Merge pull request #550 from RocketPy-Team/mnt/small-fixes-before-v1.2

MNT: small fixes before v1.2

Author: Gui-FernandesBR

.github/pull_request_template.md

@@ -16,7 +16,7 @@
 - [ ] Tests for the changes have been added (if needed)
 - [ ] Docs have been reviewed and added / updated
 - [ ] Lint (`black rocketpy/ tests/`) has passed locally 
-- [ ] All tests (`python3 -m pytest tests -m slow --runslow`) have passed locally
+- [ ] All tests (`pytest tests -m slow --runslow`) have passed locally
 - [ ] `CHANGELOG.md` has been updated (if relevant)
 
 ## Current behavior

.github/workflows/test_pytest.yaml

@@ -57,10 +57,6 @@ jobs:
       - name: Run Acceptance Tests
         run: pytest tests/acceptance --cov=rocketpy --cov-append --cov-report=xml
 
-      - name: Run pytest --runslow
-        if: github.ref == 'refs/heads/master'
-        run: pytest tests -m slow --runslow --cov=rocketpy --cov-append --cov-report=xml
-
       - name: Upload coverage to artifacts
         uses: actions/upload-artifact@v2
         with:

.pylintrc

@@ -188,6 +188,30 @@ function-naming-style=snake_case
 good-names=FlightPhases,
            WindroseAxes,
            barometric_height_ISA,
+           grain_I_33_initial,
+           convert_units_Functions,
+           Ix_volume,
+           Iy_volume,
+           Iz_volume,
+           Kn,
+           Kn_source,
+           I_dot,
+           I_CM,
+           Rdot,
+           Dx,
+           Dy,
+           Dz,
+           requires_netCDF4,
+           I_11_without_motor,
+           I_22_without_motor,
+           I_33_without_motor,
+           I_12_without_motor,
+           I_13_without_motor,
+           I_23_without_motor,
+           HTML,
+           fin_set_NACA,
+           fin_set_E473,
+           HIRESW_dictionary,
 
 
 # Good variable names regexes, separated by a comma. If names match any regex,

CHANGELOG.md

@@ -27,34 +27,55 @@ and this project adheres to [Semantic Versioning](http://semver.org/).
 
 ## [Unreleased] - yyyy-mm-dd
 
-Here we write upgrading notes for brands. It's a team effort to make them as
-straightforward as possible.
+<!-- These are the changes that were not release yet, please add them correctly.
+  Attention: The newest changes should be on top -->
+
+### Added
+
+
+### Changed
+
+
+### Fixed
+
+
+## [v1.2.0] - 2024-02-dd
+
+You can install this version by running `pip install rocketpy==1.2.0`
 
 ### Added
 
 - ENH: Function Support for CSV Header Inputs [#542](https://github.com/RocketPy-Team/RocketPy/pull/542)
+- ENH: Argument for Optional Mutation on Function Discretize [#519](https://github.com/RocketPy-Team/RocketPy/pull/519)
+- ENH: Add of a line for saving the filtered dataset [#518](https://github.com/RocketPy-Team/RocketPy/pull/518)
 - ENH: Shepard Optimized Interpolation - Multiple Inputs Support [#515](https://github.com/RocketPy-Team/RocketPy/pull/515)
 - ENH: adds new Function.savetxt method [#514](https://github.com/RocketPy-Team/RocketPy/pull/514)
-- ENH: Argument for Optional Mutation on Function Discretize [#519](https://github.com/RocketPy-Team/RocketPy/pull/519)
--  ENH: Air Brakes [#426](https://github.com/RocketPy-Team/RocketPy/pull/426)
+- DOC: add juno3 flight example [#513](https://github.com/RocketPy-Team/RocketPy/pull/513)
+- ENH: add Function.low_pass_filter method [#508](https://github.com/RocketPy-Team/RocketPy/pull/508)
+- ENH: Air Brakes [#426](https://github.com/RocketPy-Team/RocketPy/pull/426)
+- 
 
 ### Changed
 
-- MNT: Add repr method to Parachute class [#490](https://github.com/RocketPy-Team/RocketPy/pull/490)
-- ENH: Function Reverse Arithmetic Priority [#488](https://github.com/RocketPy-Team/RocketPy/pull/488)
-- DOC: Update Header Related Docs
-- ENH Precalculate Barometric Height [#511](https://github.com/RocketPy-Team/RocketPy/pull/511)
-- MNT: Encapsulate quaternion conversions [#537](https://github.com/RocketPy-Team/RocketPy/pull/537)
-- MNT: improve the low pass filter and document an example [#538](https://github.com/RocketPy-Team/RocketPy/pull/538)
 - ENH: Plotting both power on and off drag curves in a single plot [#547](https://github.com/RocketPy-Team/RocketPy/pull/547)
-- BUG: Elliptical Fins Draw [#548](https://github.com/RocketPy-Team/RocketPy/pull/548)
+- DOC: Replacing git clone command with curl in notebooks. [#544](https://github.com/RocketPy-Team/RocketPy/pull/544)
+- DOC: Installing imageio library on dispersion analysis notebook [#540](https://github.com/RocketPy-Team/RocketPy/pull/540)
+- MNT: improve the low pass filter and document an example [#538](https://github.com/RocketPy-Team/RocketPy/pull/538)
+- MNT: Encapsulate quaternion conversions [#537](https://github.com/RocketPy-Team/RocketPy/pull/537)
+- ENH: Precalculate Barometric Height [#511](https://github.com/RocketPy-Team/RocketPy/pull/511)
+- ENH: optimize get_value_opt in class Function [#501](https://github.com/RocketPy-Team/RocketPy/pull/501)
+- DOC: Update Header Related Docs [#495](https://github.com/RocketPy-Team/RocketPy/pull/495)
+- ENH: Function Reverse Arithmetic Priority [#488](https://github.com/RocketPy-Team/RocketPy/pull/488)
+- MNT: Add repr method to Parachute class [#490](https://github.com/RocketPy-Team/RocketPy/pull/490)
 
 ### Fixed
 
-- ENH: Parachute trigger doesn't work if "Apogee" is used instead of "apogee" [#489](https://github.com/RocketPy-Team/RocketPy/pull/489)
-- BUG: fin_flutter_analysis doesn't find any fin set [#510](https://github.com/RocketPy-Team/RocketPy/pull/510)
-- FIX: EmptyMotor is breaking the Rocket.draw() method [#516](https://github.com/RocketPy-Team/RocketPy/pull/516)
+- MNT: small fixes before v1.2 [#550](https://github.com/RocketPy-Team/RocketPy/pull/550)
+- BUG: Elliptical Fins Draw [#548](https://github.com/RocketPy-Team/RocketPy/pull/548)
 - BUG: 3D trajectory plot not labeling axes [#533](https://github.com/RocketPy-Team/RocketPy/pull/533)
+- FIX: EmptyMotor is breaking the Rocket.draw() method [#516](https://github.com/RocketPy-Team/RocketPy/pull/516)
+- BUG: fin_flutter_analysis doesn't find any fin set [#510](https://github.com/RocketPy-Team/RocketPy/pull/510)
+- ENH: Parachute trigger doesn't work if "Apogee" is used instead of "apogee" [#489](https://github.com/RocketPy-Team/RocketPy/pull/489)
 
 
 ## [v1.1.5] - 2024-01-21
@@ -66,80 +87,90 @@ You can install this version by running `pip install rocketpy==1.1.5`
 - BUG: Parachute Pressures not being Set before All Info. [#534](https://github.com/RocketPy-Team/RocketPy/pull/534)
 - BUG: Invalid Arguments on Two Dimensional Discretize. [#521](https://github.com/RocketPy-Team/RocketPy/pull/521)
 
-## [v1.1.4] - 2023-12-07
+## [v1.1.4] - 2023-12-09
 
 You can install this version by running `pip install rocketpy==1.1.4`
 
 ### Fixed
 
-- DOC: Change from % to ! in the first cell to run properly in Colab. [#496](https://github.com/RocketPy-Team/RocketPy/pull/496)
 - FIX: changes Generic Motor exhaust velocity to cached property [#497](https://github.com/RocketPy-Team/RocketPy/pull/497)
+- DOC: Change from % to ! in the first cell to run properly in Colab. [#496](https://github.com/RocketPy-Team/RocketPy/pull/496)
 
-## [v1.1.3] - 2023-11-30
+## [v1.1.3] - 2023-11-29
 
 You can install this version by running `pip install rocketpy==1.1.3`
 
 ### Fixed
 
-- FIX: Broken Function.get_value_opt for N-Dimensional Functions [#492](https://github.com/RocketPy-Team/RocketPy/pull/492)
 - FIX: Never ending Flight simulations when using a GenericMotor [#497](https://github.com/RocketPy-Team/RocketPy/pull/497)
+- FIX: Broken Function.get_value_opt for N-Dimensional Functions [#492](https://github.com/RocketPy-Team/RocketPy/pull/492)
 
-## [v1.1.2] - 2023-11-25
+## [v1.1.2] - 2023-11-27
 
 You can install this version by running `pip install rocketpy==1.1.2`
 
 ### Fixed
 
 - BUG: Function breaks if a header is present in the csv file [#485](https://github.com/RocketPy-Team/RocketPy/pull/485)
 
-## [v1.1.1] - 2023-11-23
+## [v1.1.1] - 2023-11-24
 
 You can install this version by running `pip install rocketpy==1.1.1`
 
 ### Added
 
-- DOC: Added this changelog file [#472](https://github.com/RocketPy-Team/RocketPy/pull/472)
 - ENH: Prevent out of bounds Tanks from Instantiation #484 [#484](https://github.com/RocketPy-Team/RocketPy/pull/484)
+- DOC: Added this changelog file [#472](https://github.com/RocketPy-Team/RocketPy/pull/472)
 
 ### Fixed
 
-- HOTFIX: Negative Static Margin [#476](https://github.com/RocketPy-Team/RocketPy/pull/476)
-- HOTFIX: 2D .CSV Function and missing set_get_value_opt call [#478](https://github.com/RocketPy-Team/RocketPy/pull/478)
 - HOTFIX: Tanks Overfill not Being Detected [#479](https://github.com/RocketPy-Team/RocketPy/pull/479)
+- HOTFIX: 2D .CSV Function and missing set_get_value_opt call [#478](https://github.com/RocketPy-Team/RocketPy/pull/478)
+- HOTFIX: Negative Static Margin [#476](https://github.com/RocketPy-Team/RocketPy/pull/476)
 
 ## [v1.1.0] - 2023-11-19
 
 You can install this version by running `pip install rocketpy==1.1.0`
 
 ### Added
 
-- DOC: Documentation for Function Class Usage [#465](https://github.com/RocketPy-Team/RocketPy/pull/465)
 - DOC: first simulation all_info [#466](https://github.com/RocketPy-Team/RocketPy/pull/466)
-- ENH: draw motors [#436](https://github.com/RocketPy-Team/RocketPy/pull/436)
+- DOC: Documentation for Function Class Usage [#465](https://github.com/RocketPy-Team/RocketPy/pull/465)
 - DOC: add documentation for flight data export. [#464](https://github.com/RocketPy-Team/RocketPy/pull/464)
 - ENH: Add mass_flow_rate() to GenericMotor class [#459](https://github.com/RocketPy-Team/RocketPy/pull/459)
 - DOC: Add documentation on how to build the docs [#452](https://github.com/RocketPy-Team/RocketPy/pull/452)
+- ENH: draw motors [#436](https://github.com/RocketPy-Team/RocketPy/pull/436)
 - ENH: new Flight.get_solution_at_time() method [#441](https://github.com/RocketPy-Team/RocketPy/pull/441)
 - ENH: rocket drawing [419](https://github.com/RocketPy-Team/RocketPy/pull/419)
 - ENH: Adding Stability Margin with Mach dependency [#377](https://github.com/RocketPy-Team/RocketPy/pull/377)
 
 ### Changed
 
-- ENH: Spherical Caps Included in Total Length [#455](https://github.com/RocketPy-Team/RocketPy/pull/455)
-  - Important: This changes behavior of `TankGeometry.add_spherical_caps()`
 - ENH: Clean Plots and Prints sub packages init files [#457](https://github.com/RocketPy-Team/RocketPy/pull/457)
 - ENH: Add \_MotorPlots Inheritance to Motor Plots Classes [#456](https://github.com/RocketPy-Team/RocketPy/pull/456)
-- DOC: organize flight examples folder [#429](https://github.com/RocketPy-Team/RocketPy/pull/429)
+- ENH: Spherical Caps Included in Total Length [#455](https://github.com/RocketPy-Team/RocketPy/pull/455)
+  - Important: This changes behavior of `TankGeometry.add_spherical_caps()`
 - DOC: improve mass and inertia docs [#445](https://github.com/RocketPy-Team/RocketPy/pull/445)
+- DOC: organize flight examples folder [#429](https://github.com/RocketPy-Team/RocketPy/pull/429)
 
 ### Fixed
 
-- MNT: Refactor exhaust velocity calculation to avoid ZeroDivisionError [#470](https://github.com/RocketPy-Team/RocketPy/pull/470)
 - BUG: Fix find_input() Function to Return a Single Value [#471](https://github.com/RocketPy-Team/RocketPy/pull/471)
+- MNT: Refactor exhaust velocity calculation to avoid ZeroDivisionError [#470](https://github.com/RocketPy-Team/RocketPy/pull/470)
 - DOC: refactor dispersion analysis notebook [#463](https://github.com/RocketPy-Team/RocketPy/pull/463)
+- DOC: fix positions and coordinate system documentation page [#454](https://github.com/RocketPy-Team/RocketPy/pull/454)
 - BUG: User input checks added for Function class [#451](https://github.com/RocketPy-Team/RocketPy/pull/451)
-- DOC: fix positions and coordinate system documentation page [#454](https://github.com/RocketPy-Team/RocketPy/pull/)
 - MNT: fix env plots legends [#440](https://github.com/RocketPy-Team/RocketPy/pull/440)
 - BUG: flight.prints.max_values() fails when launching an EmptyMotor [#438](https://github.com/RocketPy-Team/RocketPy/pull/438)
-- BUG: Maintaining Extrapolation when Adding Discrete Functions with Constants [#432](https://github.com/RocketPy-Team/RocketPy/pull/432)
 - MNT: Fix env plots max heights [#433](https://github.com/RocketPy-Team/RocketPy/pull/433)
+- BUG: Maintaining Extrapolation when Adding Discrete Functions with Constants [#432](https://github.com/RocketPy-Team/RocketPy/pull/432)
+
+
+# [v1.0.1] - 2023-10-07
+
+You can install this version by running `pip install rocketpy==1.0.1`
+
+### Fixed
+
+- BUG: Remove NoseCone Warning [#428](https://github.com/RocketPy-Team/RocketPy/pull/428)
+- BUG: motor coordinates [#423](https://github.com/RocketPy-Team/RocketPy/pull/423)

docs/examples/ndrt_2020_flight_sim.ipynb

@@ -81,7 +81,7 @@
    "source": [
     "parameters = {\n",
     "    # Mass Details\n",
-    "    \"rocket_mass\": (18.998, 0.010), # Rocket dry mass: 20.846 kg\n",
+    "    \"rocket_mass\": (18.998, 0.010),  # Rocket dry mass: 20.846 kg\n",
     "    # propulsion details\n",
     "    \"motor_structure_mass\": (1.848, 0.1),\n",
     "    \"burn_time\": (3.433, 0.1),\n",
@@ -222,7 +222,7 @@
     "    throat_radius=parameters.get(\"throat_radius\")[0],\n",
     "    interpolation_method=\"linear\",\n",
     "    nozzle_position=parameters.get(\"nozzle_position\")[0],\n",
-    "    coordinate_system_orientation=\"combustion_chamber_to_nozzle\" #combustion_chamber_to_nozzle\"\n",
+    "    coordinate_system_orientation=\"combustion_chamber_to_nozzle\",  # combustion_chamber_to_nozzle\"\n",
     ")"
    ]
   },
@@ -329,9 +329,7 @@
     ")\n",
     "ndrt2020.set_rail_buttons(1.5, 2, 45)\n",
     "\n",
-    "ndrt2020.add_motor(\n",
-    "    motor=motor_l1395, position=parameters.get(\"motor_position\")[0]\n",
-    ")"
+    "ndrt2020.add_motor(motor=motor_l1395, position=parameters.get(\"motor_position\")[0])"
    ]
   },
   {
@@ -358,7 +356,7 @@
     "nose_cone = ndrt2020.add_nose(\n",
     "    length=parameters.get(\"nose_length\")[0],\n",
     "    kind=\"tangent\",\n",
-    "    position=parameters.get(\"nose_position\")[0]\n",
+    "    position=parameters.get(\"nose_position\")[0],\n",
     ")\n",
     "fin_set = ndrt2020.add_trapezoidal_fins(\n",
     "    4,\n",
@@ -700,7 +698,7 @@
     "    outputs=\"Altitude above ground level (m)\",\n",
     "    interpolation=\"linear\",\n",
     "    extrapolation=\"zero\",\n",
-    ") # the division by 3.281 is to convert from feet to meters"
+    ")  # the division by 3.281 is to convert from feet to meters"
    ]
   },
   {
@@ -740,7 +738,7 @@
    ],
    "source": [
     "Function.compare_plots(\n",
-    "    plot_list=[(actual_vz, \"Actual\"),(actual_vz_filtered, \"Filtered\")],\n",
+    "    plot_list=[(actual_vz, \"Actual\"), (actual_vz_filtered, \"Filtered\")],\n",
     "    ylabel=\"Vertical velocity (m/s)\",\n",
     "    title=\"Vertical velocity\",\n",
     "    xlabel=\"Time (s)\",\n",
@@ -785,11 +783,11 @@
    ],
    "source": [
     "Function.compare_plots(\n",
-    "    plot_list=[(actual_az, \"Actual\"),(actual_az_filtered, \"Filtered\")],\n",
+    "    plot_list=[(actual_az, \"Actual\"), (actual_az_filtered, \"Filtered\")],\n",
     "    ylabel=\"Vertical acceleration (m/s^2)\",\n",
     "    title=\"Vertical acceleration\",\n",
     "    xlabel=\"Time (s)\",\n",
-    ")\n"
+    ")"
    ]
   },
   {

docs/notebooks/air_brakes_example.ipynb

@@ -204,14 +204,14 @@
     "    altitude_ASL = state[2]\n",
     "    altitude_AGL = altitude_ASL - env.elevation\n",
     "    vx, vy, vz = state[3], state[4], state[5]\n",
-    "    \n",
+    "\n",
     "    # Get winds in x and y directions\n",
-    "    wind_x, wind_y = env.wind_velocity_x(altitude_ASL), env.wind_velocity_y(altitude_ASL)\n",
-    "    \n",
+    "    wind_x, wind_y = env.wind_velocity_x(altitude_ASL), env.wind_velocity_y(\n",
+    "        altitude_ASL\n",
+    "    )\n",
+    "\n",
     "    # Calculate Mach number\n",
-    "    free_stream_speed = (\n",
-    "        (wind_x - vx) ** 2 + (wind_y - vy) ** 2 + (vz) ** 2\n",
-    "    ) ** 0.5\n",
+    "    free_stream_speed = ((wind_x - vx) ** 2 + (wind_y - vy) ** 2 + (vz) ** 2) ** 0.5\n",
     "    mach_number = free_stream_speed / env.speed_of_sound(altitude_ASL)\n",
     "\n",
     "    # Get previous state from state_history\n",

docs/notebooks/compare_flights_usage.ipynb

@@ -72,7 +72,7 @@
     "env = Environment(latitude=-23, longitude=-49, date=after_tomorrow)\n",
     "env.set_atmospheric_model(type=\"Forecast\", file=\"GFS\")\n",
     "\n",
-    "Pro75M1670 =  SolidMotor(\n",
+    "Pro75M1670 = SolidMotor(\n",
     "    thrust_source=\"../../data/motors/Cesaroni_M1670.eng\",\n",
     "    dry_mass=1.815,\n",
     "    dry_inertia=(0.125, 0.125, 0.002),\n",
@@ -109,9 +109,7 @@
     "\n",
     "calisto.add_motor(Pro75M1670, position=-1.255)\n",
     "\n",
-    "nosecone = calisto.add_nose(\n",
-    "    length=0.55829, kind=\"vonKarman\", position=1.278\n",
-    ")\n",
+    "nosecone = calisto.add_nose(length=0.55829, kind=\"vonKarman\", position=1.278)\n",
     "\n",
     "fin_set = calisto.add_trapezoidal_fins(\n",
     "    n=4,\n",
@@ -120,7 +118,7 @@
     "    span=0.110,\n",
     "    position=-1.04956,\n",
     "    cant_angle=0.5,\n",
-    "    airfoil=(\"../../data/calisto/NACA0012-radians.csv\",\"radians\"),\n",
+    "    airfoil=(\"../../data/calisto/NACA0012-radians.csv\", \"radians\"),\n",
     ")\n",
     "\n",
     "tail = calisto.add_tail(\n",
@@ -194,7 +192,7 @@
     "            heading=heading,\n",
     "            name=f\"Incl {inclination} Head {heading}\",\n",
     "        )\n",
-    "        flights.append(flight)\n"
+    "        flights.append(flight)"
    ]
   },
   {