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part 3 of the great sensor axis unfucking. careful flight testing may commence.
git-svn-id: https://afrodevices.googlecode.com/svn/trunk/baseflight@400 7c89a4a9-59b9-e629-4cfe-3a2d53b20e61
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5 changed files with 9 additions and 5 deletions
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@ -124,6 +124,7 @@ const clivalue_t valueTable[] = {
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{ "align_gyro", VAR_UINT8, &mcfg.gyro_align, 0, 8 },
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{ "align_acc", VAR_UINT8, &mcfg.acc_align, 0, 8 },
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{ "align_mag", VAR_UINT8, &mcfg.mag_align, 0, 8 },
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{ "yaw_control_direction", VAR_INT8, &mcfg.yaw_control_direction, -1, 1 },
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{ "acc_hardware", VAR_UINT8, &mcfg.acc_hardware, 0, 4 },
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{ "moron_threshold", VAR_UINT8, &mcfg.moron_threshold, 0, 128 },
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{ "gyro_lpf", VAR_UINT16, &mcfg.gyro_lpf, 0, 256 },
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@ -13,7 +13,7 @@ master_t mcfg; // master config struct with data independent from profiles
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config_t cfg; // profile config struct
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const char rcChannelLetters[] = "AERT1234";
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static const uint8_t EEPROM_CONF_VERSION = 50;
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static const uint8_t EEPROM_CONF_VERSION = 51;
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static uint32_t enabledSensors = 0;
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static void resetConf(void);
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@ -181,6 +181,7 @@ static void resetConf(void)
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mcfg.acc_align = ALIGN_DEFAULT;
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mcfg.mag_align = ALIGN_DEFAULT;
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mcfg.acc_hardware = ACC_DEFAULT; // default/autodetect
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mcfg.yaw_control_direction = 1;
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mcfg.moron_threshold = 32;
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mcfg.gyro_smoothing_factor = 0x00141403; // default factors of 20, 20, 3 for R/P/Y
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mcfg.vbatscale = 110;
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@ -321,17 +321,17 @@ void mixTable(void)
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// motors for non-servo mixes
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if (numberMotor > 1)
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for (i = 0; i < numberMotor; i++)
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motor[i] = rcCommand[THROTTLE] * currentMixer[i].throttle + axisPID[PITCH] * currentMixer[i].pitch + axisPID[ROLL] * currentMixer[i].roll + cfg.yaw_direction * axisPID[YAW] * currentMixer[i].yaw;
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motor[i] = rcCommand[THROTTLE] * currentMixer[i].throttle + axisPID[PITCH] * currentMixer[i].pitch + axisPID[ROLL] * currentMixer[i].roll + -cfg.yaw_direction * axisPID[YAW] * currentMixer[i].yaw;
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// airplane / servo mixes
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switch (mcfg.mixerConfiguration) {
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case MULTITYPE_BI:
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servo[4] = constrain(1500 + (cfg.yaw_direction * axisPID[YAW]) + axisPID[PITCH], 1020, 2000); //LEFT
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servo[5] = constrain(1500 + (cfg.yaw_direction * axisPID[YAW]) - axisPID[PITCH], 1020, 2000); //RIGHT
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servo[4] = constrain(1500 + (-cfg.yaw_direction * axisPID[YAW]) + axisPID[PITCH], 1020, 2000); //LEFT
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servo[5] = constrain(1500 + (-cfg.yaw_direction * axisPID[YAW]) - axisPID[PITCH], 1020, 2000); //RIGHT
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break;
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case MULTITYPE_TRI:
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servo[5] = constrain(cfg.tri_yaw_middle + cfg.yaw_direction * axisPID[YAW], cfg.tri_yaw_min, cfg.tri_yaw_max); //REAR
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servo[5] = constrain(cfg.tri_yaw_middle + -cfg.yaw_direction * axisPID[YAW], cfg.tri_yaw_min, cfg.tri_yaw_max); //REAR
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break;
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case MULTITYPE_GIMBAL:
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1
src/mw.c
1
src/mw.c
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@ -125,6 +125,7 @@ void annexCode(void)
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prop1 = 100 - (uint16_t) cfg.rollPitchRate * tmp / 500;
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prop1 = (uint16_t) prop1 *prop2 / 100;
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} else { // YAW
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tmp *= -mcfg.yaw_control_direction; //change control direction for yaw needed with new gyro orientation
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if (cfg.yawdeadband) {
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if (tmp > cfg.yawdeadband) {
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tmp -= cfg.yawdeadband;
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1
src/mw.h
1
src/mw.h
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@ -254,6 +254,7 @@ typedef struct master_t {
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sensor_align_e gyro_align; // gyro alignment
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sensor_align_e acc_align; // acc alignment
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sensor_align_e mag_align; // mag alignment
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int8_t yaw_control_direction; // change control direction of yaw (inverted, normal)
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uint8_t acc_hardware; // Which acc hardware to use on boards with more than one device
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uint16_t gyro_lpf; // gyro LPF setting - values are driver specific, in case of invalid number, a reasonable default ~30-40HZ is chosen.
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uint16_t gyro_cmpf_factor; // Set the Gyro Weight for Gyro/Acc complementary filter. Increasing this value would reduce and delay Acc influence on the output of the filter.
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