diff --git a/docs/assets/config/fw/autotune.png b/docs/assets/config/fw/autotune.png
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diff --git a/docs/en/config/_autotune.md b/docs/en/config/_autotune.md
index 0a87201c7a..9bf06a4f88 100644
--- a/docs/en/config/_autotune.md
+++ b/docs/en/config/_autotune.md
@@ -91,9 +91,17 @@ The test steps are:
3. Ensure that the **Autotune enabled** button is enabled (this will display the **Autotune** button and remove the manual tuning selectors).
4. Read the warning popup and click on **OK** to start tuning.
+
+
4. The drone will first start to perform quick roll motions followed by pitch and yaw motions.
The progress is shown in the progress bar, next to the _Autotune_ button.
+
+
+4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
+ The progress is shown in the progress bar, next to the _Autotune_ button.
+
+
5. Manually land and disarm to apply the new tuning parameters.
@@ -104,6 +112,13 @@ The test steps are:
5. The tuning will be immediately/automatically be applied and tested in flight (by default).
PX4 will then run a 4 second test and revert the new tuning if a problem is detected.
+The figure below shows how steps 4 and 5 might look in flight on the pitch axis.
+The pitch rate gradually increases up until it reaches the target.
+This amplitude is then held while the signal frequency is increased.
+You can then see how the tuned system is able to follow the setpoint in the test signal.
+
+

+
::: warning
@@ -170,9 +185,23 @@ Fast oscillations (more than 1 oscillation per second): this is because the gain
### The auto-tuning sequence fails
+
+
If the drone was not moving enough during auto-tuning, the system identification algorithm might have issues to find the correct coefficients.
-Increase the
[MC_AT_SYSID_AMP](../advanced_config/parameter_reference.md#MC_AT_SYSID_AMP)
[FW_AT_SYSID_AMP](../advanced_config/parameter_reference.md#FW_AT_SYSID_AMP)
parameter by steps of 1 and trigger the auto-tune again.
+Increase the [MC_AT_SYSID_AMP](../advanced_config/parameter_reference.md#MC_AT_SYSID_AMP) parameter by steps of 1 and trigger the auto-tune again.
+
+
+
+
+By default, the autotune maneuvers ensure that a sufficient angular rate is reached for system identification. The target rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
+
+If the signal-to-noise ratio of the vehicle is low, the system identification algorithm might have issues finding the correct coefficients. Ensure that there is no excessive noise and/or platform vibration.
+
+
+
+
+
### The drone oscillates after auto-tuning