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