docs: auto-sync metadata [skip ci]

Co-Authored-By: PX4 BuildBot <bot@px4.io>

docs/en/config_heli/index.md

@@ -42,14 +42,12 @@ To setup and configure a helicopter:
    ![Geometry: helicopter](../../assets/config/actuators/qgc_geometry_helicopter.png)
 
    The motors have no configurable geometry:
-
    - `Rotor (Motor 1)`: The main rotor
    - `Yaw tail motor (Motor 2)`: The tail rotor
 
    Swash plate servos: `3` | `4` <!-- 4 provides additional stability -->
 
    For each servo set:
-
    - `Angle`: Clockwise angle in degree on the swash plate circle at which the servo arm is attached starting from `0` pointing forwards.
      Example for a typical setup where three servos are controlling the swash plate equally distributed over the circle (360° / 3 =) 120° apart each which results in the angles:
 
@@ -65,7 +63,6 @@ To setup and configure a helicopter:
    - `Trim`: Offset individual servo positions. This is only needed in rare case when the swash plate is not level even though all servos are centered.
 
    Additional settings:
-
    - `Yaw compensation scale based on collective pitch`: How much yaw is feed forward compensated based on the current collective pitch.
    - `Main rotor turns counter-clockwise`: `Disabled` (clockwise rotation) | `Enabled`
    - `Throttle spoolup time`: Set value (in seconds) greater than the achievable minimum motor spool up time.
@@ -73,12 +70,10 @@ To setup and configure a helicopter:
 
 1. Remove the rotor blades and propellers
 1. Assign motors and servos to outputs and test (also in [Actuator configuration](../config/actuators.md)):
-
    1. Assign the [motors and servos to the outputs](../config/actuators.md#actuator-outputs).
    1. Power the vehicle with a battery and use the [actuator testing sliders](../config/actuators.md#actuator-testing) to validate correct servo and motor assignment and direction.
 
 1. Using an RC in [Acro mode](../flight_modes_mc/acro.md), verify the correct movement of the swash-plate. With most airframes you need to see the following:
-
    - Moving the roll stick to the right should tilt the swash-plate to the right.
    - Moving the pitch stick forward should tilt the swash-plate forward.
 
@@ -144,7 +139,6 @@ The rate controller should be tuned in [Acro mode](../flight_modes_mc/acro.md),
 
 3. Then enable the PID gains.
    Start off with following values:
-
    - [MC_ROLLRATE_P](../advanced_config/parameter_reference.md#MC_ROLLRATE_P), [MC_PITCHRATE_P](../advanced_config/parameter_reference.md#MC_PITCHRATE_P) a quarter of the value you found to work well as the corresponding feed forward value in the previous step. `P = FF / 4`
 
    ```sh