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betaflight/src/main/fc/rc_adjustments.c
Bruce Luckcuck c06106e2d1 Split initialization from pid.c for flash savings
Move low performance requirements initialization code into pid_init.c and optimize that for size.

Saves 2688 bytes for target STM32F7X2.
2020-05-03 13:58:55 -04:00

868 lines
33 KiB
C

/*
* This file is part of Cleanflight and Betaflight.
*
* Cleanflight and Betaflight are free software. You can redistribute
* this software and/or modify this software under the terms of the
* GNU General Public License as published by the Free Software
* Foundation, either version 3 of the License, or (at your option)
* any later version.
*
* Cleanflight and Betaflight are distributed in the hope that they
* will be useful, but WITHOUT ANY WARRANTY; without even the implied
* warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.
* See the GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with this software.
*
* If not, see <http://www.gnu.org/licenses/>.
*/
#include <stdbool.h>
#include <stdint.h>
#include <string.h>
#include <math.h>
#include "platform.h"
#include "blackbox/blackbox.h"
#include "blackbox/blackbox_fielddefs.h"
#include "build/build_config.h"
#include "common/axis.h"
#include "common/maths.h"
#include "common/utils.h"
#include "config/feature.h"
#include "drivers/time.h"
#include "config/config.h"
#include "fc/controlrate_profile.h"
#include "fc/rc_controls.h"
#include "fc/rc.h"
#include "flight/pid.h"
#include "flight/pid_init.h"
#include "io/beeper.h"
#include "io/ledstrip.h"
#include "io/motors.h"
#include "io/pidaudio.h"
#include "osd/osd.h"
#include "pg/pg.h"
#include "pg/pg_ids.h"
#include "pg/rx.h"
#include "rx/rx.h"
#include "rc_adjustments.h"
#define ADJUSTMENT_RANGE_COUNT_INVALID -1
PG_REGISTER_ARRAY(adjustmentRange_t, MAX_ADJUSTMENT_RANGE_COUNT, adjustmentRanges, PG_ADJUSTMENT_RANGE_CONFIG, 2);
uint8_t pidAudioPositionToModeMap[7] = {
// on a pot with a center detent, it's easy to have center area for off/default, then three positions to the left and three to the right.
// current implementation yields RC values as below.
PID_AUDIO_PIDSUM_X, // 900 - ~1071 - Min
PID_AUDIO_PIDSUM_Y, // ~1071 - ~1242
PID_AUDIO_PIDSUM_XY, // ~1242 - ~1414
PID_AUDIO_OFF, // ~1414 - ~1585 - Center
PID_AUDIO_OFF, // ~1585 - ~1757
PID_AUDIO_OFF, // ~1757 - ~1928
PID_AUDIO_OFF, // ~1928 - 2100 - Max
// Note: Last 3 positions are currently pending implementations and use PID_AUDIO_OFF for now.
};
STATIC_UNIT_TESTED int stepwiseAdjustmentCount = ADJUSTMENT_RANGE_COUNT_INVALID;
STATIC_UNIT_TESTED timedAdjustmentState_t stepwiseAdjustments[MAX_ADJUSTMENT_RANGE_COUNT];
STATIC_UNIT_TESTED int continuosAdjustmentCount;
STATIC_UNIT_TESTED continuosAdjustmentState_t continuosAdjustments[MAX_ADJUSTMENT_RANGE_COUNT];
static void blackboxLogInflightAdjustmentEvent(adjustmentFunction_e adjustmentFunction, int32_t newValue)
{
#ifndef USE_BLACKBOX
UNUSED(adjustmentFunction);
UNUSED(newValue);
#else
if (blackboxConfig()->device) {
flightLogEvent_inflightAdjustment_t eventData;
eventData.adjustmentFunction = adjustmentFunction;
eventData.newValue = newValue;
eventData.floatFlag = false;
blackboxLogEvent(FLIGHT_LOG_EVENT_INFLIGHT_ADJUSTMENT, (flightLogEventData_t*)&eventData);
}
#endif
}
// sync with adjustmentFunction_e
static const adjustmentConfig_t defaultAdjustmentConfigs[ADJUSTMENT_FUNCTION_COUNT - 1] = {
{
.adjustmentFunction = ADJUSTMENT_RC_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_RC_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_THROTTLE_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_YAW_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_YAW_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_YAW_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_YAW_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_RATE_PROFILE,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .switchPositions = 3 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_RC_RATE_YAW,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_F,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_FEEDFORWARD_TRANSITION,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_HORIZON_STRENGTH,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .switchPositions = 255 }
}, {
.adjustmentFunction = ADJUSTMENT_PID_AUDIO,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .switchPositions = ARRAYLEN(pidAudioPositionToModeMap) }
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_F,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_F,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_YAW_F,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .step = 1 }
}, {
.adjustmentFunction = ADJUSTMENT_OSD_PROFILE,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .switchPositions = 3 }
}, {
.adjustmentFunction = ADJUSTMENT_LED_PROFILE,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .switchPositions = 3 }
}
};
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
static const char * const adjustmentLabels[] = {
"RC RATE",
"RC EXPO",
"THROTTLE EXPO",
"ROLL RATE",
"YAW RATE",
"PITCH/ROLL P",
"PITCH/ROLL I",
"PITCH/ROLL D",
"YAW P",
"YAW I",
"YAW D",
"RATE PROFILE",
"PITCH RATE",
"ROLL RATE",
"PITCH P",
"PITCH I",
"PITCH D",
"ROLL P",
"ROLL I",
"ROLL D",
"RC RATE YAW",
"PITCH/ROLL F",
"FF TRANSITION",
"HORIZON STRENGTH",
"ROLL RC RATE",
"PITCH RC RATE",
"ROLL RC EXPO",
"PITCH RC EXPO",
"PID AUDIO",
"PITCH F",
"ROLL F",
"YAW F",
"OSD PROFILE",
};
static int adjustmentRangeNameIndex = 0;
static int adjustmentRangeValue = -1;
#endif
static int applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustmentFunction, int delta)
{
beeperConfirmationBeeps(delta > 0 ? 2 : 1);
int newValue;
switch (adjustmentFunction) {
case ADJUSTMENT_RC_RATE:
case ADJUSTMENT_ROLL_RC_RATE:
newValue = constrain((int)controlRateConfig->rcRates[FD_ROLL] + delta, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RC_RATE, newValue);
if (adjustmentFunction == ADJUSTMENT_ROLL_RC_RATE) {
break;
}
// fall through for combined ADJUSTMENT_RC_EXPO
FALLTHROUGH;
case ADJUSTMENT_PITCH_RC_RATE:
newValue = constrain((int)controlRateConfig->rcRates[FD_PITCH] + delta, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RC_RATE, newValue);
break;
case ADJUSTMENT_RC_EXPO:
case ADJUSTMENT_ROLL_RC_EXPO:
newValue = constrain((int)controlRateConfig->rcExpo[FD_ROLL] + delta, 0, CONTROL_RATE_CONFIG_RC_EXPO_MAX);
controlRateConfig->rcExpo[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RC_EXPO, newValue);
if (adjustmentFunction == ADJUSTMENT_ROLL_RC_EXPO) {
break;
}
// fall through for combined ADJUSTMENT_RC_EXPO
FALLTHROUGH;
case ADJUSTMENT_PITCH_RC_EXPO:
newValue = constrain((int)controlRateConfig->rcExpo[FD_PITCH] + delta, 0, CONTROL_RATE_CONFIG_RC_EXPO_MAX);
controlRateConfig->rcExpo[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RC_EXPO, newValue);
break;
case ADJUSTMENT_THROTTLE_EXPO:
newValue = constrain((int)controlRateConfig->thrExpo8 + delta, 0, 100); // FIXME magic numbers repeated in cli.c
controlRateConfig->thrExpo8 = newValue;
initRcProcessing();
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_THROTTLE_EXPO, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_RATE:
case ADJUSTMENT_PITCH_RATE:
newValue = constrain((int)controlRateConfig->rates[FD_PITCH] + delta, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RATE, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_RATE) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_RATE
FALLTHROUGH;
case ADJUSTMENT_ROLL_RATE:
newValue = constrain((int)controlRateConfig->rates[FD_ROLL] + delta, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RATE, newValue);
break;
case ADJUSTMENT_YAW_RATE:
newValue = constrain((int)controlRateConfig->rates[FD_YAW] + delta, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_YAW] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_RATE, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_P:
case ADJUSTMENT_PITCH_P:
newValue = constrain((int)currentPidProfile->pid[PID_PITCH].P + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_P, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_P) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_P
FALLTHROUGH;
case ADJUSTMENT_ROLL_P:
newValue = constrain((int)currentPidProfile->pid[PID_ROLL].P + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_P, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_I:
case ADJUSTMENT_PITCH_I:
newValue = constrain((int)currentPidProfile->pid[PID_PITCH].I + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_I, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_I) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_I
FALLTHROUGH;
case ADJUSTMENT_ROLL_I:
newValue = constrain((int)currentPidProfile->pid[PID_ROLL].I + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_I, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_D:
case ADJUSTMENT_PITCH_D:
newValue = constrain((int)currentPidProfile->pid[PID_PITCH].D + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_D, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_D) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_D
FALLTHROUGH;
case ADJUSTMENT_ROLL_D:
newValue = constrain((int)currentPidProfile->pid[PID_ROLL].D + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_D, newValue);
break;
case ADJUSTMENT_YAW_P:
newValue = constrain((int)currentPidProfile->pid[PID_YAW].P + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_P, newValue);
break;
case ADJUSTMENT_YAW_I:
newValue = constrain((int)currentPidProfile->pid[PID_YAW].I + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_I, newValue);
break;
case ADJUSTMENT_YAW_D:
newValue = constrain((int)currentPidProfile->pid[PID_YAW].D + delta, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_D, newValue);
break;
case ADJUSTMENT_RC_RATE_YAW:
newValue = constrain((int)controlRateConfig->rcRates[FD_YAW] + delta, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_YAW] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_RC_RATE_YAW, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_F:
case ADJUSTMENT_PITCH_F:
newValue = constrain(currentPidProfile->pid[PID_PITCH].F + delta, 0, 2000);
currentPidProfile->pid[PID_PITCH].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_F, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_F) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_F
FALLTHROUGH;
case ADJUSTMENT_ROLL_F:
newValue = constrain(currentPidProfile->pid[PID_ROLL].F + delta, 0, 2000);
currentPidProfile->pid[PID_ROLL].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_F, newValue);
break;
case ADJUSTMENT_YAW_F:
newValue = constrain(currentPidProfile->pid[PID_YAW].F + delta, 0, 2000);
currentPidProfile->pid[PID_YAW].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_F, newValue);
break;
case ADJUSTMENT_FEEDFORWARD_TRANSITION:
newValue = constrain(currentPidProfile->feedForwardTransition + delta, 1, 100); // FIXME magic numbers repeated in cli.c
currentPidProfile->feedForwardTransition = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_FEEDFORWARD_TRANSITION, newValue);
break;
default:
newValue = -1;
break;
};
return newValue;
}
static int applyAbsoluteAdjustment(controlRateConfig_t *controlRateConfig, adjustmentFunction_e adjustmentFunction, int value)
{
int newValue;
switch (adjustmentFunction) {
case ADJUSTMENT_RC_RATE:
case ADJUSTMENT_ROLL_RC_RATE:
newValue = constrain(value, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RC_RATE, newValue);
if (adjustmentFunction == ADJUSTMENT_ROLL_RC_RATE) {
break;
}
// fall through for combined ADJUSTMENT_RC_EXPO
FALLTHROUGH;
case ADJUSTMENT_PITCH_RC_RATE:
newValue = constrain(value, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RC_RATE, newValue);
break;
case ADJUSTMENT_RC_EXPO:
case ADJUSTMENT_ROLL_RC_EXPO:
newValue = constrain(value, 1, CONTROL_RATE_CONFIG_RC_EXPO_MAX);
controlRateConfig->rcExpo[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RC_EXPO, newValue);
if (adjustmentFunction == ADJUSTMENT_ROLL_RC_EXPO) {
break;
}
// fall through for combined ADJUSTMENT_RC_EXPO
FALLTHROUGH;
case ADJUSTMENT_PITCH_RC_EXPO:
newValue = constrain(value, 0, CONTROL_RATE_CONFIG_RC_EXPO_MAX);
controlRateConfig->rcExpo[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RC_EXPO, newValue);
break;
case ADJUSTMENT_THROTTLE_EXPO:
newValue = constrain(value, 0, 100); // FIXME magic numbers repeated in cli.c
controlRateConfig->thrExpo8 = newValue;
initRcProcessing();
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_THROTTLE_EXPO, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_RATE:
case ADJUSTMENT_PITCH_RATE:
newValue = constrain(value, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_PITCH] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RATE, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_RATE) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_RATE
FALLTHROUGH;
case ADJUSTMENT_ROLL_RATE:
newValue = constrain(value, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_ROLL] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RATE, newValue);
break;
case ADJUSTMENT_YAW_RATE:
newValue = constrain(value, 0, CONTROL_RATE_CONFIG_RATE_MAX);
controlRateConfig->rates[FD_YAW] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_RATE, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_P:
case ADJUSTMENT_PITCH_P:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_P, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_P) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_P
FALLTHROUGH;
case ADJUSTMENT_ROLL_P:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_P, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_I:
case ADJUSTMENT_PITCH_I:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_I, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_I) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_I
FALLTHROUGH;
case ADJUSTMENT_ROLL_I:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_I, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_D:
case ADJUSTMENT_PITCH_D:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_PITCH].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_D, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_D) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_D
FALLTHROUGH;
case ADJUSTMENT_ROLL_D:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_ROLL].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_D, newValue);
break;
case ADJUSTMENT_YAW_P:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].P = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_P, newValue);
break;
case ADJUSTMENT_YAW_I:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].I = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_I, newValue);
break;
case ADJUSTMENT_YAW_D:
newValue = constrain(value, 0, 200); // FIXME magic numbers repeated in cli.c
currentPidProfile->pid[PID_YAW].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_D, newValue);
break;
case ADJUSTMENT_RC_RATE_YAW:
newValue = constrain(value, 1, CONTROL_RATE_CONFIG_RC_RATES_MAX);
controlRateConfig->rcRates[FD_YAW] = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_RC_RATE_YAW, newValue);
break;
case ADJUSTMENT_PITCH_ROLL_F:
case ADJUSTMENT_PITCH_F:
newValue = constrain(value, 0, 2000);
currentPidProfile->pid[PID_PITCH].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_F, newValue);
if (adjustmentFunction == ADJUSTMENT_PITCH_F) {
break;
}
// fall through for combined ADJUSTMENT_PITCH_ROLL_F
FALLTHROUGH;
case ADJUSTMENT_ROLL_F:
newValue = constrain(value, 0, 2000);
currentPidProfile->pid[PID_ROLL].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_F, newValue);
break;
case ADJUSTMENT_YAW_F:
newValue = constrain(value, 0, 2000);
currentPidProfile->pid[PID_YAW].F = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_F, newValue);
break;
case ADJUSTMENT_FEEDFORWARD_TRANSITION:
newValue = constrain(value, 1, 100); // FIXME magic numbers repeated in cli.c
currentPidProfile->feedForwardTransition = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_FEEDFORWARD_TRANSITION, newValue);
break;
default:
newValue = -1;
break;
};
return newValue;
}
static uint8_t applySelectAdjustment(adjustmentFunction_e adjustmentFunction, uint8_t position)
{
uint8_t beeps = 0;
switch (adjustmentFunction) {
case ADJUSTMENT_RATE_PROFILE:
if (getCurrentControlRateProfileIndex() != position) {
changeControlRateProfile(position);
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_RATE_PROFILE, position);
beeps = position + 1;
}
break;
case ADJUSTMENT_HORIZON_STRENGTH:
{
uint8_t newValue = constrain(position, 0, 200); // FIXME magic numbers repeated in serial_cli.c
if (currentPidProfile->pid[PID_LEVEL].D != newValue) {
beeps = ((newValue - currentPidProfile->pid[PID_LEVEL].D) / 8) + 1;
currentPidProfile->pid[PID_LEVEL].D = newValue;
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_HORIZON_STRENGTH, position);
}
}
break;
case ADJUSTMENT_PID_AUDIO:
#ifdef USE_PID_AUDIO
{
pidAudioModes_e newMode = pidAudioPositionToModeMap[position];
if (newMode != pidAudioGetMode()) {
pidAudioSetMode(newMode);
}
}
#endif
break;
case ADJUSTMENT_OSD_PROFILE:
#ifdef USE_OSD_PROFILES
if (getCurrentOsdProfileIndex() != (position + 1)) {
changeOsdProfileIndex(position+1);
}
#endif
break;
case ADJUSTMENT_LED_PROFILE:
#ifdef USE_LED_STRIP
if (getLedProfile() != position) {
setLedProfile(position);
}
#endif
break;
default:
break;
}
if (beeps) {
beeperConfirmationBeeps(beeps);
}
return position;
}
#define ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET 1
static void calcActiveAdjustmentRanges(void)
{
adjustmentRange_t defaultAdjustmentRange;
memset(&defaultAdjustmentRange, 0, sizeof(defaultAdjustmentRange));
stepwiseAdjustmentCount = 0;
continuosAdjustmentCount = 0;
for (int i = 0; i < MAX_ADJUSTMENT_RANGE_COUNT; i++) {
const adjustmentRange_t * const adjustmentRange = adjustmentRanges(i);
if (memcmp(adjustmentRange, &defaultAdjustmentRange, sizeof(defaultAdjustmentRange)) != 0) {
const adjustmentConfig_t *adjustmentConfig = &defaultAdjustmentConfigs[adjustmentRange->adjustmentConfig - ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET];
if (adjustmentRange->adjustmentCenter == 0 && adjustmentConfig->mode != ADJUSTMENT_MODE_SELECT) {
timedAdjustmentState_t *adjustmentState = &stepwiseAdjustments[stepwiseAdjustmentCount++];
adjustmentState->adjustmentRangeIndex = i;
adjustmentState->timeoutAt = 0;
adjustmentState->ready = true;
} else {
continuosAdjustmentState_t *adjustmentState = &continuosAdjustments[continuosAdjustmentCount++];
adjustmentState->adjustmentRangeIndex = i;
adjustmentState->lastRcData = 0;
}
}
}
}
#define VALUE_DISPLAY_LATENCY_MS 2000
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
static void updateOsdAdjustmentData(int newValue, adjustmentFunction_e adjustmentFunction)
{
static timeMs_t lastValueChangeMs;
timeMs_t currentTimeMs = millis();
if (newValue != -1
&& adjustmentFunction != ADJUSTMENT_RATE_PROFILE // Rate profile already has an OSD element
#ifdef USE_OSD_PROFILES
&& adjustmentFunction != ADJUSTMENT_OSD_PROFILE
#endif
) {
adjustmentRangeNameIndex = adjustmentFunction;
adjustmentRangeValue = newValue;
lastValueChangeMs = currentTimeMs;
}
if (cmp32(currentTimeMs, lastValueChangeMs + VALUE_DISPLAY_LATENCY_MS) >= 0) {
adjustmentRangeNameIndex = 0;
}
}
#endif
#define RESET_FREQUENCY_2HZ (1000 / 2)
static void processStepwiseAdjustments(controlRateConfig_t *controlRateConfig, const bool canUseRxData)
{
const timeMs_t now = millis();
for (int index = 0; index < stepwiseAdjustmentCount; index++) {
timedAdjustmentState_t *adjustmentState = &stepwiseAdjustments[index];
const adjustmentRange_t *const adjustmentRange = adjustmentRanges(adjustmentState->adjustmentRangeIndex);
const adjustmentConfig_t *adjustmentConfig = &defaultAdjustmentConfigs[adjustmentRange->adjustmentConfig - ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET];
const adjustmentFunction_e adjustmentFunction = adjustmentConfig->adjustmentFunction;
if (!isRangeActive(adjustmentRange->auxChannelIndex, &adjustmentRange->range) ||
adjustmentFunction == ADJUSTMENT_NONE) {
adjustmentState->timeoutAt = 0;
continue;
}
if (cmp32(now, adjustmentState->timeoutAt) >= 0) {
adjustmentState->timeoutAt = now + RESET_FREQUENCY_2HZ;
adjustmentState->ready = true;
}
if (!canUseRxData) {
continue;
}
const uint8_t channelIndex = NON_AUX_CHANNEL_COUNT + adjustmentRange->auxSwitchChannelIndex;
if (adjustmentConfig->mode == ADJUSTMENT_MODE_STEP) {
int delta;
if (rcData[channelIndex] > rxConfig()->midrc + 200) {
delta = adjustmentConfig->data.step;
} else if (rcData[channelIndex] < rxConfig()->midrc - 200) {
delta = -adjustmentConfig->data.step;
} else {
// returning the switch to the middle immediately resets the ready state
adjustmentState->ready = true;
adjustmentState->timeoutAt = now + RESET_FREQUENCY_2HZ;
continue;
}
if (!adjustmentState->ready) {
continue;
}
int newValue = applyStepAdjustment(controlRateConfig, adjustmentFunction, delta);
setConfigDirty();
pidInitConfig(currentPidProfile);
adjustmentState->ready = false;
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
updateOsdAdjustmentData(newValue, adjustmentConfig->adjustmentFunction);
#else
UNUSED(newValue);
#endif
}
}
}
static void setConfigDirtyIfNotPermanent(const channelRange_t *range)
{
if (!(range->startStep == MIN_MODE_RANGE_STEP && range->endStep == MAX_MODE_RANGE_STEP)) {
// Only set the configuration dirty if this range is NOT permanently enabled (and the config thus never used).
setConfigDirty();
}
}
static void processContinuosAdjustments(controlRateConfig_t *controlRateConfig)
{
for (int i = 0; i < continuosAdjustmentCount; i++) {
continuosAdjustmentState_t *adjustmentState = &continuosAdjustments[i];
const adjustmentRange_t * const adjustmentRange = adjustmentRanges(adjustmentState->adjustmentRangeIndex);
const uint8_t channelIndex = NON_AUX_CHANNEL_COUNT + adjustmentRange->auxSwitchChannelIndex;
const adjustmentConfig_t *adjustmentConfig = &defaultAdjustmentConfigs[adjustmentRange->adjustmentConfig - ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET];
const adjustmentFunction_e adjustmentFunction = adjustmentConfig->adjustmentFunction;
if (isRangeActive(adjustmentRange->auxChannelIndex, &adjustmentRange->range) &&
adjustmentFunction != ADJUSTMENT_NONE) {
if (rcData[channelIndex] != adjustmentState->lastRcData) {
int newValue = -1;
if (adjustmentConfig->mode == ADJUSTMENT_MODE_SELECT) {
int switchPositions = adjustmentConfig->data.switchPositions;
if (adjustmentFunction == ADJUSTMENT_RATE_PROFILE && systemConfig()->rateProfile6PosSwitch) {
switchPositions = 6;
}
const uint16_t rangeWidth = (2100 - 900) / switchPositions;
const uint8_t position = (constrain(rcData[channelIndex], 900, 2100 - 1) - 900) / rangeWidth;
newValue = applySelectAdjustment(adjustmentFunction, position);
setConfigDirtyIfNotPermanent(&adjustmentRange->range);
} else {
// If setting is defined for step adjustment and center value has been specified, apply values directly (scaled) from aux channel
if (adjustmentRange->adjustmentCenter &&
(adjustmentConfig->mode == ADJUSTMENT_MODE_STEP)) {
int value = (((rcData[channelIndex] - PWM_RANGE_MIDDLE) * adjustmentRange->adjustmentScale) / (PWM_RANGE_MIDDLE - PWM_RANGE_MIN)) + adjustmentRange->adjustmentCenter;
newValue = applyAbsoluteAdjustment(controlRateConfig, adjustmentFunction, value);
setConfigDirtyIfNotPermanent(&adjustmentRange->range);
pidInitConfig(currentPidProfile);
}
}
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
updateOsdAdjustmentData(newValue, adjustmentConfig->adjustmentFunction);
#else
UNUSED(newValue);
#endif
adjustmentState->lastRcData = rcData[channelIndex];
}
} else {
adjustmentState->lastRcData = 0;
}
}
}
void processRcAdjustments(controlRateConfig_t *controlRateConfig)
{
const bool canUseRxData = rxIsReceivingSignal();
// Recalculate the new active adjustments if required
if (stepwiseAdjustmentCount == ADJUSTMENT_RANGE_COUNT_INVALID) {
calcActiveAdjustmentRanges();
}
processStepwiseAdjustments(controlRateConfig, canUseRxData);
if (canUseRxData) {
processContinuosAdjustments(controlRateConfig);
}
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
// Hide the element if there is no change
updateOsdAdjustmentData(-1, 0);
#endif
}
#if defined(USE_OSD) && defined(USE_OSD_ADJUSTMENTS)
const char *getAdjustmentsRangeName(void)
{
if (adjustmentRangeNameIndex > 0) {
return &adjustmentLabels[adjustmentRangeNameIndex - 1][0];
} else {
return NULL;
}
}
int getAdjustmentsRangeValue(void)
{
return adjustmentRangeValue;
}
#endif
void activeAdjustmentRangeReset(void)
{
stepwiseAdjustmentCount = ADJUSTMENT_RANGE_COUNT_INVALID;
}