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In the current master branch, altitude hold seems to be broken. This seems to come from the work on the position controller (see #136) that broke the control modes contained in the setpoint structure.
The text was updated successfully, but these errors were encountered:
With PR #172 the altitude hold now holds a constant vertical velocity. The current altitude estimator is not outputting vertical velocity which would explain this phenomena.
39831c3 fixes altitude-hold. I also tried to tune a bit the Z estimator (there was an oscillation between the thrust and the height measurement, fixed by filtering the pressure sensor a bit harder).
In the current master branch, altitude hold seems to be broken. This seems to come from the work on the position controller (see #136) that broke the control modes contained in the setpoint structure.
The text was updated successfully, but these errors were encountered: