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Maktabah Reza Ervani

15%

Rp 1.500.000 dari target Rp 10.000.000



Judul Kitab : Principia Mathematica - Detail Buku
Halaman Ke : 206
Jumlah yang dimuat : 585
« Sebelumnya Halaman 206 dari 585 Berikutnya » Daftar Isi
Arabic Original Text
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Bahasa Indonesia Translation

THE MATHEMATICAL PRINCIPLES [BOOK 1 elliptical figure before-mentioned upon two accounts ; first because that force is not directed from P to T ; and, secondly, because it is not recipro cally proportional to the square of the distance PT. These things being premised, it is manifest that the areas are then most nearly proportional to the times, when that third force is the least possible, the rest preserving their former quantity ; and that the orbit PAB does then approach nearest to the elliptical figure above-mentioned, when both the second and third, but especially the third force, is the least possible; the first force remain ing in its former quantity. Let the accelerative attraction of the body T towards S be expressed by the line SN ; then if the accelerative attractions SM and SN were equal, these, attracting the bodies T and P equally and in parallel directions would not at all change their situation with respect to each other. The mo tions of the bodies between themselves would be the same in that case as if those attractions did not act at all, by Cor. 6, of the Laws of Motion. And, by a like reasoning, if the attraction SN is less than the attraction SM, it will take away out of the attraction SM the part SN, so that there will re main only the part (of the attraction) MN to disturb the proportionality of the areas and times, and the elliptical figure of the orbit. And in like manner if the attraction SN be greater than the attraction SM, the pertur bation of the orbit and proportion will be produced by the difference MN alone. After this manner the attraction SN reduces always the attraction SM to the attraction MN, the first and second attractions rema ning per fectly unchanged ; and therefore the areas and times come then nearest to proportionality, and the orbit PAB to the above-mentioned elliptical figure, when the attraction MN is either none, or the least that is possible; that is, when the accelerative attractions of the bodies P and T approach as near as possible to equality ; that is, when the attraction SN is neither none at all, nor less than the least of all the attractions SM, but is, as it were, a mean between the greatest and least of all those attractions SM, that is, not much greater nor much less than the attraction SK. Q.E.D. CASE 2. Let now the lesser bodies P. S, revolve about a greater T in dif ferent planes ; and the force LM, acting in the direction of the line PT situate in the plane of the orbit PAB, will have the same effect as before ; neither will it draw the body P from the plane of its orbit. But the other force NM acting in the direction of a line parallel to ST (and which, there fore, when the body S is without the line of the nodes is inclined to the plane of the orbit PAB), besides the perturbation of the motion just now spoken of as to longitude, introduces another perturbation also as to latitude, attracting the body P out of the plane of its orbit. And this perturbation, in any given situation of the bodies P and T to each other, will be as the generating force MN ; and therefore becomes least when the force MN is least, that is (as was just now shewn), where the attraction SN is not nrirb greater nor much less than the attraction SK. Q.E.D.


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