add harmonic notch tracking mode
call AP_GyroFFT::update_freq_hover() from update_throttle_hover()
move gyrofft configuration and control to AP_Vehicle
move fft logging to fft library
this stops us using uninitialised values in modes like circle which
can operate either with or without RC input. If we didn't have a RC
receiver attached then they would use a maximum yaw rate (which
produces quite a spectacular result for a tuned up racing quad)
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.
Added equivalent parameters to WPNAV_SPEED_UP and WPNAV_SPEED_DN
New parameters named:
PILOT_SPEED_UP (technically renamed PILOT_VELZ_MAX)
PILOT_SPEED_DN
Removed parameter PILOT_VELZ_MAX (technically renamed to PILOT_SPEED_UP).
Flight Modes impacted:
ALTHOLD
AUTOTUNE
CIRCLE
LOITER
POSHOLD
SPORT
TAKEOFF
Update a section in GUIDED mode but I don't think it is ever used but update just in case.
It will use the PILOT_SPEED_UP for ascending max velocity. For down it will check if
it is 0, if so then it will PILOT_SPEED_UP instead, if non zero it will use PILOT_SPEED_DN.
This retains current behavior and gives the flexibility to change it if desired.
this handles glitches from the rangefinder when tracking the
ground. It requires 3 readings in a row to settle on a new target
altitude
thanks to discussions with Leonard and Randy
Previously we loaded up the I term from the pilot's input but a more reliable method is to get what was passed into the attitude controller. In particular the addition of the acro-thr-mid parameter means the pilot's input must be interpreted differently for different flight modes.
Previously we had _smooth and non-smooth methods in the attitude
controller but as part of the move to quaternions these have been replaced
by a single call which always takes a smoothing gain
Peter Barker
Leonard Hall
Andy Piper
Randy Mackay
Andrew Tridgell
Michael du Breuil
Ebin
Dr.-Ing. Amilcar Do Carmo Lucas
ChrisBird
Mathieu OTHACEHE