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public:fs_astronomie [2023/05/16 17:02] psio |
public:fs_astronomie [2023/05/16 17:14] (current) psio |
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| - | ====== | + | ====== |
| ===== Constants to know from heart ===== | ===== Constants to know from heart ===== | ||
| ^Name ^Equation ^Description ^ | ^Name ^Equation ^Description ^ | ||
| - | |c - Velocity of light |$c = 3 * 10^{8}\frac{m}{s}$ | | | + | |c - Velocity of light |$c = 3 * 10^{8}\frac{m}{s}$ |Velocity of light in vacuum |
| - | |AU - Astronomical Unit |$1 AU = 1,5 * 10^{11}m$ |unit The mean distance from earth to sun | | + | |AU - Astronomical Unit |$1 AU = 1,5 * 10^{11}m$ |The mean distance from earth to sun | |
| |Ly - Lightyear|$1Ly \approx 9,5 * 10^{15}m$ |Distance light travels in one year| | |Ly - Lightyear|$1Ly \approx 9,5 * 10^{15}m$ |Distance light travels in one year| | ||
| |pc - Parsec|$1 pc \approx 3Ly$|One parsec is the dinstance, from wich 1 AU looks like an angle of 1 second| | |pc - Parsec|$1 pc \approx 3Ly$|One parsec is the dinstance, from wich 1 AU looks like an angle of 1 second| | ||
| - | ==== Formulars ==== | + | ===== Formulars |
| - | + | ==== Keplers 3rd Law ==== | |
| - | ^Name ^Formula ^where | + | ^Name ^ Formula |
| - | |Keplers 3rd Law|\begin{align*}a^3 = \frac{GMP^2}{4\pi^2} \end{align*}|\begin{align*} | + | |Keplers 3rd Law |\begin{align*}a^3 = \frac{GMP^2}{4\pi^2} \end{align*} |
| a &= \text{Semi-major axis of elliptical orbit}\\ | a &= \text{Semi-major axis of elliptical orbit}\\ | ||
| G & | G & | ||
| M & | M & | ||
| P & | P & | ||
| - | \end{align*}| | + | \end{align*} |
| - | |Keplers 3rd Law in simplified units|\begin{equation} | + | |Keplers 3rd law in simplified units|\begin{equation} |
| a^3 = P^2M | a^3 = P^2M | ||
| - | \end{equation}|\begin{align*} | + | \end{equation} |\begin{align*} |
| a &= \text{Semi-major axis of elliptical orbit in Units of AU}\\ | a &= \text{Semi-major axis of elliptical orbit in Units of AU}\\ | ||
| M & | M & | ||
| - | P & | + | P & |
| - | \end{align*}|| | + | \end{align*} |
| - | + | |Keplers 3rd law when mass of planet is much smaller than the star $\frac{M}{M_\odot} \approx 1$ | \begin{equation} | |
| - | when mass of planet is much smaller than the star, then $\frac{M}{M_\odot} \approx 1$, so: | + | |
| - | \begin{equation} | + | |
| a^3 = P^2 | a^3 = P^2 | ||
| - | \end{equation} | + | \end{equation} |
| + | a &= \text{Semi-major axis of elliptical orbit in Units of AU}\\ | ||
| + | P & | ||
| + | \end{align*} | ||
| - | \subsection{Small angle formular} | + | ==== Small angle ==== |
| - | \begin{equation} | + | |
| + | |\begin{equation} | ||
| \frac{D2}{D1} = \sin{\alpha} \approx \alpha | \frac{D2}{D1} = \sin{\alpha} \approx \alpha | ||
| - | \end{equation} | + | \end{equation} |
| - | where: | + | |
| - | \begin{align*} | + | |
| \alpha &= \text{viewing angle (for small angles) in rad}\\ | \alpha &= \text{viewing angle (for small angles) in rad}\\ | ||
| D1 & | D1 & | ||
| D2 & | D2 & | ||
| - | \end{align*} | + | \end{align*}| |
| - | + | ||
| - | ^ Formel | + | |
| - | | $\sum_{n=1}^{\infty} \frac{1}{n}$ | + | |
| - | | $\sum_{n=0}^{\infty} n$ | $\infty$ | + | |