MNT: patching missing keys

Author: aasitvora99

src/views/flight.py

@@ -27,9 +27,7 @@ class FlightSimulation(ApiBaseView):
     terminate_on_apogee: Optional[bool] = None
     initial_solution: Optional[list] = None
     rocket: Optional[RocketSimulation] = None
-    environment: Optional[EnvironmentSimulation] = None
-
-    # Key Flight Function attributes (discretized by rocketpy_encoder, serialized by RocketPyEncoder)
+    env: Optional[EnvironmentSimulation] = None
 
     # Position and trajectory
     latitude: Optional[Any] = None
@@ -44,12 +42,15 @@ class FlightSimulation(ApiBaseView):
     vy: Optional[Any] = None
     vz: Optional[Any] = None
     speed: Optional[Any] = None
+    max_speed: Optional[Any] = None
+    max_speed_time: Optional[Any] = None
 
     # Key flight metrics
     apogee: Optional[Any] = None
     apogee_time: Optional[Any] = None
     apogee_x: Optional[Any] = None
     apogee_y: Optional[Any] = None
+    apogee_freestream_speed: Optional[Any] = None
     x_impact: Optional[Any] = None
     y_impact: Optional[Any] = None
     z_impact: Optional[Any] = None
@@ -61,6 +62,10 @@ class FlightSimulation(ApiBaseView):
     max_acceleration_time: Optional[Any] = None
     aerodynamic_drag: Optional[Any] = None
     aerodynamic_lift: Optional[Any] = None
+    max_acceleration_power_on: Optional[Any] = None
+    max_acceleration_power_on_time: Optional[Any] = None
+    max_acceleration_power_off: Optional[Any] = None
+    max_acceleration_power_off_time: Optional[Any] = None
 
     # Flight dynamics
     mach_number: Optional[Any] = None
@@ -69,12 +74,34 @@ class FlightSimulation(ApiBaseView):
     angle_of_attack: Optional[Any] = None
     dynamic_pressure: Optional[Any] = None
     max_dynamic_pressure: Optional[Any] = None
+    max_dynamic_pressure_time: Optional[Any] = None
+    reynolds_number: Optional[Any] = None
+    max_reynolds_number: Optional[Any] = None
+    max_reynolds_number_time: Optional[Any] = None
 
     # Time and simulation data
     time: Optional[Any] = None
     solution: Optional[Any] = None
-
-    # Function attributes (discretized by rocketpy_encoder, serialized by RocketPyEncoder)
+    t_final: Optional[Any] = None
+    max_time: Optional[Any] = None
+    max_time_step: Optional[Any] = None
+    min_time_step: Optional[Any] = None
+    rtol: Optional[Any] = None
+    atol: Optional[Any] = None
+    time_overshoot: Optional[Any] = None
+    out_of_rail_time: Optional[Any] = None
+    out_of_rail_time_index: Optional[Any] = None
+    out_of_rail_velocity: Optional[Any] = None
+
+    # Stability margins
+    out_of_rail_stability_margin: Optional[Any] = None
+    initial_stability_margin: Optional[Any] = None
+    max_stability_margin: Optional[Any] = None
+    max_stability_margin_time: Optional[Any] = None
+    min_stability_margin: Optional[Any] = None
+    min_stability_margin_time: Optional[Any] = None
+
+    # Function attributes (discretized by rocketpy_encoder)
     angular_position: Optional[Any] = None
     attitude_angle: Optional[Any] = None
     attitude_vector_x: Optional[Any] = None
@@ -86,13 +113,15 @@ class FlightSimulation(ApiBaseView):
     acceleration_power_off: Optional[Any] = None
     stream_velocity: Optional[Any] = None
     free_stream_speed: Optional[Any] = None
-    apogee_freestream_speed: Optional[Any] = None
-    reynolds_number: Optional[Any] = None
     total_pressure: Optional[Any] = None
     rail_button_normal_force: Optional[Any] = None
     max_rail_button_normal_force: Optional[Any] = None
     rail_button_shear_force: Optional[Any] = None
     max_rail_button_shear_force: Optional[Any] = None
+    max_rail_button1_normal_force: Optional[Any] = None
+    max_rail_button1_shear_force: Optional[Any] = None
+    max_rail_button2_normal_force: Optional[Any] = None
+    max_rail_button2_shear_force: Optional[Any] = None
     rotational_energy: Optional[Any] = None
     translational_energy: Optional[Any] = None
     kinetic_energy: Optional[Any] = None
@@ -102,6 +131,9 @@ class FlightSimulation(ApiBaseView):
     drag_power: Optional[Any] = None
     drift: Optional[Any] = None
 
+    # Environmental conditions
+    frontal_surface_wind: Optional[Any] = None
+    lateral_surface_wind: Optional[Any] = None
 
 class FlightView(FlightModel):
     flight_id: str