run motors output at rate thread loop rate
allow rate thread to be enabled/disabled at runtime for in-flight impact testing
setup the right PID notch sample rate when using the rate thread the PID notches
run at a very different sample rate
call update_dynamic_notch_at_specified_rate() in rate thread
log RTDT messages to track rate loop performance
set dt each cycle of the rate loop thread
run rate controller on samples as soon as they are ready
detect overload conditions in both the rate loop and main loop
decimate the rate thread if the CPU appears overloaded
decimate the gyro window inside the IMU
add in gyro drift to attitude rate thread
add fixed-rate thread option
configure rate loop based on AP_INERTIALSENSOR_FAST_SAMPLE_WINDOW_ENABLED
better rate loop thread decimation management
ensure fix rate attitude is enabled on arming
add rate loop timing debug
update backend filters rather than all the backends
provide more options around attitude rates
only log attitude and IMU from main loop
force trigger_groups() and reduce attitude thread priority
migrate fast rate enablement to FSTRATE_ENABLE
remove rate thread logging configuration and choose sensible logging rates
conditionally compile rate thread pieces
allow fast rate decimation to be user throttled
if target rate changes immediately jump to target rate
recover quickly from rate changes
ensure fixed rate always prints the rate on arming and is always up to date
add support for fixed rate attitude that does not change when disarmed
only push to subsystems at main loop rate
add logging and motor timing debug
correctly round gyro decimation rates
set dshot rate when changing attitude rate
fallback to higher dshot rates at lower loop rates
re-factor rate loop rate updates
log rates in systemid mode
reset target modifiers at loop rate
don't compile in support on tradheli
move rate thread into its own compilation unit
add rate loop config abstraction that allows code to be elided on non-copter builds
dynamically enable/disable rate thread correctly
add design comment for the rate thread
Co-authored-by: Andrew Tridgell <andrew@tridgell.net>
Fixes this compiler error:
In file included from ../../ArduCopter/sensors.cpp:1:
In file included from ../../ArduCopter/Copter.h:195:
../../ArduCopter/mode.h:1291:9: fatal error: declaration shadows a variable in the global namespace [-Wshadow]
AUTO, // after A and B defined, pilot toggle the switch from one side to the other, vehicle flies autonomously
^
../../ArduCopter/defines.h:38:5: note: previous declaration is here
AUTO = 3, // fully automatic waypoint control using mission commands
^
1 error generated.
this implements what betaflight calls 'air-mode'. This gives attitude
control when throttle is at zero, allowing for zero-throttle maneuvers,
plus keeping the copter level on the ground.
This was already implemented if an interlock switch was setup, but it
should also work with an arming switch. If using an arming switch then
throttle should not be considered zero as long as the arming switch
hasn't gone low.
Now calls AP_SmartRTL::set_home when arming. In addition, it calls it whenever
the ahrs home is set to the current location, whether by GCS or in-flight
Copter: merge
Calling update_simple_mode_bearing calls get-heading
rather than the other way around
This will have the advantage of not calculating home bearing
when we stop calling update_simple_mode_bearing unnecesarily
Andy Piper
Peter Barker
muramura
Iampete1
Tatsuya Yamaguchi
Peter Hall
Randy Mackay
bnsgeyer
Patrick José Pereira
Tom Pittenger
Andrew Tridgell
Michael du Breuil
Peter Barker
Dylan Herman