The OSD stats provide no meaningful information and are just an annoyance when exiting these special states.
For Launch Control the stats will be displayed if the launch is triggered and normal flight occurrred.
If the quad is in an extreme orientation (like upside down) the transition to self-level modes can cause enough motion to trigger crash recovery. Added a 1 second delay during which crash recovery detection is blocked immediately after entering a self-level mode.
This also addresses an issue with GPS Rescue as when it activates it enables self-level. If in the above scenario this triggered a crash recovery detection then GPS Rescue would interpret this as a crash and immediately disarm.
Percentage implementation
Settings fix, formatting
Add support for different number of motors
Optimize and cut superfluous code
Hard-add mixer.h
Formatting adjustment to fit BF standards, linking error in unittest fix attempt
Add stubs and variables for unittests
Character based indicators
Change output to special characters
Fix spacing
Update test code, add variable
Include changes as per peer review
Adds a race start assistance system that allows the pilot to pitch forward and then release the sticks with the quad holding position for the race start.
Remove unnecessary decidegrees conversions as all temperature providers are in degrees celcius.
Fixed rounding for imperial units.
Fixed data type error in core temp warning element. Temperature is captured as int16 and can be negative but logic was using uint8 leading to an underflow for negative temperatures and a false alarm triggering.
Refactor iterm_relax to iterm_relax_axis
Isolate pidLevel test
Isolate pidHorizon tests
remove if UNIT_TEST
revert to iterm_relax from iterm_relax_axis
Previously the logic would process all possible ranges defined by MAX_ADJUSTMENT_RANGE_COUNT even if some (or even all) ranges were not configured. This change first builds a list of configured ranges and only processes thos entries.
Reduces CPU load by skipping unnecessary processing and minimizes the impact of increasing the number of available ranges.
Calculation was assuming that the GPS groundspeed was in 1/10 m/s when in reality it's in cm/s units. This was causing the value sent in telemetry to be 10 times too large.
Refactor PID code Iterm Relax and Absolute control
Move defines for unittest to Makefile
Fix unittest isAirmodeActivated()
Absolute control unittests + optimizations
Fix dead code absolute control // unittests
Further optimizations to absolute control switch logic
