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.
for all auto-throttle modes we should not allow a mode change to the
mode if the motor runup is not complete.
This moves the code to the set_mode() so it applies to all modes
fixes issue #6956
Previously we always reset the altitude target to the current altitude but this causes a jump if the vehicle is already in an alt-hold flight mode but has an altitude error
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controller but as part of the move to quaternions these have been replaced
by a single call which always takes a smoothing gain
Further to refactor of RC_Channel class which included
adding get_xx set_xx methods, change reads and writes to the public members
to calls to get and set functionsss
old public member(int16_t) get function -> int16_t set function (int16_t)
(expression where c is an object of type RC_Channel)
c.radio_in c.get_radio_in() c.set_radio_in(v)
c.control_in c.get_control_in() c.set_control_in(v)
c.servo_out c.get_servo_out() c.set_servo_out(v)
c.pwm_out c.get_pwm_out() // use existing
c.radio_out c.get_radio_out() c.set_radio_out(v)
c.radio_max c.get_radio_max() c.set_radio_max(v)
c.radio_min c.get_radio_min() c.set_radio_min(v)
c.radio_trim c.get_radio_trim() c.set_radio_trim(v);
c.min_max_configured() // return true if min and max are configured
Because data members of RC_Channels are now private and so cannot be written directly
some overloads are provided in the Plane classes to provide the old functionality
new overload Plane::stick_mix_channel(RC_Channel *channel)
which forwards to the previously existing
void stick_mix_channel(RC_Channel *channel, int16_t &servo_out);
new overload Plane::channel_output_mixer(Rc_Channel* , RC_Channel*)const
which forwards to
(uint8_t mixing_type, int16_t & chan1, int16_t & chan2)const;
Rename functions
RC_Channel_aux::set_radio_trim(Aux_servo_function_t function)
to RC_Channel_aux::set_trim_to_radio_in_for(Aux_servo_function_t function)
RC_Channel_aux::set_servo_out(Aux_servo_function_t function, int16_t value)
to RC_Channel_aux::set_servo_out_for(Aux_servo_function_t function, int16_t value)
Rationale:
RC_Channel is a complicated class, which combines
several functionalities dealing with stick inputs
in pwm and logical units, logical and actual actuator
outputs, unit conversion etc, etc
The intent of this PR is to clarify existing use of
the class. At the basic level it should now be possible
to grep all places where private variable is set by
searching for the set_xx function.
(The wider purpose is to provide a more generic and
logically simpler method of output mixing. This is a small step)
The problem with using min() and max() is that they conflict with some
C++ headers. Name the macros in uppercase instead. We may go case by
case later converting them to be typesafe.
Changes generated with:
git ls-files '*.cpp' '*.h' -z | xargs -0 sed -i 's/\([^_[:alnum:]]\)max(/\1MAX(/g'
git ls-files '*.cpp' '*.h' -z | xargs -0 sed -i 's/\([^_[:alnum:]]\)min(/\1MIN(/g'
get_pilot_desired_lean_angles function now takes angle max parameter but
all flight modes except AltHold simply pass in the ANGLE_MAX parameter
meaning no functional change for them
Peter Barker
Michael du Breuil
Leonard Hall
Randy Mackay
Ebin
Andrew Tridgell
ChrisBird
Mathieu OTHACEHE
mirkix
skyscraper
dgrat
Jonathan Challinger
Lucas De Marchi
bugobliterator
Robert Lefebvre