Skip to content
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

Edit typo #129

Merged
merged 1 commit into from
Sep 14, 2023
Merged
Show file tree
Hide file tree
Changes from all commits
Commits
File filter

Filter by extension

Filter by extension

Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
4 changes: 2 additions & 2 deletions README.rst
Original file line number Diff line number Diff line change
Expand Up @@ -90,7 +90,7 @@ Currently you have available these sources
How to contribute
-----------------

- Write pep8 complaint code.
- Wrap the code on 100 collumns.
- Write pep8 compliant code.
- Wrap the code on 100 columns.
- Always use a branch for each feature and Merge Proposals.
- Always run the tests before to push. (test implies pep8 validation)
2 changes: 1 addition & 1 deletion orbit_predictor/utils.py
Original file line number Diff line number Diff line change
Expand Up @@ -402,7 +402,7 @@ def get_satellite_minus_penumbra_verticals(r, when_utc, r_p=R_E_MEAN_KM):
The zeros of the function are only in the transitions from illuminated to
penumbra (when going from positive to negative)
and from penumbra to illuminated (when going from negative to positive).
BEWARE: it can have local minimuns with positive values.
BEWARE: it can have local minimums with positive values.
Works for highly elliptical orbits too.
The internals are the same as shadow function based on
Algorithm 34 from Vallado, section 5.3.
Expand Down
Loading