Add Kepler and Encke orbit propagation method #79
Conversation
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
1 task
suzuki-toshihir0
approved these changes
Apr 11, 2022
Sign up for free
to join this conversation on GitHub.
Already have an account?
Sign in to comment
Add this suggestion to a batch that can be applied as a single commit.
This suggestion is invalid because no changes were made to the code.
Suggestions cannot be applied while the pull request is closed.
Suggestions cannot be applied while viewing a subset of changes.
Only one suggestion per line can be applied in a batch.
Add this suggestion to a batch that can be applied as a single commit.
Applying suggestions on deleted lines is not supported.
You must change the existing code in this line in order to create a valid suggestion.
Outdated suggestions cannot be applied.
This suggestion has been applied or marked resolved.
Suggestions cannot be applied from pending reviews.
Suggestions cannot be applied on multi-line comments.
Suggestions cannot be applied while the pull request is queued to merge.
Suggestion cannot be applied right now. Please check back later.
Overview
Add Kepler and Encke orbit propagation method
Issue
Details
Kepler orbit propagation for pure two-body problem is newly implemented. I believe it is easier to use and faster than other methods.
Encke's orbit propagation method is also newly implemented. It is more accurate than the normal RK4 method and it can be apply for relative orbit propagation.
I also fixed some issues in the
Orbitclass like #23.Validation results
It will be write in the
s2e-documentsoon.Scope of influence
Huge. Users need to update their ini file to suit with the #23.
Supplement
NA
Note
NA