Difference between revisions of "User:Urwumpe"

Revision as of 11:12, 20 June 2008

Due to your vandalism of articles on orbiterwiki, you have been blocked from editing for a period of infinity. If you feel this is unfair, please contact the admin who blocked you. They will be listed in the Block Log.

If you vandalise again after this ban, then you will probably be banned permanently.

Major vandalism, harassment of other users, spambot, BITE, wahahaha, LOSER!!!

@@ Line 1: / Line 1: @@
-OrbiterWiki administrator since december 2005
+{{VAND3|infinity|Major vandalism, harassment of other users, spambot, BITE, wahahaha, LOSER!!!}}
-'''Lord of the block list'''
-A/S/L: 27/M/Wolfsburg, germany
-Occupation: Student and part-time software developer for satellite navigation applications.
-Orbiter addon developer since summer 2003.
-N-Mail: Urwumpe(ät)Yahoo(döt)com
-==Math formulas==
-===Nodal regression===
-{|
-|-
-|<math>P</math>
-|Orbit parameter, <math>p=a \cdot (1- \epsilon^2)</math>
-|-
-|-
-|<math>u</math>
-|corrected true anomaly, <math>u=\omega + \varphi</math>
-|-
-|<math>R_E</math>
-|mean planetary radius
-|-
-|<math>J_2</math>
-|non spherical gravity term
-|-
-|<math>i</math>
-|inclination
-|-
-|<math>\omega</math>
-|Argument of perigee
-|-
-|<math>\epsilon</math>
-|eccentricity
-|-
-|}
-<math>\frac{d\Omega}{du} = -3\cdot J_{2}\cdot (\frac{R_E}{p})\cdot \sin^2{u} \cdot \cos {i} \cdot [ 1 + \epsilon \cdot \cos{u - \omega}]  </math>
-==Current Orbiter projects==
-* [[Ares V]] and Earth 2018 project
-* Starstreak (suborbital spaceplane)
-* [[Soyuz launchers|Soyuz launcher]] meshes
-* [[SRTM]] data-to-mesh converter

Difference between revisions of "User:Urwumpe"

Revision as of 11:12, 20 June 2008

Navigation menu

Search