Search Results
| Search type | Search syntax |
|---|---|
| Tags | [tag] |
| Exact | "words here" |
| Author |
user:1234 user:me (yours) |
| Score |
score:3 (3+) score:0 (none) |
| Answers |
answers:3 (3+) answers:0 (none) isaccepted:yes hasaccepted:no inquestion:1234 |
| Views | views:250 |
| Code | code:"if (foo != bar)" |
| Sections |
title:apples body:"apples oranges" |
| URL | url:"*.example.com" |
| Saves | in:saves |
| Status |
closed:yes duplicate:no migrated:no wiki:no |
| Types |
is:question is:answer |
| Exclude |
-[tag] -apples |
| For more details on advanced search visit our help page | |
Results tagged with orbital-mechanics
Search options not deleted
user 37473
The application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft.
4
votes
1
answer
286
views
How to translate from local laplace plane to ecliptic J2000 (or ICRF)
The NASA JPL websize gives mean orbital elements for e.g. Iapetus or Titan in relation to the local laplace plane.
// Mean orbital elements for Iapetus referred to the local Laplace planes
a(km) e …
- 421