This allows PWM and all other output methods to configure
stopped, idling and full thrust points and use them consistently.
The fact that a fixed wing motor can be stopped when zero thrust
is demanded is explicit and could in principle even be disabled.
The mechanism is the same as for a standard VTOL stopping the
multicopter motors in the fixed wing flight phase.
This allows to consistently define:
Motor stopped - disarmed PWM
Motor idling - minimum PWM
Motor at full thrust - maximum PWM
Any allocation can then distinctly decide if
a motor should be running or not depending
on the context and also explicitly command that.
This is required to process data from the ADS1115 ADC and enables the
params BATx_I_CHANNEL and BATx_V_CHANNEL.
Testing is required whether this actually works on Pixhawk 6X though.
Signed-off-by: Julian Oes <julian@oes.ch>
When switching into Hold mode establish a Loiter around current position,
even if we were before already loitering (eg in Mission mode).
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Having newline between I think didn't apply the PR stale days setting of
30 properly (it was using 45)
And it seemd that unless I set the days-before-close to -1
intentionally, it would still close the Issue/PRs, as the default value
is 7 already.
Also updated version of the stale action to v8
* Remove old stale bot yaml file
* Remove slack svg file (unused)
* Stale action: Only apply stale label, and no other actions
Respecting the opinion on
fa9ac6ecf6,
it seems reasonable to disable commenting feature, and just keep the
action only applying the `stale` label. This will reduce the noise /
email spams / ping pong fight with the stale bot (Action)
- Remove unnecessary text rendering, which made clicking log links
harder
- Re adjust markdown elements to make it easier to read / intuitive when
creating an issue
Instead of hard-coding the tilting duration (from FW to MC tilt),
expose it as a parameter (VT_BT_TILT_DUR). The default is the same
as the hard-coded value previously (1s).
Slower tilting mechanisms need a higher value here, while for smaller
ones a too high value results in unnecessary delays till the motors
are in hover configuration.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This affects how soon after a backtransition the vehicle has the
full hover controller running again. Specifically it reduces the
duration of the ramp down of the motors prior to tilting them.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Matthias Grob
xianglunkai
Beat Küng
bresch
Julian Oes
Vincent Poon
Antonio Sanjurjo C
Patrick José Pereira
Thomas Stastny
Silvan Fuhrer
Andrew Brahim
Igor Mišić
Harrison Gieraltowski
Junwoo Hwang
Peter van der Perk
Ramon Roche