The StorageManager read_block/write_block methods only return failure if
an out of bounds access is performed. Assert statically that this does
not happen.
Also remove the now-impossible failed to add node state.
This example intercepts PREFLIGHT_REBOOT_SHUTDOWN COMMAND_LONG's and if
param1==2, it shuts down the BQ40Z smart battery BMS. Otherwise it
passes through the COMMAND_LONG as a COMMAND_INT (this required updating
the gcs:run_command_int to return a MAV_RESULT rather than a bool).
This adds bindings for an I2CDevice's transfer() function, an example,
and removes the nil return hint from the get_device() docs as it never
actually returns nil.
Remove unnecessary header
Switch parameters to default initialization
Change pointer casting to prevent a const_cast, and remove doubled sync byte when echoing ASCII messages
Fix Valgrind report by preventing use of nmea_printf on buffers which may not be null-terminated
In AHRS Mode, split the single message to an IMU packet and an AHRS packet; in EKF Mode, split the two messages into an IMU message, an EKF packet, and a GNSS packet.
Simplify message header definition to consolidate and eliminate the need for static asserts
Update healthy logic and use to represent new packet structure
Replace EAH3 message with messages per-packet
Add Ypr as configured output in the EKF message
These concern the TAKEOFF flight stage and address #27147.
* Logging metadata fixes
* Disabled continuous TECS reset during takeoff
* Fixed bug in reached_speed_takeoff calculation
* Limited SPDWEIGHT=2 to only first part of takeoff climb
* _post_TO_hgt_offset set to constant
* Takeoff I-gain now defaults to 0 and is used
* Use at least TRIM_THROTTLE during the climb
* Updated description of TECS_TKOFF_IGAIN with new behaviour
* Forced max throttle while below TKOFF_LVL_ALT
* Added throttle constraints in no-airspeed mode
Additionally, set_min_throttle() has been created, that allows one to
set the minimum TECS throttle for the next update_pitch_throttle() loop.
Additionally, the throttle limits system has been reworked. TECS will
receive external throttle limits from Plane and will always take them
into account and respect them.
If the Gyro/Accel ID is already in the registered list, do not try to add it again.
This stops an issue seen on a CubeOrangePlus BG3 where, during the very first boot after a parameter wipe, software incorrectly registers a fourth IMU.
The Fourth IMU is registered because the AUX IMU is the same DevID as the third ICM45686.
- Wrapped the definition of `serial_instance` with preprocessor directives to ensure it is only defined when necessary.
- This resolves the compile error caused by the unused variable when no features requiring `serial_instance` are enabled.
