MNT: Tweak the discretization bounds.

Author: phmbressan

rocketpy/rocket/aero_surface/fins/fins.py

@@ -441,7 +441,7 @@ def to_dict(self, **kwargs):
             cl = self.cl
             if kwargs.get("discretize", False):
                 cl = cl.set_discrete(
-                    (-np.pi / 12, 0), (np.pi / 12, 2), (10, 10), mutate_self=False
+                    (-np.pi / 6, 0), (np.pi / 6, 2), (10, 10), mutate_self=False
                 )
 
             data.update(

rocketpy/rocket/aero_surface/nose_cone.py

@@ -537,9 +537,9 @@ def to_dict(self, **kwargs):
             clalpha = self.clalpha
             cl = self.cl
             if kwargs.get("discretize", False):
-                clalpha = clalpha.set_discrete(0, 2, 50)
+                clalpha = clalpha.set_discrete(0, 4, 50)
                 cl = cl.set_discrete(
-                    (-np.pi / 12, 0), (np.pi / 12, 2), (10, 10), mutate_self=False
+                    (-np.pi / 6, 0), (np.pi / 6, 2), (10, 10), mutate_self=False
                 )
             data["cp"] = self.cp
             data["clalpha"] = clalpha

rocketpy/rocket/aero_surface/tail.py

@@ -218,9 +218,9 @@ def to_dict(self, **kwargs):
             clalpha = self.clalpha
             cl = self.cl
             if kwargs.get("discretize", False):
-                clalpha = clalpha.set_discrete(0, 2, 50)
+                clalpha = clalpha.set_discrete(0, 4, 50)
                 cl = cl.set_discrete(
-                    (-np.pi / 12, 0), (np.pi / 12, 2), (10, 10), mutate_self=False
+                    (-np.pi / 6, 0), (np.pi / 6, 2), (10, 10), mutate_self=False
                 )
 
             data.update(

rocketpy/rocket/rocket.py

@@ -1899,8 +1899,8 @@ def to_dict(self, **kwargs):
         power_off_drag = self.power_off_drag
         power_on_drag = self.power_on_drag
         if discretize:
-            power_off_drag = power_off_drag.set_discrete(0, 2, 50, mutate_self=False)
-            power_on_drag = power_on_drag.set_discrete(0, 2, 50, mutate_self=False)
+            power_off_drag = power_off_drag.set_discrete(0, 4, 50, mutate_self=False)
+            power_on_drag = power_on_drag.set_discrete(0, 4, 50, mutate_self=False)
 
         rocket_dict = {
             "radius": self.radius,
@@ -1940,7 +1940,7 @@ def to_dict(self, **kwargs):
                 thrust_to_weight = thrust_to_weight.set_discrete_based_on_model(
                     self.motor.thrust, mutate_self=False
                 )
-                cp_position = cp_position.set_discrete(0, 2, 25, mutate_self=False)
+                cp_position = cp_position.set_discrete(0, 4, 25, mutate_self=False)
                 stability_margin = stability_margin.set_discrete(
                     (0, self.motor.burn_time[0]),
                     (2, self.motor.burn_time[1]),