GeezerVisonThe World Wide Web, restored to 800 pixels of glory. |
| Home|About|Gaming cabinet|Archives|How it works|Starter sites |
GeezerVison is showing github.com — Tags · RocketPy-Team/RocketPy
Tags
v1.13.0Rel/v1.13.0 (#1080) * Merge pull request #1074 from RocketPy-Team/bug/pre-release-v1.13.0-review-fixes BUG/MNT: pre-release v1.13.0 review fixes * DOC: Update Changelog for PR #1074 * REL: consolidate changelog for v1.13.0 release Fold the #1074 pre-release review fixes into the [v1.13.0] section, reset [Unreleased] to the empty template, and set the release date. Co-Authored-By: Claude Opus 4.8 (1M context) <[email protected]> --------- Co-authored-by: github-actions[bot] <github-actions[bot]@users.noreply.github.com> Co-authored-by: Claude Opus 4.8 (1M context) <[email protected]> v1.12.1HOTFIX: Migrate Forecasts to UCAR THREDDS (#943) * BUG: Fix hard-coded radius value for parachute added mass calculation (#889) * Fix hard-coded radius value for parachute added mass calculation Calculate radius from cd_s using a typical hemispherical parachute drag coefficient (1.4) when radius is not explicitly provided. This fixes drift distance calculations for smaller parachutes like drogues. Formula: R = sqrt(cd_s / (Cd * π)) Closes #860 Co-authored-by: Gui-FernandesBR <[email protected]> Address code review: improve docstrings and add explicit None defaults Co-authored-by: Gui-FernandesBR <[email protected]> Add CHANGELOG entry for PR #889 Co-authored-by: Gui-FernandesBR <[email protected]> Update rocket.add_parachute to use radius=None for consistency Changed the default radius from 1.5 to None in the add_parachute method to match the Parachute class behavior. This ensures consistent automatic radius calculation from cd_s across both APIs. Co-authored-by: Gui-FernandesBR <[email protected]> Refactor Parachute class to remove hard-coded radius value and introduce drag_coefficient parameter for radius estimation Fix hard-coded radius value for parachute added mass calculation Calculate radius from cd_s using a typical hemispherical parachute drag coefficient (1.4) when radius is not explicitly provided. This fixes drift distance calculations for smaller parachutes like drogues. Formula: R = sqrt(cd_s / (Cd * π)) Closes #860 Co-authored-by: Gui-FernandesBR <[email protected]> Add CHANGELOG entry for PR #889 Co-authored-by: Gui-FernandesBR <[email protected]> Refactor Parachute class to remove hard-coded radius value and introduce drag_coefficient parameter for radius estimation MNT: Extract noise initialization to fix pylint too-many-statements in Parachute.__init__ Co-authored-by: Gui-FernandesBR <[email protected]> * Refactor environment method access in controller test for clarity * fix pylint * fix comments * avoid breaking change with drag_coefficient * reafactors Parachute.__init__ method * fix tests --------- Co-authored-by: copilot-swe-agent[bot] <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> * ENH: get changes from BUG: All NOAA NOMADS Dependent Atmosphere Models Broken Fixes #933 * ENH: Add guidelines for simulation safety, Sphinx documentation, and pytest standards (GitHub Copilot) (#937) * REL: bump version to 1.12 * ENH: Add explicit timeouts to ThrustCurve API requests and update changelog (#940) * Initial plan * ENH: Add explicit timeouts to ThrustCurve API requests Co-authored-by: MateusStano <[email protected]> * DOC: Add timeout fix PR to changelog Co-authored-by: MateusStano <[email protected]> --------- Co-authored-by: copilot-swe-agent[bot] <[email protected]> Co-authored-by: MateusStano <[email protected]> * ENH: Restore power_off/on_drag as Function objects; add _input attributes for raw user input and update changelog (#941) * Initial plan * ENH: Restore power_off/on_drag as Function, add _input attributes for raw user input Co-authored-by: MateusStano <[email protected]> * DOC: Add PR #941 compatibility fix to changelog Co-authored-by: MateusStano <[email protected]> * Update rocketpy/rocket/rocket.py Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: ruff pylint --------- Co-authored-by: copilot-swe-agent[bot] <[email protected]> Co-authored-by: MateusStano <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> Co-authored-by: MateusStano <[email protected]> * MNT: Remove unused imports and deprecated functions from mathutils/function.py * BUG: Readd SourceType enumeration for function source types and clean up imports * BUG: Fix incorrect Jacobian in `only_radial_burn` branch of `SolidMotor.evaluate_geometry` (#944) * Initial plan * BUG: Fix incorrect Jacobian in only_radial_burn branch of evaluate_geometry Co-authored-by: MateusStano <[email protected]> --------- Co-authored-by: copilot-swe-agent[bot] <[email protected]> Co-authored-by: MateusStano <[email protected]> * ENH: move weathercocking_coeff to PointMassRockt * MNT: ruff * MNT: fix cyclic import * BUG: Add wraparound logic for wind direction in environment plots (#939) * chore: added personal toolkit files * update branch name in workflow * chore: update toolkit files * Fix: add wraparound logic for wind direction and related tests * style: fix ruff formatting * Remove unused import Co-authored-by: Copilot Autofix powered by AI <[email protected]> * refactor: move repetitive logic into helper method * fix: update test logic in test_environment * add changelog entry --------- Co-authored-by: Copilot Autofix powered by AI <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: add numpy import to test_environment.py * MNT: rename constant for wraparound threshold in _break_direction_wraparound method * ENH: Adaptive Monte Carlo via Convergence Criteria (#922) * ENH: added a new function (simulate_convergence) * DOC: added a cell to show simulate_convergence function usage * TST: integration test for simulate_convergence * DOC: updated changelog for this PR * ENH: ran black to lint intg test file * new fixes thx to copilot comments * linted rocketpy/simulation/monte_carlo.py --------- Co-authored-by: Malmahrouqi3 <[email protected]> * DOC: add latitude range in docs Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: remove unnecessary pylint warning Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: remove unnecessary pylint warning Co-authored-by: Gui-FernandesBR <[email protected]> * DOC: correctly link to WeatherModelMapping Co-authored-by: Copilot <[email protected]> * DOCS: checked todo Co-authored-by: Copilot <[email protected]> * ENH: address copilot comments * TST: improve tests * ENH: get changes from BUG: All NOAA NOMADS Dependent Atmosphere Models Broken Fixes #933 * BUG: Fix hard-coded radius value for parachute added mass calculation (#889) * Fix hard-coded radius value for parachute added mass calculation Calculate radius from cd_s using a typical hemispherical parachute drag coefficient (1.4) when radius is not explicitly provided. This fixes drift distance calculations for smaller parachutes like drogues. Formula: R = sqrt(cd_s / (Cd * π)) Closes #860 Co-authored-by: Gui-FernandesBR <[email protected]> Address code review: improve docstrings and add explicit None defaults Co-authored-by: Gui-FernandesBR <[email protected]> Add CHANGELOG entry for PR #889 Co-authored-by: Gui-FernandesBR <[email protected]> Update rocket.add_parachute to use radius=None for consistency Changed the default radius from 1.5 to None in the add_parachute method to match the Parachute class behavior. This ensures consistent automatic radius calculation from cd_s across both APIs. Co-authored-by: Gui-FernandesBR <[email protected]> Refactor Parachute class to remove hard-coded radius value and introduce drag_coefficient parameter for radius estimation Fix hard-coded radius value for parachute added mass calculation Calculate radius from cd_s using a typical hemispherical parachute drag coefficient (1.4) when radius is not explicitly provided. This fixes drift distance calculations for smaller parachutes like drogues. Formula: R = sqrt(cd_s / (Cd * π)) Closes #860 Co-authored-by: Gui-FernandesBR <[email protected]> Add CHANGELOG entry for PR #889 Co-authored-by: Gui-FernandesBR <[email protected]> Refactor Parachute class to remove hard-coded radius value and introduce drag_coefficient parameter for radius estimation MNT: Extract noise initialization to fix pylint too-many-statements in Parachute.__init__ Co-authored-by: Gui-FernandesBR <[email protected]> * Refactor environment method access in controller test for clarity * fix pylint * fix comments * avoid breaking change with drag_coefficient * reafactors Parachute.__init__ method * fix tests --------- Co-authored-by: copilot-swe-agent[bot] <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> * ENH: Add guidelines for simulation safety, Sphinx documentation, and pytest standards (GitHub Copilot) (#937) * REL: bump version to 1.12 * BUG: Add wraparound logic for wind direction in environment plots (#939) * chore: added personal toolkit files * update branch name in workflow * chore: update toolkit files * Fix: add wraparound logic for wind direction and related tests * style: fix ruff formatting * Remove unused import Co-authored-by: Copilot Autofix powered by AI <[email protected]> * refactor: move repetitive logic into helper method * fix: update test logic in test_environment * add changelog entry --------- Co-authored-by: Copilot Autofix powered by AI <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: add numpy import to test_environment.py * MNT: rename constant for wraparound threshold in _break_direction_wraparound method * DOC: add latitude range in docs Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: remove unnecessary pylint warning Co-authored-by: Gui-FernandesBR <[email protected]> * MNT: remove unnecessary pylint warning Co-authored-by: Gui-FernandesBR <[email protected]> * ENH: address copilot comments * TST: improve tests * DOC: correctly link to WeatherModelMapping Co-authored-by: Copilot <[email protected]> * DOCS: checked todo Co-authored-by: Copilot <[email protected]> * ENH: Adaptive Monte Carlo via Convergence Criteria (#922) * ENH: added a new function (simulate_convergence) * DOC: added a cell to show simulate_convergence function usage * TST: integration test for simulate_convergence * DOC: updated changelog for this PR * ENH: ran black to lint intg test file * new fixes thx to copilot comments * linted rocketpy/simulation/monte_carlo.py --------- Co-authored-by: Malmahrouqi3 <[email protected]> * DEV: remove unwanted changes from develop * DEV: Update for hotfix * TST: add tests * MNT: remove changes from develop again * MNT: Refactor longitude and latitude index functions * MNT: ruff --------- Co-authored-by: Copilot <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> Co-authored-by: Gui-FernandesBR <[email protected]> Co-authored-by: Khushal Kottaru <[email protected]> Co-authored-by: Copilot Autofix powered by AI <[email protected]> Co-authored-by: Mohammed S. Al-Mahrouqi <[email protected]> Co-authored-by: Malmahrouqi3 <[email protected]> PreviousNext
|
| You are visitor 01402503 — GeezerVison does not store the pages you look up. Best viewed with Netscape Navigator 4.7 or Internet Explorer 6 at 800×600. No cookies required. |