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AC_AttitudeControl: use AC_PID defaults to tidy rate Sub PID initialisation

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makes it look like multi ie. legible
This commit is contained in:
Peter Barker 2024-09-20 17:17:43 +10:00 committed by Andrew Tridgell
parent 4d7b94c3cb
commit 6a74a97bf7
2 changed files with 34 additions and 7 deletions
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5
libraries/AC_AttitudeControl/AC_AttitudeControl_Sub.cpp
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@ -336,10 +336,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Sub::var_info[] = {
AC_AttitudeControl_Sub::AC_AttitudeControl_Sub(AP_AHRS_View &ahrs, const AP_MultiCopter &aparm, AP_MotorsMulticopter& motors) : AC_AttitudeControl_Sub::AC_AttitudeControl_Sub(AP_AHRS_View &ahrs, const AP_MultiCopter &aparm, AP_MotorsMulticopter& motors) :
AC_AttitudeControl(ahrs, aparm, motors), AC_AttitudeControl(ahrs, aparm, motors),
_motors_multi(motors), _motors_multi(motors)
_pid_rate_roll(AC_ATC_SUB_RATE_RP_P, AC_ATC_SUB_RATE_RP_I, AC_ATC_SUB_RATE_RP_D, 0.0f, AC_ATC_SUB_RATE_RP_IMAX, AC_ATC_SUB_RATE_RP_FILT_HZ, 0.0f, AC_ATC_SUB_RATE_RP_FILT_HZ),
_pid_rate_pitch(AC_ATC_SUB_RATE_RP_P, AC_ATC_SUB_RATE_RP_I, AC_ATC_SUB_RATE_RP_D, 0.0f, AC_ATC_SUB_RATE_RP_IMAX, AC_ATC_SUB_RATE_RP_FILT_HZ, 0.0f, AC_ATC_SUB_RATE_RP_FILT_HZ),
_pid_rate_yaw(AC_ATC_SUB_RATE_YAW_P, AC_ATC_SUB_RATE_YAW_I, AC_ATC_SUB_RATE_YAW_D, 0.0f, AC_ATC_SUB_RATE_YAW_IMAX, AC_ATC_SUB_RATE_YAW_FILT_HZ, 0.0f, AC_ATC_SUB_RATE_YAW_FILT_HZ)
{ {
AP_Param::setup_object_defaults(this, var_info); AP_Param::setup_object_defaults(this, var_info);

36
libraries/AC_AttitudeControl/AC_AttitudeControl_Sub.h
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@ -83,9 +83,39 @@ protected:
float get_throttle_avg_max(float throttle_in); float get_throttle_avg_max(float throttle_in);
AP_MotorsMulticopter& _motors_multi; AP_MotorsMulticopter& _motors_multi;
AC_PID _pid_rate_roll;
AC_PID _pid_rate_pitch; // Roll and Pitch rate PIDs share the same defaults:
AC_PID _pid_rate_yaw; const AC_PID::Defaults rp_defaults {
AC_PID::Defaults{
.p = AC_ATC_SUB_RATE_RP_P,
.i = AC_ATC_SUB_RATE_RP_I,
.d = AC_ATC_SUB_RATE_RP_D,
.ff = 0.0f,
.imax = AC_ATC_SUB_RATE_RP_IMAX,
.filt_T_hz = AC_ATC_SUB_RATE_RP_FILT_HZ,
.filt_E_hz = 0.0,
.filt_D_hz = AC_ATC_SUB_RATE_RP_FILT_HZ,
.srmax = 0,
.srtau = 1.0
}
};
AC_PID _pid_rate_roll { rp_defaults };
AC_PID _pid_rate_pitch { rp_defaults };
AC_PID _pid_rate_yaw {
AC_PID::Defaults{
.p = AC_ATC_SUB_RATE_YAW_P,
.i = AC_ATC_SUB_RATE_YAW_I,
.d = AC_ATC_SUB_RATE_YAW_D,
.ff = 0.0f,
.imax = AC_ATC_SUB_RATE_YAW_IMAX,
.filt_T_hz = AC_ATC_SUB_RATE_YAW_FILT_HZ,
.filt_E_hz = 0.0f,
.filt_D_hz = AC_ATC_SUB_RATE_YAW_FILT_HZ,
.srmax = 0,
.srtau = 1.0
}
};
AP_Float _thr_mix_man; // throttle vs attitude control prioritisation used when using manual throttle (higher values mean we prioritise attitude control over throttle) AP_Float _thr_mix_man; // throttle vs attitude control prioritisation used when using manual throttle (higher values mean we prioritise attitude control over throttle)
AP_Float _thr_mix_min; // throttle vs attitude control prioritisation used when landing (higher values mean we prioritise attitude control over throttle) AP_Float _thr_mix_min; // throttle vs attitude control prioritisation used when landing (higher values mean we prioritise attitude control over throttle)