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1 change: 1 addition & 0 deletions CHANGELOG.md
Original file line number Diff line number Diff line change
Expand Up @@ -60,6 +60,7 @@ Attention: The newest changes should be on top -->
- BUG: energy_data plot not working for 3 dof sims [[#906](https://github.com/RocketPy-Team/RocketPy/issues/906)]
- BUG: Fix CSV column header spacing in FlightDataExporter [#864](https://github.com/RocketPy-Team/RocketPy/issues/864)
- BUG: Fix parallel Monte Carlo simulation showing incorrect iteration count [#806](https://github.com/RocketPy-Team/RocketPy/pull/806)
- BUG: Fix missing titles in roll parameter plots for fin sets [#934](https://github.com/RocketPy-Team/RocketPy/pull/934)
- BUG: Duplicate _controllers in Flight.TimeNodes.merge() [#931](https://github.com/RocketPy-Team/RocketPy/pull/931)

## [v1.11.0] - 2025-11-01
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1 change: 0 additions & 1 deletion rocketpy/plots/aero_surface_plots.py
Original file line number Diff line number Diff line change
Expand Up @@ -164,7 +164,6 @@ def roll(self):
None
"""
print("Roll parameters:")
# TODO: lacks a title in the plots
self.aero_surface.roll_parameters[0]()
self.aero_surface.roll_parameters[1]()

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2 changes: 2 additions & 0 deletions rocketpy/rocket/aero_surface/fins/fins.py
Original file line number Diff line number Diff line change
Expand Up @@ -328,6 +328,7 @@ def evaluate_roll_parameters(self):
) # Function of mach number
clf_delta.set_inputs("Mach")
clf_delta.set_outputs("Roll moment forcing coefficient derivative")
clf_delta.set_title(None)
cld_omega = (
2
* self.roll_damping_interference_factor
Expand All @@ -339,6 +340,7 @@ def evaluate_roll_parameters(self):
) # Function of mach number
cld_omega.set_inputs("Mach")
cld_omega.set_outputs("Roll moment damping coefficient derivative")
cld_omega.set_title(None)
self.roll_parameters = [clf_delta, cld_omega, self.cant_angle_rad]
return self.roll_parameters

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