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.
control copter floor fence with autoenable
autoenable floor fence with a margin
check for manual recovery only after having checked the fences
make auto-disabling for minimum altitude fence an option
output message when fence floor auto-enabled
re-use fence floor auto-enable/disable from plane
auto-disable on landing
do not update enable parameter when controlling through mavlink
make sure get_enabled_fences() actually returns enabled fences.
make current fences enabled internal state rather than persistent
implement auto options correctly and on copter
add fence names utility
use ExpandingString for constructing fence names
correctly check whether fences are enabled or not and disable min alt for landing in all auto modes
add enable_configured() for use by mavlink and rc
add events for all fence types
make sure that auto fences are no longer candidates after manual updates
add fence debug
make sure rc switch is the ultimate authority on fences
reset auto mask when enabling or disabling fencing
ensure auto-enable on arming works as intended
simplify printing fence notices
reset autofences when auot-enablement is changed
When stall prevention is enabled we were scaling from the aircraft's
minimum flight speed. However this is normally already picked as being
above the stall speed, and for a variety of reasons we may want to pin
the aircraft at a higher minimum speed. But if the aircraft was
commanded to fly to close to that minimum speed as soon as it banked for
a pattern it would command a increase in speed to keep it away from
stalling. However if your minimum speed is far from stalling this
increase was incorrect. To make it worse what this actually results in
happening is an aircraft diving for more speed (over 10 m/s on some
aircraft) as well as descending to gain that speed resulting in over 200
foot deviations in altitude control.
Only create the binding object (singleton metatable/userdata or C
function reference) once the user first references a particular
singleton or userdata creation function. Once created, the object is
stored into the script's environment so it doesn't get recreated on the
next reference and there isn't any further overhead. The userdatas are
no longer shared between scripts which imposes a slight memory penalty
for multiple scripts using the same singleton but this avoids an
additional lookup time cost.
Userdata and ap_objects aren't eligible for this optimization as the C++
code might want a particular metatable at any time.
Saves ~9.3K Lua heap.
The global table is then used as the __index metamethod of each state's
environment table. Avoids the overhead of loading binding objects into
each state. The binding objects are immutable from Lua so sandboxing is
not violated.
Does have the slight downside that a script can no longer know all the
binding names by enumerating _ENV.
Saves ~700B of memory per loaded script.
Thomas Watson
Ian Burwell
Iampete1
Bob Long
BLash
George Zogopoulos
cuav-chen2
Peter Barker
Andrew Tridgell
yaapu
muramura
Leonard Hall
Randy Mackay
Andy Piper
James O'Shannessy
Luca Pescante
bugobliterator
mduclehcm
Paul Riseborough
rishabsingh3003
Henry Wurzburg
Rhys Mainwaring
xiaozhou
Michael du Breuil