Difference between revisions of "User:Urwumpe"

Revision as of 20:17, 24 September 2006

OrbiterWiki administrator since december 2005

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

$P$	Orbit parameter, $p=a\cdot (1-\epsilon ^{2})$
$u$	corrected true anomaly, $u=\omega +\varphi$
$R_{E}$	mean planetary radius
$J_{2}$	non spherical gravity term
$i$	inclination
$\omega$	Argument of perigee
$\epsilon$	eccentricity

${\frac {d\Omega }{du}}=-3\cdot J_{2}\cdot ({\frac {R_{E}}{p}})\cdot \sin ^{2}{u}\cdot \cos {i}\cdot [1+\epsilon \cdot \cos u-\omega ]$

@@ Line 11: / Line 11: @@
 N-Mail: Urwumpe(ät)Yahoo(döt)com
-==Stuff==
+==Math formulas==
-РАЭРЕШ РАЭАРРИТ
+===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==