Ardu copter 3.2.1 #1
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headers were not always being written
the new GPS driver only ever needs a non-blocking port
the EKF check works reliably but attempts to check the inertial nav for errors has not been successful. I could not find a way to reliably catch flyaways without also introducing false positives (and thus unwanted LANDings)
… used for control pass-through.
… constructor. To be used for flybar passthrough.
reference to rc_1, rc2 are replaced with constant updates during acro_run
fixes pull #1320 thanks Arthur!
this saves a tiny amount of time by removing the memory copy of a Vector3f
this allows magfailed status to show on console via SYS_STATUS health bits
Made more strict by requiring 50 consecutive iterations where the climb rate is below +- 40cm/s. Previously it was 50 cumulative. Removed check of failsafe.radio when clearing the land flag because it could result in the vehicle taking off if the user picked it up.
Simulated copter is flying too high and causing the land to timeout
this prevents a "jump loop" from causing a firmware lockup. Thanks to dellarb for reporting this!
Protect against the GCS sending multiple arming messages close together which disrupts the gyro calibration
The alt limit is instead enforced when the target is set using the set_alt_target_from_climb_rate function Also updated comments
No changes from AC3.2.1-rc2
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