Fix comment

zuorenchen · zuorenchen · commit f87fd028d650 · 2026-06-14T22:28:58.000+01:00
diff --git a/rocketpy/rocket/actuator/thrust_vector.py b/rocketpy/rocket/actuator/thrust_vector.py
@@ -164,8 +164,8 @@ class ThrustVectorActuator2D:
         Time constant for the thrust vector actuator dynamics (first-order IIR filter) in seconds.
     ThrustVectorActuator2D.actuator_initial_output : float
         Initial thrust  gimbal angles in deg.
-    ThrustVectorActuator2D.actuator_output : float
-        Current thrust vector gimble angles in deg.
+    ThrustVectorActuator2D.actuator_output : tuple[float, float]
+        Current thrust vector gimbal angles (x, y) in deg.
 
     """
 
diff --git a/rocketpy/simulation/flight.py b/rocketpy/simulation/flight.py
@@ -1878,7 +1878,7 @@ def u_dot(self, t, u, post_processing=False):  # pylint: disable=too-many-locals
                 getattr(self.rocket, "throttle_control", None), "throttle", 1.0
             )
 
-            # Thrust Vector Control (TVC))
+            # Thrust Vector Control (TVC)
             if hasattr(self.rocket, "thrust_vector_control"):
                 # TVC Fz thrust: F = T * sqrt(1 - sin(gimbal_angle_x)**2 - sin(gimbal_angle_y)**2)
                 thrust3 = effective_thrust * np.sqrt(

Original file line number	Diff line number	Diff line change
`@@ -1878,7 +1878,7 @@ def u_dot(self, t, u, post_processing=False): # pylint: disable=too-many-locals`
`1878`	`1878`	`getattr(self.rocket, "throttle_control", None), "throttle", 1.0`
`1879`	`1879`	`)`
`1880`	`1880`
`1881`		`- # Thrust Vector Control (TVC))`
	`1881`	`+ # Thrust Vector Control (TVC)`
`1882`	`1882`	`if hasattr(self.rocket, "thrust_vector_control"):`
`1883`	`1883`	`# TVC Fz thrust: F = T * sqrt(1 - sin(gimbal_angle_x)2 - sin(gimbal_angle_y)2)`
`1884`	`1884`	`thrust3 = effective_thrust * np.sqrt(`