Skip to content
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

Update quadplane-transitions.rst #6515

Merged
merged 1 commit into from
Jan 7, 2025
Merged
Changes from all commits
Commits
File filter

Filter by extension

Filter by extension

Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
2 changes: 1 addition & 1 deletion plane/source/docs/quadplane-transitions.rst
Original file line number Diff line number Diff line change
Expand Up @@ -40,7 +40,7 @@ Transition to Fixed Wing Mode from VTOL

- If :ref:`Q_TRANS_FAIL<Q_TRANS_FAIL>` is not zero, then exceeding this time before reaching :ref:`AIRSPEED_MIN <AIRSPEED_MIN>` airspeed will cancel the transition and the aircraft will immediately execute the action specified by :ref:`Q_TRANS_FAIL_ACT<Q_TRANS_FAIL_ACT>`. The default is 0, which disables this timeout.

.. note:: if bit 19 of :ref:`Q_OPTIONS<Q_OPTIONS>` is set and :ref:`Q_TRANS_FAIL<Q_TRANS_FAIL>` is not zero, and if the airspeed is greater than 1/2 of :ref:`AIRSPEED_MIN<AIRSPEED_MIN>`, then the transition to fixed wing will immediately complete. This is useful if no airspeed sensor is being used, and the transition is into a headwind, which could prevent an accurate airspeed estimate from being obtained until a turn is made. Without using the :ref:`Q_TRANS_FAIL<Q_TRANS_FAIL>` timeout and this Q_OPTION, the transition could be indefinitely long since airspeed might be reported as below :ref:`AIRSPEED_MIN<AIRSPEED_MIN>` due to low groundspeed.
.. note:: for tiltrotors only: if bit 19 of :ref:`Q_OPTIONS<Q_OPTIONS>` is set and :ref:`Q_TRANS_FAIL<Q_TRANS_FAIL>` is not zero, and if the groundspeed is greater than 1/2 of :ref:`AIRSPEED_MIN<AIRSPEED_MIN>`, then the transition to fixed wing will immediately complete. This is useful if no airspeed sensor is being used, and the transition is into a headwind, which could prevent an accurate airspeed estimate from being obtained until a turn is made. Without using the :ref:`Q_TRANS_FAIL<Q_TRANS_FAIL>` timeout and this Q_OPTION, the transition could be indefinitely long since airspeed might be reported as below :ref:`AIRSPEED_MIN<AIRSPEED_MIN>` due to low groundspeed.

.. note:: The airspeed used during transition can be found in dataflash logs as CTUN.As. This is a canonical value which will include the airspeed sensor if enabled, or use the synthetic airspeed if not.

Expand Down