According to the mavlink spec we should be publishing the home attitude
as a quaternion rather than just the yaw/heading.
Additionally, this allows setting the landing roll and pitch angle using
DO_SET_HOME (this yet needs to go into the MAVLink spec though).
This time including the message versioning and translation.
According to the mavlink spec we should be publishing the home attitude
as a quaternion rather than just the yaw/heading.
Additionally, this allows setting the landing roll and pitch angle using
DO_SET_HOME (this yet needs to go into the MAVLink spec though).
Within the first 2min of a flight, check if the integrated GNSS vertical velocity and the baro
measurements disagree with the reported GNSS altitude, and in that case update the
set home position altitude to cancel out GNSS altitude drift.
* prevent re-init when reaching negative altitudes
* only allow correction during the first 120 second after takeoff
* add dependency to COM_HOME_EN parameter. reset vel-integral for multiple takeoffs
