Skip to content

Commit

Permalink
AP_Quicktune: optimise enum usage
Browse files Browse the repository at this point in the history
this is a separate commit in case it isn't to the taste of the
reviewer
It saves around 500 bytes
  • Loading branch information
tridge committed Oct 19, 2024
1 parent 3eac1e9 commit e88683d
Show file tree
Hide file tree
Showing 2 changed files with 102 additions and 147 deletions.
236 changes: 91 additions & 145 deletions libraries/AP_Quicktune/AP_Quicktune.cpp
Original file line number Diff line number Diff line change
Expand Up @@ -246,18 +246,15 @@ void AP_Quicktune::update(bool mode_supports_quicktune)
// We are just starting tuning, get current values
GCS_SEND_TEXT(MAV_SEVERITY_NOTICE, "Tuning: Starting tune");
// Get all params
for (int8_t pname = 0; pname < uint8_t(Param::END); pname++) {
param_saved[pname] = get_param_value(Param(pname));
for (uint8_t p = 0; p < uint8_t(Param::END); p++) {
param_saved[p] = get_param_value(Param(p));
}
// Set up SMAX
Param is[3];
is[0] = Param::RLL_SMAX;
is[1] = Param::PIT_SMAX;
is[2] = Param::YAW_SMAX;
for (uint8_t i = 0; i < 3; i++) {
float smax = get_param_value(is[i]);
const Param is[3] { Param::RLL_SMAX, Param::PIT_SMAX, Param::YAW_SMAX };
for (const auto p : is) {
float smax = get_param_value(p);
if (smax <= 0) {
adjust_gain(is[i], DEFAULT_SMAX);
adjust_gain(p, DEFAULT_SMAX);
}
}
}
Expand All @@ -271,12 +268,12 @@ void AP_Quicktune::update(bool mode_supports_quicktune)
setup_filters(axis);
}

Param pname = get_pname(axis, current_stage);
float pval = get_param_value(pname);
float limit = gain_limit(pname);
bool limited = (limit > 0.0 && pval >= limit);
float srate = get_slew_rate(axis);
bool oscillating = srate > osc_smax;
const Param pname = get_pname(axis, current_stage);
const float pval = get_param_value(pname);
const float limit = gain_limit(pname);
const bool limited = (limit > 0.0 && pval >= limit);
const float srate = get_slew_rate(axis);
const bool oscillating = srate > osc_smax;

// Check if reached limit
if (limited || oscillating) {
Expand All @@ -290,11 +287,15 @@ void AP_Quicktune::update(bool mode_supports_quicktune)
}
float old_gain = param_saved[uint8_t(pname)];
if (new_gain < old_gain && (pname == Param::PIT_D || pname == Param::RLL_D)) {
// We are lowering a D gain from the original gain. Also lower the P gain by the same amount so that we don't trigger P oscillation. We don't drop P by more than a factor of 2
float ratio = fmaxf(new_gain / old_gain, 0.5);
Param P_name = Param(uint8_t(pname)-2); //from D to P
float old_pval = get_param_value(P_name);;
float new_pval = old_pval * ratio;
// We are lowering a D gain from the original gain. Also
// lower the P gain by the same amount so that we don't
// trigger P oscillation. We don't drop P by more than a
// factor of 2
const float ratio = fmaxf(new_gain / old_gain, 0.5);
const uint8_t P_TO_D_OFS = uint8_t(Param::RLL_D) - uint8_t(Param::RLL_P);
const Param P_name = Param(uint8_t(pname)-P_TO_D_OFS); //from D to P
const float old_pval = get_param_value(P_name);;
const float new_pval = old_pval * ratio;
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "Adjusting %s %.3f -> %.3f", get_param_name(P_name), old_pval, new_pval);
adjust_gain_limited(P_name, new_pval);
}
Expand Down Expand Up @@ -355,15 +356,15 @@ void AP_Quicktune::setup_filters(AP_Quicktune::AxisName axis)
}
AP_InertialSensor *imu = AP_InertialSensor::get_singleton();
if (imu == nullptr) {
GCS_SEND_TEXT(MAV_SEVERITY_EMERGENCY, "Quicktune: can't find IMU.");
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return;
}
float gyro_filter = imu->get_gyro_filter_hz();
const float gyro_filter = imu->get_gyro_filter_hz();
adjust_gain(get_pname(axis, Stage::FLTT), gyro_filter * FLTT_MUL);
adjust_gain(get_pname(axis, Stage::FLTD), gyro_filter * FLTT_MUL);

if (axis == AxisName::YAW) {
float FLTE = get_param_value(Param::YAW_FLTE);
const float FLTE = get_param_value(Param::YAW_FLTE);
if (FLTE < 0.0 || FLTE > YAW_FLTE_MAX) {
adjust_gain(Param::YAW_FLTE, YAW_FLTE_MAX);
}
Expand All @@ -375,9 +376,9 @@ void AP_Quicktune::setup_filters(AP_Quicktune::AxisName axis)
bool AP_Quicktune::have_pilot_input()
{
const auto &rcmap = *AP::rcmap();
float roll = rc().rc_channel(rcmap.roll()-1)->norm_input_dz();
float pitch = rc().rc_channel(rcmap.pitch()-1)->norm_input_dz();
float yaw = rc().rc_channel(rcmap.yaw()-1)->norm_input_dz();
const float roll = rc().rc_channel(rcmap.roll()-1)->norm_input_dz();
const float pitch = rc().rc_channel(rcmap.pitch()-1)->norm_input_dz();
const float yaw = rc().rc_channel(rcmap.yaw()-1)->norm_input_dz();

if (fabsf(roll) > 0 || fabsf(pitch) > 0 || fabsf(yaw) > 0) {
return true;
Expand All @@ -396,20 +397,32 @@ AP_Quicktune::AxisName AP_Quicktune::get_current_axis()
return AxisName::DONE;
}

float AP_Quicktune::get_slew_rate(AP_Quicktune::AxisName axis)
// get the AC_PID object for an axis
AC_PID *AP_Quicktune::get_axis_pid(AP_Quicktune::AxisName axis)
{
auto &attitude_control = *AC_AttitudeControl::get_singleton();
switch(axis) {
case AxisName::RLL:
return attitude_control.get_rate_roll_pid().get_pid_info().slew_rate;
return &attitude_control.get_rate_roll_pid();
case AxisName::PIT:
return attitude_control.get_rate_pitch_pid().get_pid_info().slew_rate;
return &attitude_control.get_rate_pitch_pid();
case AxisName::YAW:
return attitude_control.get_rate_yaw_pid().get_pid_info().slew_rate;
return &attitude_control.get_rate_yaw_pid();
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return 0.0;
break;
}
return nullptr;
}

// get slew rate parameter for an axis
float AP_Quicktune::get_slew_rate(AP_Quicktune::AxisName axis)
{
auto *pid = get_axis_pid(axis);
if (pid == nullptr) {
return 0;
}
return pid->get_pid_info().slew_rate;
}

// Move to next stage of tune
Expand All @@ -432,8 +445,10 @@ void AP_Quicktune::adjust_gain(AP_Quicktune::Param param, float value)

if (get_stage(param) == Stage::P) {
// Also change I gain
Param iname = Param(uint8_t(param)+1);
Param ffname = Param(uint8_t(param)+7);
const uint8_t P_TO_I_OFS = uint8_t(Param::RLL_I) - uint8_t(Param::RLL_P);
const uint8_t P_TO_FF_OFS = uint8_t(Param::RLL_FF) - uint8_t(Param::RLL_P);
const Param iname = Param(uint8_t(param)+P_TO_I_OFS);
const Param ffname = Param(uint8_t(param)+P_TO_FF_OFS);
float FF = get_param_value(ffname);
if (FF > 0) {
// If we have any FF on an axis then we don't couple I to P,
Expand Down Expand Up @@ -461,10 +476,10 @@ void AP_Quicktune::adjust_gain_limited(AP_Quicktune::Param param, float value)

float AP_Quicktune::limit_gain(AP_Quicktune::Param param, float value)
{
float saved_value = param_saved[uint8_t(param)];
const float saved_value = param_saved[uint8_t(param)];
if (reduce_max >= 0 && reduce_max < 100 && saved_value > 0) {
// Check if we exceeded gain reduction
float reduction_pct = 100.0 * (saved_value - value) / saved_value;
const float reduction_pct = 100.0 * (saved_value - value) / saved_value;
if (reduction_pct > reduce_max) {
float new_value = saved_value * (100 - reduce_max) * 0.01;
GCS_SEND_TEXT(MAV_SEVERITY_INFO, "Limiting %s %.3f -> %.3f", get_param_name(param), value, new_value);
Expand Down Expand Up @@ -509,78 +524,41 @@ float AP_Quicktune::get_gain_mul()

void AP_Quicktune::restore_all_params()
{
for (int8_t pname = 0; pname < uint8_t(Param::END); pname++) {
if (BIT_IS_SET(param_changed, pname)) {
set_param_value(Param(pname), param_saved[pname]);
BIT_CLEAR(param_changed, pname);
for (uint8_t p = 0; p < uint8_t(Param::END); p++) {
const auto param = Param(p);
if (BIT_IS_SET(param_changed, p)) {
set_param_value(param, param_saved[p]);
BIT_CLEAR(param_changed, p);
}
}
}

void AP_Quicktune::save_all_params()
{
// for pname in pairs(params) do
for (int8_t pname = 0; pname < uint8_t(Param::END); pname++) {
if (BIT_IS_SET(param_changed, pname)) {
set_and_save_param_value(Param(pname), get_param_value(Param(pname)));
param_saved[pname] = get_param_value(Param(pname));
BIT_CLEAR(param_changed, pname);
}
for (uint8_t p = 0; p < uint8_t(Param::END); p++) {
const auto param = Param(p);
set_and_save_param_value(param, get_param_value(param));
param_saved[p] = get_param_value(param);
BIT_CLEAR(param_changed, p);
}
}

AP_Quicktune::Param AP_Quicktune::get_pname(AP_Quicktune::AxisName axis, AP_Quicktune::Stage stage)
{
switch (axis)
const uint8_t axis_offset = uint8_t(axis) * param_per_axis;
switch (stage)
{
case AxisName::RLL:
switch (stage)
{
case Stage::P:
return Param::RLL_P;
case Stage::D:
return Param::RLL_D;
case Stage::FLTT:
return Param::RLL_FLTT;
case Stage::FLTD:
return Param::RLL_FLTD;
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return Param::END;
}
case AxisName::PIT:
switch (stage)
{
case Stage::P:
return Param::PIT_P;
case Stage::D:
return Param::PIT_D;
case Stage::FLTT:
return Param::PIT_FLTT;
case Stage::FLTD:
return Param::PIT_FLTD;
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return Param::END;
}
case AxisName::YAW:
switch (stage)
{
case Stage::P:
return Param::YAW_P;
case Stage::D:
return Param::YAW_D;
case Stage::FLTT:
return Param::YAW_FLTT;
case Stage::FLTD:
return Param::YAW_FLTD;
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return Param::END;
}
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return Param::END;
case Stage::P:
return Param(uint8_t(Param::RLL_P) + axis_offset);
case Stage::D:
return Param(uint8_t(Param::RLL_D) + axis_offset);
case Stage::FLTT:
return Param(uint8_t(Param::RLL_FLTT) + axis_offset);
case Stage::FLTD:
return Param(uint8_t(Param::RLL_FLTD) + axis_offset);
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return Param::END;
}
}

Expand All @@ -595,57 +573,30 @@ AP_Quicktune::Stage AP_Quicktune::get_stage(AP_Quicktune::Param param)

AP_Float *AP_Quicktune::get_param_pointer(AP_Quicktune::Param param)
{
auto &attitude_control = *AC_AttitudeControl::get_singleton();
switch (param)
const AxisName axis = AxisName(uint8_t(param) / param_per_axis);
auto *pid = get_axis_pid(axis);
if (pid == nullptr) {
return nullptr;
}
const Param roll_param = Param(uint8_t(param) % param_per_axis);
switch (roll_param)
{
case Param::RLL_P:
return &attitude_control.get_rate_roll_pid().kP();
return &pid->kP();
case Param::RLL_I:
return &attitude_control.get_rate_roll_pid().kI();
return &pid->kI();
case Param::RLL_D:
return &attitude_control.get_rate_roll_pid().kD();
return &pid->kD();
case Param::RLL_SMAX:
return &attitude_control.get_rate_roll_pid().slew_limit();
return &pid->slew_limit();
case Param::RLL_FLTT:
return &attitude_control.get_rate_roll_pid().filt_T_hz();
return &pid->filt_T_hz();
case Param::RLL_FLTD:
return &attitude_control.get_rate_roll_pid().filt_D_hz();
return &pid->filt_D_hz();
case Param::RLL_FLTE:
return &attitude_control.get_rate_roll_pid().filt_E_hz();
return &pid->filt_E_hz();
case Param::RLL_FF:
return &attitude_control.get_rate_roll_pid().ff();
case Param::PIT_P:
return &attitude_control.get_rate_pitch_pid().kP();
case Param::PIT_I:
return &attitude_control.get_rate_pitch_pid().kI();
case Param::PIT_D:
return &attitude_control.get_rate_pitch_pid().kD();
case Param::PIT_SMAX:
return &attitude_control.get_rate_pitch_pid().slew_limit();
case Param::PIT_FLTT:
return &attitude_control.get_rate_pitch_pid().filt_T_hz();
case Param::PIT_FLTD:
return &attitude_control.get_rate_pitch_pid().filt_D_hz();
case Param::PIT_FLTE:
return &attitude_control.get_rate_pitch_pid().filt_E_hz();
case Param::PIT_FF:
return &attitude_control.get_rate_pitch_pid().ff();
case Param::YAW_P:
return &attitude_control.get_rate_yaw_pid().kP();
case Param::YAW_I:
return &attitude_control.get_rate_yaw_pid().kI();
case Param::YAW_D:
return &attitude_control.get_rate_yaw_pid().kD();
case Param::YAW_SMAX:
return &attitude_control.get_rate_yaw_pid().slew_limit();
case Param::YAW_FLTT:
return &attitude_control.get_rate_yaw_pid().filt_T_hz();
case Param::YAW_FLTD:
return &attitude_control.get_rate_yaw_pid().filt_D_hz();
case Param::YAW_FLTE:
return &attitude_control.get_rate_yaw_pid().filt_E_hz();
case Param::YAW_FF:
return &attitude_control.get_rate_roll_pid().ff();
return &pid->ff();
default:
INTERNAL_ERROR(AP_InternalError::error_t::flow_of_control);
return nullptr;
Expand Down Expand Up @@ -686,15 +637,10 @@ void AP_Quicktune::set_and_save_param_value(AP_Quicktune::Param param, float val

AP_Quicktune::AxisName AP_Quicktune::get_axis(AP_Quicktune::Param param)
{
if (param < Param::PIT_P) {
return AxisName::RLL;
} else if (param < Param::YAW_P) {
return AxisName::PIT;
} else if (param < Param::END) {
return AxisName::YAW;
} else {
if (param >= Param::END) {
return AxisName::END;
}
return AxisName(uint8_t(param) / param_per_axis);
}

const char* AP_Quicktune::get_axis_name(AP_Quicktune::AxisName axis)
Expand Down Expand Up @@ -723,7 +669,7 @@ float AP_Quicktune::gain_limit(AP_Quicktune::Param param)
return yaw_d_max;
}
}
return 0.0;
return 0.0;
}


Expand Down
Loading

0 comments on commit e88683d

Please sign in to comment.