Difference between revisions of "Template:OrbitAltitude/Core"
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(Created page with "<includeonly>{{#expr:(({{{1}}}^2 * {{G}} * {{{2}}}/(4 * pi^2)) ^ (1/3)) - {{{3}}}}}</includeonly><noinclude>Calcuates the orbital height without any formatting. {| ! # ! Desc...") |
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| − | <includeonly>{{#expr:(({{{1}}}^2 * {{G}} * {{{2}}}/(4 * pi^2)) ^ (1/3)) - {{{3}}}}}</includeonly><noinclude> | + | <includeonly>{{#expr:(((({{#if: {{{1|}}}{{#if: {{{b|}}}||1}}|{{{1}}}|{{Body data|{{{b}}}|sidrot}}}}{{#if: {{{pf|}}}|*{{{pf}}}}})^2 * {{G}} * {{#if: {{{2|}}}{{#if: {{{b|}}}||1}}|{{{2}}}|{{Body data/Mass|{{{b}}}}}}}/(4 * pi^2)) ^ (1/3)) - {{#if: {{{3|}}}{{#if: {{{b|}}}||1}}|{{#if: {{{3|}}}|{{{3}}}|0}}|{{Body data|{{{b}}}|radius}}}}) {{#switch: {{{f|}}} |
| + | |k=/1000 | ||
| + | |M=/1000000 | ||
| + | |G=/1000000000}}}}</includeonly><noinclude>Calculates the orbital height without any formatting. | ||
| − | {| | + | {{Parameter table|parameters= |
| − | + | {{Parameter row|1|Period of the orbit in seconds}} | |
| − | + | {{Parameter row|2|Mass of central body in kilograms}} | |
| − | | | + | {{Parameter row|3|Radius of central body in meters|0}} |
| − | | | + | {{Parameter row|f|Factor in which the altitude should be shown. Available values: None (m), '''k''' (km), '''M''' (Mm), '''G''' (Gm). If the radius was given kilometers it uses the factor '''k'''.|None}} |
| − | | | + | {{Parameter row|b|Uses the sidereal rotation period, mass and radius as default from the given body. Can be overwritten.|Not set (makes the first three parameters mandatory)}} |
| − | | | + | {{Parameter row|pf|2=Multiplies the period with this value. Useful to easily calculate semi-synchronous orbits (<tt>pf=1/2</tt> then).|3=<tt>1</tt>}} |
| − | | | + | }} |
| − | | | + | |
| − | |- | + | [[Category:Templates]]</noinclude> |
| − | | 3 | ||
| − | |||
| − | |||
Latest revision as of 13:01, 10 May 2018
Calculates the orbital height without any formatting.
| # | Optional | Description | Default |
|---|---|---|---|
| 1 | No | Period of the orbit in seconds | |
| 2 | No | Mass of central body in kilograms | |
| 3 | Yes | Radius of central body in meters | 0 |
| f | Yes | Factor in which the altitude should be shown. Available values: None (m), k (km), M (Mm), G (Gm). If the radius was given kilometers it uses the factor k. | None |
| b | Yes | Uses the sidereal rotation period, mass and radius as default from the given body. Can be overwritten. | Not set (makes the first three parameters mandatory) |
| pf | Yes | Multiplies the period with this value. Useful to easily calculate semi-synchronous orbits (pf=1/2 then). | 1 |
