/
rc_adjustments.c
660 lines (602 loc) · 25.2 KB
/
rc_adjustments.c
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/*
* This file is part of Cleanflight.
*
* Cleanflight is free software: you can redistribute it and/or modify
* it 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 is distributed in the hope that it 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 Cleanflight. If not, see <http://www.gnu.org/licenses/>.
*/
#include <stdbool.h>
#include <stdint.h>
#include <string.h>
#include "platform.h"
#include "blackbox/blackbox.h"
#include "blackbox/blackbox_fielddefs.h"
#include "common/axis.h"
#include "common/maths.h"
#include "common/utils.h"
#include "config/feature.h"
#include "config/parameter_group.h"
#include "config/parameter_group_ids.h"
#include "drivers/time.h"
#include "fc/config.h"
#include "fc/controlrate_profile.h"
#include "fc/rc_adjustments.h"
#include "fc/rc_curves.h"
#include "navigation/navigation.h"
#include "flight/mixer.h"
#include "flight/pid.h"
#include "io/beeper.h"
#include "sensors/boardalignment.h"
#include "rx/rx.h"
PG_REGISTER_ARRAY(adjustmentRange_t, MAX_ADJUSTMENT_RANGE_COUNT, adjustmentRanges, PG_ADJUSTMENT_RANGE_CONFIG, 0);
static uint8_t adjustmentStateMask = 0;
#define MARK_ADJUSTMENT_FUNCTION_AS_BUSY(adjustmentIndex) adjustmentStateMask |= (1 << adjustmentIndex)
#define MARK_ADJUSTMENT_FUNCTION_AS_READY(adjustmentIndex) adjustmentStateMask &= ~(1 << adjustmentIndex)
#define IS_ADJUSTMENT_FUNCTION_BUSY(adjustmentIndex) (adjustmentStateMask & (1 << adjustmentIndex))
#define RC_ADJUSTMENT_EXPO_MIN 0
#define RC_ADJUSTMENT_EXPO_MAX 100
#define RC_ADJUSTMENT_MANUAL_RATE_MIN 0
#define RC_ADJUSTMENT_MANUAL_RATE_MAX 100
#define RC_ADJUSTMENT_PID_MIN 0
#define RC_ADJUSTMENT_PID_MAX 200
// sync with adjustmentFunction_e
static const adjustmentConfig_t defaultAdjustmentConfigs[ADJUSTMENT_FUNCTION_COUNT - 1] = {
{
.adjustmentFunction = ADJUSTMENT_RC_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_RC_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_THROTTLE_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_YAW_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_ROLL_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_YAW_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_YAW_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_YAW_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_RATE_PROFILE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_RC_YAW_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_RC_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_RC_YAW_EXPO,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_PITCH_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_ROLL_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_PITCH_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_MANUAL_YAW_RATE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_NAV_FW_CRUISE_THR,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 10 }}
}, {
.adjustmentFunction = ADJUSTMENT_NAV_FW_PITCH2THR,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_ROLL_BOARD_ALIGNMENT,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 5 }}
}, {
.adjustmentFunction = ADJUSTMENT_PITCH_BOARD_ALIGNMENT,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 5 }}
}, {
.adjustmentFunction = ADJUSTMENT_LEVEL_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_LEVEL_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_LEVEL_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_XY_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_XY_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_XY_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_Z_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_Z_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_POS_Z_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_HEADING_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_XY_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_XY_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_XY_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_Z_P,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_Z_I,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_VEL_Z_D,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 1 }}
}, {
.adjustmentFunction = ADJUSTMENT_FW_MIN_THROTTLE_DOWN_PITCH_ANGLE,
.mode = ADJUSTMENT_MODE_STEP,
.data = { .stepConfig = { .step = 5 }}
#ifdef USE_INFLIGHT_PROFILE_ADJUSTMENT
}, {
.adjustmentFunction = ADJUSTMENT_PROFILE,
.mode = ADJUSTMENT_MODE_SELECT,
.data = { .selectConfig = { .switchPositions = 3 }}
#endif
}
};
#define ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET 1
static adjustmentState_t adjustmentStates[MAX_SIMULTANEOUS_ADJUSTMENT_COUNT];
static void configureAdjustment(uint8_t index, uint8_t auxSwitchChannelIndex, const adjustmentConfig_t *adjustmentConfig)
{
adjustmentState_t * const adjustmentState = &adjustmentStates[index];
if (adjustmentState->config == adjustmentConfig) {
// already configured
return;
}
adjustmentState->auxChannelIndex = auxSwitchChannelIndex;
adjustmentState->config = adjustmentConfig;
adjustmentState->timeoutAt = 0;
MARK_ADJUSTMENT_FUNCTION_AS_READY(index);
}
static void blackboxLogInflightAdjustmentEvent(adjustmentFunction_e adjustmentFunction, int32_t newValue)
{
#ifndef USE_BLACKBOX
UNUSED(adjustmentFunction);
UNUSED(newValue);
#else
if (feature(FEATURE_BLACKBOX)) {
flightLogEvent_inflightAdjustment_t eventData;
eventData.adjustmentFunction = adjustmentFunction;
eventData.newValue = newValue;
eventData.floatFlag = false;
blackboxLogEvent(FLIGHT_LOG_EVENT_INFLIGHT_ADJUSTMENT, (flightLogEventData_t*)&eventData);
}
#endif
}
#if 0
static void blackboxLogInflightAdjustmentEventFloat(adjustmentFunction_e adjustmentFunction, float newFloatValue)
{
#ifndef USE_BLACKBOX
UNUSED(adjustmentFunction);
UNUSED(newFloatValue);
#else
if (feature(FEATURE_BLACKBOX)) {
flightLogEvent_inflightAdjustment_t eventData;
eventData.adjustmentFunction = adjustmentFunction;
eventData.newFloatValue = newFloatValue;
eventData.floatFlag = true;
blackboxLogEvent(FLIGHT_LOG_EVENT_INFLIGHT_ADJUSTMENT, (flightLogEventData_t*)&eventData);
}
#endif
}
#endif
static void applyAdjustmentU8(adjustmentFunction_e adjustmentFunction, uint8_t *val, int delta, int low, int high)
{
int newValue = constrain((int)(*val) + delta, low, high);
*val = newValue;
blackboxLogInflightAdjustmentEvent(adjustmentFunction, newValue);
}
static void applyAdjustmentU16(adjustmentFunction_e adjustmentFunction, uint16_t *val, int delta, int low, int high)
{
int newValue = constrain((int)(*val) + delta, low, high);
*val = newValue;
blackboxLogInflightAdjustmentEvent(adjustmentFunction, newValue);
}
static void applyAdjustmentExpo(adjustmentFunction_e adjustmentFunction, uint8_t *val, int delta)
{
applyAdjustmentU8(adjustmentFunction, val, delta, RC_ADJUSTMENT_EXPO_MIN, RC_ADJUSTMENT_EXPO_MAX);
}
static void applyAdjustmentManualRate(adjustmentFunction_e adjustmentFunction, uint8_t *val, int delta)
{
return applyAdjustmentU8(adjustmentFunction, val, delta, RC_ADJUSTMENT_MANUAL_RATE_MIN, RC_ADJUSTMENT_MANUAL_RATE_MAX);
}
static void applyAdjustmentPID(adjustmentFunction_e adjustmentFunction, uint8_t *val, int delta)
{
applyAdjustmentU8(adjustmentFunction, val, delta, RC_ADJUSTMENT_PID_MIN, RC_ADJUSTMENT_PID_MAX);
}
static void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustmentFunction, int delta)
{
if (delta > 0) {
beeperConfirmationBeeps(2);
} else {
beeperConfirmationBeeps(1);
}
switch (adjustmentFunction) {
case ADJUSTMENT_RC_EXPO:
applyAdjustmentExpo(ADJUSTMENT_RC_EXPO, &controlRateConfig->stabilized.rcExpo8, delta);
break;
case ADJUSTMENT_RC_YAW_EXPO:
applyAdjustmentExpo(ADJUSTMENT_RC_YAW_EXPO, &controlRateConfig->stabilized.rcYawExpo8, delta);
break;
case ADJUSTMENT_MANUAL_RC_EXPO:
applyAdjustmentExpo(ADJUSTMENT_MANUAL_RC_EXPO, &controlRateConfig->manual.rcExpo8, delta);
break;
case ADJUSTMENT_MANUAL_RC_YAW_EXPO:
applyAdjustmentExpo(ADJUSTMENT_MANUAL_RC_YAW_EXPO, &controlRateConfig->manual.rcYawExpo8, delta);
break;
case ADJUSTMENT_THROTTLE_EXPO:
applyAdjustmentExpo(ADJUSTMENT_THROTTLE_EXPO, &controlRateConfig->throttle.rcExpo8, delta);
break;
case ADJUSTMENT_PITCH_ROLL_RATE:
case ADJUSTMENT_PITCH_RATE:
applyAdjustmentU8(ADJUSTMENT_PITCH_RATE, &controlRateConfig->stabilized.rates[FD_PITCH], delta, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MIN, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MAX);
if (adjustmentFunction == ADJUSTMENT_PITCH_RATE) {
schedulePidGainsUpdate();
break;
}
// follow though for combined ADJUSTMENT_PITCH_ROLL_RATE
FALLTHROUGH;
case ADJUSTMENT_ROLL_RATE:
applyAdjustmentU8(ADJUSTMENT_ROLL_RATE, &controlRateConfig->stabilized.rates[FD_ROLL], delta, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MIN, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MAX);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_MANUAL_PITCH_ROLL_RATE:
case ADJUSTMENT_MANUAL_ROLL_RATE:
applyAdjustmentManualRate(ADJUSTMENT_MANUAL_ROLL_RATE, &controlRateConfig->manual.rates[FD_ROLL], delta);
if (adjustmentFunction == ADJUSTMENT_MANUAL_ROLL_RATE)
break;
// follow though for combined ADJUSTMENT_MANUAL_PITCH_ROLL_RATE
FALLTHROUGH;
case ADJUSTMENT_MANUAL_PITCH_RATE:
applyAdjustmentManualRate(ADJUSTMENT_MANUAL_PITCH_RATE, &controlRateConfig->manual.rates[FD_PITCH], delta);
break;
case ADJUSTMENT_YAW_RATE:
applyAdjustmentU8(ADJUSTMENT_YAW_RATE, &controlRateConfig->stabilized.rates[FD_YAW], delta, CONTROL_RATE_CONFIG_YAW_RATE_MIN, CONTROL_RATE_CONFIG_YAW_RATE_MAX);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_MANUAL_YAW_RATE:
applyAdjustmentManualRate(ADJUSTMENT_MANUAL_YAW_RATE, &controlRateConfig->manual.rates[FD_YAW], delta);
break;
case ADJUSTMENT_PITCH_ROLL_P:
case ADJUSTMENT_PITCH_P:
applyAdjustmentPID(ADJUSTMENT_PITCH_P, &pidBankMutable()->pid[PID_PITCH].P, delta);
if (adjustmentFunction == ADJUSTMENT_PITCH_P) {
schedulePidGainsUpdate();
break;
}
// follow though for combined ADJUSTMENT_PITCH_ROLL_P
FALLTHROUGH;
case ADJUSTMENT_ROLL_P:
applyAdjustmentPID(ADJUSTMENT_ROLL_P, &pidBankMutable()->pid[PID_ROLL].P, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_PITCH_ROLL_I:
case ADJUSTMENT_PITCH_I:
applyAdjustmentPID(ADJUSTMENT_PITCH_I, &pidBankMutable()->pid[PID_PITCH].I, delta);
if (adjustmentFunction == ADJUSTMENT_PITCH_I) {
schedulePidGainsUpdate();
break;
}
// follow though for combined ADJUSTMENT_PITCH_ROLL_I
FALLTHROUGH;
case ADJUSTMENT_ROLL_I:
applyAdjustmentPID(ADJUSTMENT_ROLL_I, &pidBankMutable()->pid[PID_ROLL].I, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_PITCH_ROLL_D:
case ADJUSTMENT_PITCH_D:
applyAdjustmentPID(ADJUSTMENT_PITCH_D, &pidBankMutable()->pid[PID_PITCH].D, delta);
if (adjustmentFunction == ADJUSTMENT_PITCH_D) {
schedulePidGainsUpdate();
break;
}
// follow though for combined ADJUSTMENT_PITCH_ROLL_D
FALLTHROUGH;
case ADJUSTMENT_ROLL_D:
applyAdjustmentPID(ADJUSTMENT_ROLL_D, &pidBankMutable()->pid[PID_ROLL].D, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_YAW_P:
applyAdjustmentPID(ADJUSTMENT_YAW_P, &pidBankMutable()->pid[PID_YAW].P, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_YAW_I:
applyAdjustmentPID(ADJUSTMENT_YAW_I, &pidBankMutable()->pid[PID_YAW].I, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_YAW_D:
applyAdjustmentPID(ADJUSTMENT_YAW_D, &pidBankMutable()->pid[PID_YAW].D, delta);
schedulePidGainsUpdate();
break;
case ADJUSTMENT_NAV_FW_CRUISE_THR:
applyAdjustmentU16(ADJUSTMENT_NAV_FW_CRUISE_THR, &navConfigMutable()->fw.cruise_throttle, delta, 1000, 2000);
break;
case ADJUSTMENT_NAV_FW_PITCH2THR:
applyAdjustmentU8(ADJUSTMENT_NAV_FW_PITCH2THR, &navConfigMutable()->fw.pitch_to_throttle, delta, 0, 100);
break;
case ADJUSTMENT_ROLL_BOARD_ALIGNMENT:
updateBoardAlignment(delta, 0);
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_BOARD_ALIGNMENT, boardAlignment()->rollDeciDegrees);
break;
case ADJUSTMENT_PITCH_BOARD_ALIGNMENT:
updateBoardAlignment(0, delta);
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_BOARD_ALIGNMENT, boardAlignment()->pitchDeciDegrees);
break;
case ADJUSTMENT_LEVEL_P:
applyAdjustmentPID(ADJUSTMENT_LEVEL_P, &pidBankMutable()->pid[PID_LEVEL].P, delta);
// TODO: Need to call something to take it into account?
break;
case ADJUSTMENT_LEVEL_I:
applyAdjustmentPID(ADJUSTMENT_LEVEL_I, &pidBankMutable()->pid[PID_LEVEL].I, delta);
// TODO: Need to call something to take it into account?
break;
case ADJUSTMENT_LEVEL_D:
applyAdjustmentPID(ADJUSTMENT_LEVEL_D, &pidBankMutable()->pid[PID_LEVEL].D, delta);
// TODO: Need to call something to take it into account?
break;
case ADJUSTMENT_POS_XY_P:
applyAdjustmentPID(ADJUSTMENT_POS_XY_P, &pidBankMutable()->pid[PID_POS_XY].P, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_POS_XY_I:
applyAdjustmentPID(ADJUSTMENT_POS_XY_I, &pidBankMutable()->pid[PID_POS_XY].I, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_POS_XY_D:
applyAdjustmentPID(ADJUSTMENT_POS_XY_D, &pidBankMutable()->pid[PID_POS_XY].D, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_POS_Z_P:
applyAdjustmentPID(ADJUSTMENT_POS_Z_P, &pidBankMutable()->pid[PID_POS_Z].P, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_POS_Z_I:
applyAdjustmentPID(ADJUSTMENT_POS_Z_I, &pidBankMutable()->pid[PID_POS_Z].I, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_POS_Z_D:
applyAdjustmentPID(ADJUSTMENT_POS_Z_D, &pidBankMutable()->pid[PID_POS_Z].D, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_HEADING_P:
applyAdjustmentPID(ADJUSTMENT_HEADING_P, &pidBankMutable()->pid[PID_HEADING].P, delta);
// TODO: navigationUsePIDs()?
break;
case ADJUSTMENT_VEL_XY_P:
applyAdjustmentPID(ADJUSTMENT_VEL_XY_P, &pidBankMutable()->pid[PID_VEL_XY].P, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_VEL_XY_I:
applyAdjustmentPID(ADJUSTMENT_VEL_XY_I, &pidBankMutable()->pid[PID_VEL_XY].I, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_VEL_XY_D:
applyAdjustmentPID(ADJUSTMENT_VEL_XY_D, &pidBankMutable()->pid[PID_VEL_XY].D, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_VEL_Z_P:
applyAdjustmentPID(ADJUSTMENT_VEL_Z_P, &pidBankMutable()->pid[PID_VEL_Z].P, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_VEL_Z_I:
applyAdjustmentPID(ADJUSTMENT_VEL_Z_I, &pidBankMutable()->pid[PID_VEL_Z].I, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_VEL_Z_D:
applyAdjustmentPID(ADJUSTMENT_VEL_Z_D, &pidBankMutable()->pid[PID_VEL_Z].D, delta);
navigationUsePIDs();
break;
case ADJUSTMENT_FW_MIN_THROTTLE_DOWN_PITCH_ANGLE:
applyAdjustmentU16(ADJUSTMENT_FW_MIN_THROTTLE_DOWN_PITCH_ANGLE, &mixerConfigMutable()->fwMinThrottleDownPitchAngle, delta, 0, FW_MIN_THROTTLE_DOWN_PITCH_ANGLE_MAX);
break;
default:
break;
};
}
#ifdef USE_INFLIGHT_PROFILE_ADJUSTMENT
static void applySelectAdjustment(uint8_t adjustmentFunction, uint8_t position)
{
bool applied = false;
switch (adjustmentFunction) {
case ADJUSTMENT_RATE_PROFILE:
if (getCurrentControlRateProfile() != position) {
changeControlRateProfile(position);
blackboxLogInflightAdjustmentEvent(ADJUSTMENT_RATE_PROFILE, position);
applied = true;
}
break;
}
if (applied) {
beeperConfirmationBeeps(position + 1);
}
}
#endif
#define RESET_FREQUENCY_2HZ (1000 / 2)
void processRcAdjustments(controlRateConfig_t *controlRateConfig)
{
const uint32_t now = millis();
const bool canUseRxData = rxIsReceivingSignal();
for (int adjustmentIndex = 0; adjustmentIndex < MAX_SIMULTANEOUS_ADJUSTMENT_COUNT; adjustmentIndex++) {
adjustmentState_t * const adjustmentState = &adjustmentStates[adjustmentIndex];
if (!adjustmentState->config) {
continue;
}
const uint8_t adjustmentFunction = adjustmentState->config->adjustmentFunction;
if (adjustmentFunction == ADJUSTMENT_NONE) {
continue;
}
const int32_t signedDiff = now - adjustmentState->timeoutAt;
const bool canResetReadyStates = signedDiff >= 0L;
if (canResetReadyStates) {
adjustmentState->timeoutAt = now + RESET_FREQUENCY_2HZ;
MARK_ADJUSTMENT_FUNCTION_AS_READY(adjustmentIndex);
}
if (!canUseRxData) {
continue;
}
const uint8_t channelIndex = NON_AUX_CHANNEL_COUNT + adjustmentState->auxChannelIndex;
if (adjustmentState->config->mode == ADJUSTMENT_MODE_STEP) {
int delta;
if (rcData[channelIndex] > PWM_RANGE_MIDDLE + 200) {
delta = adjustmentState->config->data.stepConfig.step;
} else if (rcData[channelIndex] < PWM_RANGE_MIDDLE - 200) {
delta = 0 - adjustmentState->config->data.stepConfig.step;
} else {
// returning the switch to the middle immediately resets the ready state
MARK_ADJUSTMENT_FUNCTION_AS_READY(adjustmentIndex);
adjustmentState->timeoutAt = now + RESET_FREQUENCY_2HZ;
continue;
}
if (IS_ADJUSTMENT_FUNCTION_BUSY(adjustmentIndex)) {
continue;
}
// it is legitimate to adjust an otherwise const item here
applyStepAdjustment(controlRateConfig, adjustmentFunction, delta);
#ifdef USE_INFLIGHT_PROFILE_ADJUSTMENT
} else if (adjustmentState->config->mode == ADJUSTMENT_MODE_SELECT) {
const uint16_t rangeWidth = ((2100 - 900) / adjustmentState->config->data.selectConfig.switchPositions);
const uint8_t position = (constrain(rcData[channelIndex], 900, 2100 - 1) - 900) / rangeWidth;
applySelectAdjustment(adjustmentFunction, position);
#endif
}
MARK_ADJUSTMENT_FUNCTION_AS_BUSY(adjustmentIndex);
}
}
void resetAdjustmentStates(void)
{
memset(adjustmentStates, 0, sizeof(adjustmentStates));
}
void updateAdjustmentStates(void)
{
for (int index = 0; index < MAX_ADJUSTMENT_RANGE_COUNT; index++) {
const adjustmentRange_t * const adjustmentRange = adjustmentRanges(index);
if (isRangeActive(adjustmentRange->auxChannelIndex, &adjustmentRange->range)) {
const adjustmentConfig_t *adjustmentConfig = &defaultAdjustmentConfigs[adjustmentRange->adjustmentFunction - ADJUSTMENT_FUNCTION_CONFIG_INDEX_OFFSET];
configureAdjustment(adjustmentRange->adjustmentIndex, adjustmentRange->auxSwitchChannelIndex, adjustmentConfig);
}
}
}
bool isAdjustmentFunctionSelected(uint8_t adjustmentFunction) {
for (uint8_t index = 0; index < MAX_SIMULTANEOUS_ADJUSTMENT_COUNT; ++index) {
if (adjustmentStates[index].config->adjustmentFunction == adjustmentFunction) {
return true;
}
}
return false;
}