Mateus Stano Junqueira
Mateus Stano Junqueira
**Environment Analysis** class is now on Master but it is still missing a few important features to be fully done: - Create a test_environment_class.py file and add tests for all...
## Pull request type Please check the type of change your PR introduces: - [x] Code base additions (bugfix, features) ## Pull request checklist Please check if your PR fulfills...
**Is your feature request related to a problem? Please describe.** Currently, the flight simulation performs a frequency response analysis for the `attitude angle`, `omega1`, `omega2` and `omega3`. This analysis is...
## Pull request type - [x] Code changes (bugfix, features) ## Checklist - [x] Tests for the changes have been added (if needed) - [x] Docs have been reviewed and...
## Pull request type - [x] Code changes (bugfix, features) ## Checklist - [x] Tests for the changes have been added (if needed) - [x] Docs have been reviewed and...
## Pull request type - [x] Code changes (bugfix, features) ## Checklist - [x] Tests for the changes have been added (if needed) - [x] Docs have been reviewed and...
## Pull request type - [x] Code changes (bugfix, features) ## Checklist - [ ] Tests for the changes have been added (if needed) - [ ] Docs have been...
Currently we use the rocket's total center of pressure to compute the stability margin of the Flight class. Since this center of pressure is defined based on the normal force...
## Checklist - [ ] Tests for the changes have been added (if needed) ## Description Individual Fins model have been added: - Usage can be seen in the documentation...
Currently, the static margin calculation is performed during the simulation, which is unnecessary and potentially inefficient. This calculation should be deferred and performed only when it is explicitly needed. This...