- force initialize takeoff airspeed setpoint at start of takeoff modes
- force set airspeed constraints if slewed value is out of bounds
- always slew airspeed setpoints as long as inside constraints
- move target airspeed setpoint calculation into mode specific logic regions (hand vs runway)
when we're in a takeoff situation, we only want to adapt the airspeed to
avoid accelerated stall due to load factor changes. Disable othre logic
like minimum ground speed, wind based adaption and airspeed slew rating.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- on NuttX if the SD card was just cleared (quick format) it's possible for the newly created uninitialized dataman file to still have the previous compatibility key, which causes the initialization to be skipped
When the yaw estimate is converging, the controller makes the drone yaw
in order to follow the current setpoint. This is unintuitive for the
pilot and it is preferable if the drone continues to fly towards the
same physical direction.
This estimate doesn't converge to the true yaw but can be used as a
more consistent but drifting heading source.
It can be used by a setpoint generator to adjust its heading setpoint
while the true yaw estimate is converging in order to keep a constant
course over ground.
If the measured voltage is more than 65v we need to split the voltage
over multiple cells in order to avoid overflowing the uint16. This is
according to the MAVLink spec.
Signed-off-by: Julian Oes <julian@oes.ch>
The extension fields need to be 0 by default according to the MAVLink
spec. This is because extensions are 0 by default and need to be 0 when
unknown/unused for backwards compatibility.
The patch also simplifies the flow slightly in that it doesn't create a
temporary array but just fills in the cell voltages directly.
Signed-off-by: Julian Oes <julian@oes.ch>
- Enable arbitrary euler angle for Mag rotation
- new CUSTOM rotation enum out of the normal enum range
- mag_rot: automatically change to custom if euler rot is set
- sensor_calibration: Magnetometer save custom rotation parameters
- mag_cal: cross mention rotation parameters
- This allows the user to see the RPY options when searching for the rotation parameter
---------
Co-authored-by: Junwoo Hwang <junwoo@auterion.com>
Co-authored-by: bresch <[brescianimathieu@gmail.com](mailto:brescianimathieu@gmail.com)>
Co-authored-by: Daniel Agar <daniel@agar.ca>
During transition to FF, only allow update thrust axis up to 45° as with a high tilt angle
the effectiveness of the thrust axis in z is apporaching 0, and by that is increasing
the motor output to max.
Transition to HF: disable thrust axis tilting, and assume motors are vertical. This is to avoid
a thrust spike when the transition is initiated (as then the tilt is fully forward).
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
EffectivenessTiltrotor: link time when to tilt motors to MC position to COM_SPOOLUP_TIME
- remove VT_TILT_SPINUP and special spin up tilt handling form the VTOL module
- now handle the spoolup in the allocation, directly linked to COM_SPOOLUP_TIME
- leave tilts at disarmed value during spoolup
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- when GNSS is used require low mag heading innovations during
horizontal acceleration (yaw observable) to validate the mag
- only fuse mag heading just enough to constrain the yaw estimate
variance to a sane value. Leave enough uncertainty to allow for a
correction when the yaw is observable through GNSS fusion
In the mavlink_receiver code, after a while it will try to resend some
parameter update through the MAVLink instance. But for Iridium links
those are not a good idea. So this adds a condition that prevent the
sending if the MAVLink instance is in Iridium mode.
Related to issue #21496
