489 Z +0. 125224 +0. 125908 +0. 125589 +0. 125217 +O. 125793 +0. 125997 X^ +0. 446200 +0. 443864 +0. 445037 +0. 446198 -0. 443721 +0. 443432 Y' +0. 347541 +0. 347166 +0. 347367 +0. 347548 +0. 347165 +0. 347085 Zl +1. 393368 +1. 393785 +1. 393542 +1. 393387 +1. 393897 +1. 393841 The following comparison* are of particular interest.
VI -V VI -IV 1...-1V X, + 291 + 1073 - 2 Y^ + 101 +517 +36 2 +204 +760 +7 X ' -289 - 276S + 2 . - T' - 85 - 463 - i 2' + 216 + 454 - 19 The differences between Orbit IV and Orbit vl show that Orbit IV is correct only to two places. In the comparison of Orbit 1 and Orbit IV where the parallax is entirely neglected the differences are so small and at the same tine are within the errors of computation that it is quits evident that the partial elimination has no decided effect upon the orbit.
The differences between Orbit V and Vl where parallax - 13 is completely eliminated show that Orbit VI is correct to three places.
What to read after Numerical Investigation of the Formulae for the Elimination of Geocentric And Ba?
You can find similar books in the "Read Also" column, or choose other free books by Sarah De Camp Morgan to read onlineMoreLess
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