mirror of
https://github.com/php/presentations.git
synced 2026-03-24 07:32:11 +01:00
75 lines
2.6 KiB
XML
75 lines
2.6 KiB
XML
<?xml version="1.0" encoding="utf-8"?>
|
|
<presentation css="10gen-strict.css">
|
|
<topic>PHP</topic>
|
|
<title>PHP in Space</title>
|
|
<event>PHP UK Conference</event>
|
|
<location>London, UK</location>
|
|
<lat>45.49938</lat><lon>-73.56787</lon>
|
|
<date>February 22nd, 2014</date>
|
|
<speaker>Derick Rethans</speaker>
|
|
<email>derick@derickrethans.nl</email>
|
|
<twitter>derickr</twitter>
|
|
<joindin>http://joind.in/10709</joindin>
|
|
|
|
<slide>slides/map/title.xml</slide>
|
|
<!--
|
|
Jebediah is an astronaut, who wants to go from his house to Eve.
|
|
He lives a while from the space station so he needs to walk there first.
|
|
- Calculate d.x from dms
|
|
- Figure out the distance
|
|
- Calculate initial bearing
|
|
- At the half way point
|
|
- Only in daylight, so we need to know when the sun is up
|
|
- When it rises, is the sun up? earth_sunpos()
|
|
- The first trip is to the Mun, so we need to calculate when it rises
|
|
- Then we need to rocket into the sky. Thrust/Weight
|
|
- Explain delta-v
|
|
- Atmospheric drag
|
|
- Three body system?
|
|
- Mun landing
|
|
- Minmus - plane change
|
|
- Orbit to orbit - hoffman transfer
|
|
- Eve landing
|
|
- Not enough fuel to get off :-(
|
|
-->
|
|
<slide>slides/space/jebediah.xml</slide>
|
|
<slide>slides/space/kerbin.xml</slide>
|
|
<slide>slides/space/kerbin-system.xml</slide>
|
|
<slide>slides/space/mun.xml</slide>
|
|
<slide>slides/space/minmus.xml</slide>
|
|
<slide>slides/space/eve.xml</slide>
|
|
<slide>slides/space/duna.xml</slide>
|
|
|
|
<slide>slides/space/getting-to-ksp.xml</slide>
|
|
<slide>slides/space/extensions.xml</slide>
|
|
<slide>slides/space/dms_to_decimal.xml</slide>
|
|
<slide>slides/space/decimal_to_dms.xml</slide>
|
|
<slide>slides/space/distance.xml</slide>
|
|
<slide>slides/space/distance-vincenty.xml</slide>
|
|
<slide>slides/space/kerbin.xml</slide>
|
|
<slide>slides/space/distance-on-kerbin.xml</slide>
|
|
<slide>slides/space/direction.xml</slide>
|
|
<slide>slides/space/something-about-the-line.xml</slide>
|
|
|
|
<slide>slides/space/kerbals-like-flight-at-day.xml</slide>
|
|
<slide>slides/space/sun-position.xml</slide>
|
|
<slide>slides/space/thrust-to-weight-ratio.xml</slide>
|
|
<slide>slides/space/thrust-to-weight-ratio-calculation.xml</slide>
|
|
<slide>slides/space/thrust-to-weight-max-weight.xml</slide>
|
|
<slide>slides/space/get-it-right.xml</slide>
|
|
|
|
<slide>slides/space/delta-v.xml</slide>
|
|
<slide>slides/space/delta-v-specific-impulse.xml</slide>
|
|
<slide>slides/space/delta-v-specific-calculation.xml</slide>
|
|
|
|
<slide>slides/space/orbital-transfers.xml</slide>
|
|
<slide>slides/space/vis-viva-equation.xml</slide>
|
|
<slide>slides/space/vis-viva-equation-circle.xml</slide>
|
|
|
|
<slide>slides/space/to-duna.xml</slide>
|
|
<slide>slides/space/still-to-do.xml</slide>
|
|
<slide>slides/space/bill-explosion.xml</slide>
|
|
<slide>slides/space/resources.xml</slide>
|
|
|
|
</presentation>
|