REV: revert airbrakes commits

RocketPy-Team · Oct 6, 2023 · 75698c8 · 75698c8
1 parent 9bd78df
commit 75698c8
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Showing 12 changed files with 2 additions and 433 deletions.
diff --git a/rocketpy/__init__.py b/rocketpy/__init__.py
@@ -22,7 +22,6 @@
     TankGeometry,
     UllageBasedTank,
 )
-from .control import Controller
 from .rocket import (
     AeroSurface,
     Components,

diff --git a/rocketpy/control/__init__.py b/rocketpy/control/__init__.py
diff --git a/rocketpy/control/controller.py b/rocketpy/control/controller.py
diff --git a/rocketpy/plots/__init__.py b/rocketpy/plots/__init__.py
@@ -4,7 +4,6 @@
     _NoseConePlots,
     _TailPlots,
     _TrapezoidalFinsPlots,
-    _AirbrakesPlots,
 )
 from .compare import Compare, CompareFlights
 from .environment_analysis_plots import _EnvironmentAnalysisPlots

diff --git a/rocketpy/plots/aero_surface_plots.py b/rocketpy/plots/aero_surface_plots.py
@@ -448,28 +448,3 @@ def __init__(self, tail):
     def draw(self):
         # This will de done in the future
         return None
-
-
-class _AirbrakesPlots(_AeroSurfacePlots):
-    """Class that contains all tail plots."""
-
-    def __init__(self, tail):
-        """Initialize the class
-
-        Parameters
-        ----------
-        tail : rocketpy.AeroSurface.Tail
-            Tail object to be plotted
-
-        Returns
-        -------
-        None
-        """
-        super().__init__(tail)
-        return None
-
-    def cd_s_curve(self):
-        return self.cd_s_curve.plot(0, 1)
-
-    def draw(self):
-        raise NotImplementedError
diff --git a/rocketpy/prints/__init__.py b/rocketpy/prints/__init__.py
@@ -4,7 +4,6 @@
     _RailButtonsPrints,
     _TailPrints,
     _TrapezoidalFinsPrints,
-    _AirbrakesPrints,
 )
 from .compare_prints import _ComparePrints
 from .environment_analysis_prints import _EnvironmentAnalysisPrints

diff --git a/rocketpy/prints/aero_surface_prints.py b/rocketpy/prints/aero_surface_prints.py
@@ -291,41 +291,3 @@ def geometry(self):
             f"Angular position of the buttons: {self.aero_surface.angular_position:.3f} deg\n"
         )
         return None
-
-
-class _AirbrakesPrints(_AeroSurfacePrints):
-    """Class that contains all tail prints."""
-
-    def __init__(self, Airbrakes):
-        """Initialize the class
-
-        Parameters
-        ----------
-        Airbrakes : rocketpy.AeroSurface.Airbrakes
-            Air break object to be printed.
-
-        Returns
-        -------
-        None
-        """
-        super().__init__(Airbrakes)
-        return None
-
-    def geometry(self):
-        """Prints the geometric information of the air break.
-
-        Returns
-        -------
-        None
-        """
-        print(f"Geometric information of the Air Break:")
-        print(f"----------------------------------")
-        print(
-            f"Current deployed level: {self.aero_surface.deployed_level:.2f} = {100*self.aero_surface.deployed_level:.0f} %"
-        )
-        print(
-            f"Current Cd_S: {self.aero_surface.cd_s_curve(self.aero_surface.deployed_level)} m²"
-        )
-        print(f"Maximum Cd_S: {self.aero_surface.cd_s.max:.3f} m²")
-        print(f"Minimum Cd_S: {self.aero_surface.cd_s.min:.3f} m²")
-        return None
diff --git a/rocketpy/prints/control_prints.py b/rocketpy/prints/control_prints.py
diff --git a/rocketpy/rocket/__init__.py b/rocketpy/rocket/__init__.py
@@ -6,7 +6,6 @@
     RailButtons,
     Tail,
     TrapezoidalFins,
-    Airbrakes,
 )
 from .components import Components
 from .parachute import Parachute