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Commit98056ed8a125233f98492152918d9b1678428f9c (patch)
Author
 Syndamia <kamen@syndamia.com>
2025-06-06 08:57:18 +0300
Committer
 Syndamia <kamen@syndamia.com>
2025-06-06 08:57:18 +0300
Files436fc44b04ea69b100fcec3bf148157a8eaa9ea0
uni-projects-main.tar
uni-projects-main.tar.gz
uni-projects-main.zip
Parent57b94ba37adf8289ad47066e25f3e885d276cf92 (diff)
cm: Fix formula for q HEAD main
This fix was done with a pen when my work was returned, so I could get an immediate excellent grade, on 28.05.25
3 files changed, 14 insertions, 14 deletions
-rw-r--r--Year 4/Celestial mechanics/Exercise2.R6
-rw-r--r--Year 4/Celestial mechanics/Project.pdfbin118004 -> 117804 bytes
-rw-r--r--Year 4/Celestial mechanics/Project.tex22
diff --git a/Year 4/Celestial mechanics/Exercise2.R b/Year 4/Celestial mechanics/Exercise2.R
index 7646b28..7d5af5e 100644
--- a/Year 4/Celestial mechanics/Exercise2.R
+++ b/Year 4/Celestial mechanics/Exercise2.R
@@ -102,8 +102,8 @@ poincare2 <- function() {
result <- rbind(
result,
- c(L, sqrt(2*(L-G)) * cos(g + theta), sqrt(2*(G-Theta)) * cos(theta),
- l + g + theta, -sqrt(2*(L-G)) * sin(g + theta), sqrt(2*(G-Theta)) * sin(theta))
+ c(L, sqrt(2*(L-G)) * cos(g + theta), sqrt(2*(G-Theta)) * cos(theta),
+ l + g + theta, -sqrt(2*(L-G)) * sin(g + theta), -sqrt(2*(G-Theta)) * sin(theta))
)
}
@@ -112,4 +112,4 @@ poincare2 <- function() {
p(delaunayAtBirth())
p(poincare1())
-p(poincare2()) \ No newline at end of file
+p(poincare2())
diff --git a/Year 4/Celestial mechanics/Project.pdf b/Year 4/Celestial mechanics/Project.pdf
index 84c62af..649453b 100644
--- a/Year 4/Celestial mechanics/Project.pdf
+++ b/Year 4/Celestial mechanics/Project.pdf
Binary files differ
diff --git a/Year 4/Celestial mechanics/Project.tex b/Year 4/Celestial mechanics/Project.tex
index 62b6faa..1376202 100644
--- a/Year 4/Celestial mechanics/Project.tex
+++ b/Year 4/Celestial mechanics/Project.tex
@@ -631,7 +631,7 @@ poincare1 <- function() {
\begin{align*}
\begin{matrix}
L, & \xi = \sqrt{2(L - G)} \cos(g + \theta), & p = \sqrt{2(G - \Theta)} \cos(\theta), \\
- l + g + \theta, & \eta = - \sqrt{2(L - G)} \sin(g + \theta), & q = \sqrt{2(G - \Theta)} \sin(\theta)
+ l + g + \theta, & \eta = - \sqrt{2(L - G)} \sin(g + \theta), & q = - \sqrt{2(G - \Theta)} \sin(\theta)
\end{matrix}
\end{align*}
@@ -650,8 +650,8 @@ poincare2 <- function() {
result <- rbind(
result,
- c(L, sqrt(2*(L-G)) * cos(g + theta), sqrt(2*(G-Theta)) * cos(theta),
- l + g + theta, -sqrt(2*(L-G)) * sin(g + theta), sqrt(2*(G-Theta)) * sin(theta))
+ c(L, sqrt(2*(L-G)) * cos(g + theta), sqrt(2*(G-Theta)) * cos(theta),
+ l + g + theta, -sqrt(2*(L-G)) * sin(g + theta), -sqrt(2*(G-Theta)) * sin(theta))
)
}
@@ -773,14 +773,14 @@ Neptune & 0.000282474574098807182 & 0.000102183215085003621 & -0.00034595077044
\begin{tabular}{c|c|c|c}
Поанкаре 2 вид & $l + g + \theta$ & $\eta$ & $q$ \\
\hline\hline
-Mercury & 64.935104730684670926166 & -0.000064860017692109048 & 0.000029016152403852770 \\
-Venus & 26.874312304520689309584 & -0.000007310622668714660 & 0.000083171755027473018 \\
-EM Bary & 16.332237622190888259865 & -0.000028397780808021289 & 0.000000000000000000000 \\
-Mars & 7.671847350991824576738 & 0.000023939472880300536 & 0.000015469785726697444 \\
-Jupiter & 1.829323592481375992946 & -0.000574271300256992776 & 0.001043799184507826754 \\
-Saturn & 1.366943839440607932900 & -0.001598872025701959104 & 0.001179865410141265995 \\
-Uranus & 5.640560234109244674983 & -0.000102673689729541247 & 0.000179171552127487335 \\
-Neptune & -0.873555660858104765509 & -0.000102030956457410801 & 0.000387140939560313784 \\
+Mercury & 64.935104730684670926166 & -0.000064860017692109048 & -0.000029016152403852770 \\
+Venus & 26.874312304520689309584 & -0.000007310622668714660 & -0.000083171755027473018 \\
+EM Bary & 16.332237622190888259865 & -0.000028397780808021289 & -0.000000000000000000000 \\
+Mars & 7.671847350991824576738 & 0.000023939472880300536 & -0.000015469785726697444 \\
+Jupiter & 1.829323592481375992946 & -0.000574271300256992776 & -0.001043799184507826754 \\
+Saturn & 1.366943839440607932900 & -0.001598872025701959104 & -0.001179865410141265995 \\
+Uranus & 5.640560234109244674983 & -0.000102673689729541247 & -0.000179171552127487335 \\
+Neptune & -0.873555660858104765509 & -0.000102030956457410801 & -0.000387140939560313784 \\
\end{tabular}
\end{center}
\end{table}