mirror of
https://github.com/iNavFlight/inav.git
synced 2025-07-26 01:35:35 +03:00
Merge branch 'master' into delayed_safehome
This commit is contained in:
commit
a89eb8ceff
16 changed files with 209 additions and 21 deletions
|
@ -39,7 +39,7 @@ Tool for Blackbox logs analysis is available [here](https://github.com/iNavFligh
|
||||||
|
|
||||||
### Telemetry screen for OpenTX
|
### Telemetry screen for OpenTX
|
||||||
|
|
||||||
Users of FrSky Taranis X9 and Q X7 can use INAV Lua Telemetry screen created by @teckel12 . Software and installation instruction are available here: [https://github.com/iNavFlight/LuaTelemetry](https://github.com/iNavFlight/LuaTelemetry)
|
Users of OpenTX radios (Taranis, Horus, Jumper, Radiomaster, Nirvana) can use INAV OpenTX Telemetry Widget screen. Software and installation instruction are available here: [https://github.com/iNavFlight/OpenTX-Telemetry-Widget](https://github.com/iNavFlight/OpenTX-Telemetry-Widget)
|
||||||
|
|
||||||
## Installation
|
## Installation
|
||||||
|
|
||||||
|
|
|
@ -123,7 +123,7 @@ The following sensors are transmitted
|
||||||
* **0450** : 'Flight Path Vector' or 'Course over ground' in degrees*10
|
* **0450** : 'Flight Path Vector' or 'Course over ground' in degrees*10
|
||||||
### Compatible SmartPort/INAV telemetry flight status
|
### Compatible SmartPort/INAV telemetry flight status
|
||||||
|
|
||||||
To quickly and easily monitor these SmartPort sensors and flight modes, install [iNav LuaTelemetry](https://github.com/iNavFlight/LuaTelemetry) to your Taranis Q X7, X9D, X9D+ or X9E transmitter.
|
To quickly and easily monitor these SmartPort sensors and flight modes, install [OpenTX Telemetry Widget](https://github.com/iNavFlight/OpenTX-Telemetry-Widget) to your Taranis Q X7, X9D, X9D+ or X9E transmitter.
|
||||||
|
|
||||||
## FrSky telemetry
|
## FrSky telemetry
|
||||||
|
|
||||||
|
|
|
@ -567,6 +567,11 @@ static bool mspFcProcessOutCommand(uint16_t cmdMSP, sbuf_t *dst, mspPostProcessF
|
||||||
sbufWriteU16(dst, programmingPids(i)->gains.FF);
|
sbufWriteU16(dst, programmingPids(i)->gains.FF);
|
||||||
}
|
}
|
||||||
break;
|
break;
|
||||||
|
case MSP2_INAV_PROGRAMMING_PID_STATUS:
|
||||||
|
for (int i = 0; i < MAX_PROGRAMMING_PID_COUNT; i++) {
|
||||||
|
sbufWriteU32(dst, programmingPidGetOutput(i));
|
||||||
|
}
|
||||||
|
break;
|
||||||
#endif
|
#endif
|
||||||
case MSP2_COMMON_MOTOR_MIXER:
|
case MSP2_COMMON_MOTOR_MIXER:
|
||||||
for (uint8_t i = 0; i < MAX_SUPPORTED_MOTORS; i++) {
|
for (uint8_t i = 0; i < MAX_SUPPORTED_MOTORS; i++) {
|
||||||
|
|
|
@ -2807,8 +2807,8 @@ groups:
|
||||||
description: "Value below which Crossfire SNR Alarm pops-up. (dB)"
|
description: "Value below which Crossfire SNR Alarm pops-up. (dB)"
|
||||||
default_value: "4"
|
default_value: "4"
|
||||||
field: snr_alarm
|
field: snr_alarm
|
||||||
min: -12
|
min: -20
|
||||||
max: 8
|
max: 10
|
||||||
- name: osd_link_quality_alarm
|
- name: osd_link_quality_alarm
|
||||||
condition: USE_SERIALRX_CRSF
|
condition: USE_SERIALRX_CRSF
|
||||||
description: "LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%"
|
description: "LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%"
|
||||||
|
|
|
@ -1699,7 +1699,7 @@ static bool osdDrawSingleElement(uint8_t item)
|
||||||
}
|
}
|
||||||
|
|
||||||
case OSD_CRSF_SNR_DB: {
|
case OSD_CRSF_SNR_DB: {
|
||||||
const char* showsnr = "-12";
|
const char* showsnr = "-20";
|
||||||
const char* hidesnr = " ";
|
const char* hidesnr = " ";
|
||||||
int16_t osdSNR_Alarm = rxLinkStatistics.uplinkSNR;
|
int16_t osdSNR_Alarm = rxLinkStatistics.uplinkSNR;
|
||||||
if (osdSNR_Alarm <= osdConfig()->snr_alarm) {
|
if (osdSNR_Alarm <= osdConfig()->snr_alarm) {
|
||||||
|
@ -1776,9 +1776,6 @@ static bool osdDrawSingleElement(uint8_t item)
|
||||||
gpsLocation_t wp2;
|
gpsLocation_t wp2;
|
||||||
int j;
|
int j;
|
||||||
|
|
||||||
tfp_sprintf(buff, "W%u/%u", posControl.activeWaypointIndex, posControl.waypointCount);
|
|
||||||
displayWrite(osdGetDisplayPort(), 13, osdConfig()->hud_margin_v - 1, buff);
|
|
||||||
|
|
||||||
for (int i = osdConfig()->hud_wp_disp - 1; i >= 0 ; i--) { // Display in reverse order so the next WP is always written on top
|
for (int i = osdConfig()->hud_wp_disp - 1; i >= 0 ; i--) { // Display in reverse order so the next WP is always written on top
|
||||||
j = posControl.activeWaypointIndex + i;
|
j = posControl.activeWaypointIndex + i;
|
||||||
if (posControl.waypointList[j].lat != 0 && posControl.waypointList[j].lon != 0 && j <= posControl.waypointCount) {
|
if (posControl.waypointList[j].lat != 0 && posControl.waypointList[j].lon != 0 && j <= posControl.waypointCount) {
|
||||||
|
|
|
@ -297,7 +297,7 @@ typedef struct osdConfig_s {
|
||||||
float gforce_axis_alarm_min;
|
float gforce_axis_alarm_min;
|
||||||
float gforce_axis_alarm_max;
|
float gforce_axis_alarm_max;
|
||||||
#ifdef USE_SERIALRX_CRSF
|
#ifdef USE_SERIALRX_CRSF
|
||||||
int16_t snr_alarm; //CRSF SNR alarm in dB
|
int8_t snr_alarm; //CRSF SNR alarm in dB
|
||||||
int8_t link_quality_alarm;
|
int8_t link_quality_alarm;
|
||||||
#endif
|
#endif
|
||||||
#ifdef USE_BARO
|
#ifdef USE_BARO
|
||||||
|
|
|
@ -63,6 +63,7 @@
|
||||||
#define MSP2_INAV_GVAR_STATUS 0x2027
|
#define MSP2_INAV_GVAR_STATUS 0x2027
|
||||||
#define MSP2_INAV_PROGRAMMING_PID 0x2028
|
#define MSP2_INAV_PROGRAMMING_PID 0x2028
|
||||||
#define MSP2_INAV_SET_PROGRAMMING_PID 0x2029
|
#define MSP2_INAV_SET_PROGRAMMING_PID 0x2029
|
||||||
|
#define MSP2_INAV_PROGRAMMING_PID_STATUS 0x202A
|
||||||
|
|
||||||
#define MSP2_PID 0x2030
|
#define MSP2_PID 0x2030
|
||||||
#define MSP2_SET_PID 0x2031
|
#define MSP2_SET_PID 0x2031
|
||||||
|
@ -79,4 +80,3 @@
|
||||||
#define MSP2_INAV_SET_SAFEHOME 0x2039
|
#define MSP2_INAV_SET_SAFEHOME 0x2039
|
||||||
|
|
||||||
#define MSP2_INAV_MISC2 0x203A
|
#define MSP2_INAV_MISC2 0x203A
|
||||||
|
|
||||||
|
|
|
@ -569,7 +569,7 @@ static bool estimationCalculateCorrection_Z(estimationContext_t * ctx)
|
||||||
if (ctx->newFlags & EST_GPS_Z_VALID) {
|
if (ctx->newFlags & EST_GPS_Z_VALID) {
|
||||||
// Trust GPS velocity only if residual/error is less than 2.5 m/s, scale weight according to gaussian distribution
|
// Trust GPS velocity only if residual/error is less than 2.5 m/s, scale weight according to gaussian distribution
|
||||||
const float gpsRocResidual = posEstimator.gps.vel.z - posEstimator.est.vel.z;
|
const float gpsRocResidual = posEstimator.gps.vel.z - posEstimator.est.vel.z;
|
||||||
const float gpsRocScaler = bellCurve(gpsRocResidual, 2.5f);
|
const float gpsRocScaler = bellCurve(gpsRocResidual, 250.0f);
|
||||||
ctx->estVelCorr.z += gpsRocResidual * positionEstimationConfig()->w_z_gps_v * gpsRocScaler * ctx->dt;
|
ctx->estVelCorr.z += gpsRocResidual * positionEstimationConfig()->w_z_gps_v * gpsRocScaler * ctx->dt;
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
|
@ -418,7 +418,7 @@ static int logicConditionGetFlightOperandValue(int operand) {
|
||||||
break;
|
break;
|
||||||
|
|
||||||
case LOGIC_CONDITION_OPERAND_FLIGHT_VERTICAL_SPEED: // cm/s
|
case LOGIC_CONDITION_OPERAND_FLIGHT_VERTICAL_SPEED: // cm/s
|
||||||
return constrain(getEstimatedActualVelocity(Z), 0, INT16_MAX);
|
return constrain(getEstimatedActualVelocity(Z), INT16_MIN, INT16_MAX);
|
||||||
break;
|
break;
|
||||||
|
|
||||||
case LOGIC_CONDITION_OPERAND_FLIGHT_TROTTLE_POS: // %
|
case LOGIC_CONDITION_OPERAND_FLIGHT_TROTTLE_POS: // %
|
||||||
|
|
|
@ -110,7 +110,7 @@ void programmingPidInit(void)
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
int programmingPidGetOutput(uint8_t i) {
|
int32_t programmingPidGetOutput(uint8_t i) {
|
||||||
return programmingPidState[constrain(i, 0, MAX_PROGRAMMING_PID_COUNT)].output;
|
return programmingPidState[constrain(i, 0, MAX_PROGRAMMING_PID_COUNT)].output;
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
|
@ -51,4 +51,4 @@ typedef struct programmingPidState_s {
|
||||||
void programmingPidUpdateTask(timeUs_t currentTimeUs);
|
void programmingPidUpdateTask(timeUs_t currentTimeUs);
|
||||||
void programmingPidInit(void);
|
void programmingPidInit(void);
|
||||||
void programmingPidReset(void);
|
void programmingPidReset(void);
|
||||||
int programmingPidGetOutput(uint8_t i);
|
int32_t programmingPidGetOutput(uint8_t i);
|
|
@ -56,7 +56,7 @@
|
||||||
|
|
||||||
baro_t baro; // barometer access functions
|
baro_t baro; // barometer access functions
|
||||||
|
|
||||||
PG_REGISTER_WITH_RESET_TEMPLATE(barometerConfig_t, barometerConfig, PG_BAROMETER_CONFIG, 2);
|
PG_REGISTER_WITH_RESET_TEMPLATE(barometerConfig_t, barometerConfig, PG_BAROMETER_CONFIG, 3);
|
||||||
|
|
||||||
#ifdef USE_BARO
|
#ifdef USE_BARO
|
||||||
#define BARO_HARDWARE_DEFAULT BARO_AUTODETECT
|
#define BARO_HARDWARE_DEFAULT BARO_AUTODETECT
|
||||||
|
@ -65,7 +65,7 @@ PG_REGISTER_WITH_RESET_TEMPLATE(barometerConfig_t, barometerConfig, PG_BAROMETER
|
||||||
#endif
|
#endif
|
||||||
PG_RESET_TEMPLATE(barometerConfig_t, barometerConfig,
|
PG_RESET_TEMPLATE(barometerConfig_t, barometerConfig,
|
||||||
.baro_hardware = BARO_HARDWARE_DEFAULT,
|
.baro_hardware = BARO_HARDWARE_DEFAULT,
|
||||||
.use_median_filtering = 0,
|
.use_median_filtering = 1,
|
||||||
.baro_calibration_tolerance = 150
|
.baro_calibration_tolerance = 150
|
||||||
);
|
);
|
||||||
|
|
||||||
|
|
|
@ -350,7 +350,7 @@ void compassUpdate(timeUs_t currentTimeUs)
|
||||||
static sensorCalibrationState_t calState;
|
static sensorCalibrationState_t calState;
|
||||||
static timeUs_t calStartedAt = 0;
|
static timeUs_t calStartedAt = 0;
|
||||||
static int16_t magPrev[XYZ_AXIS_COUNT];
|
static int16_t magPrev[XYZ_AXIS_COUNT];
|
||||||
static int magGain[XYZ_AXIS_COUNT] = {-4096, -4096, -4096};
|
static int magAxisDeviation[XYZ_AXIS_COUNT];
|
||||||
|
|
||||||
// Check magZero
|
// Check magZero
|
||||||
if (
|
if (
|
||||||
|
@ -381,6 +381,7 @@ void compassUpdate(timeUs_t currentTimeUs)
|
||||||
compassConfigMutable()->magZero.raw[axis] = 0;
|
compassConfigMutable()->magZero.raw[axis] = 0;
|
||||||
compassConfigMutable()->magGain[axis] = 1024;
|
compassConfigMutable()->magGain[axis] = 1024;
|
||||||
magPrev[axis] = 0;
|
magPrev[axis] = 0;
|
||||||
|
magAxisDeviation[axis] = 0; // Gain is based on the biggest absolute deviation from the mag zero point. Gain computation starts at 0
|
||||||
}
|
}
|
||||||
|
|
||||||
beeper(BEEPER_ACTION_SUCCESS);
|
beeper(BEEPER_ACTION_SUCCESS);
|
||||||
|
@ -400,9 +401,9 @@ void compassUpdate(timeUs_t currentTimeUs)
|
||||||
diffMag += (mag.magADC[axis] - magPrev[axis]) * (mag.magADC[axis] - magPrev[axis]);
|
diffMag += (mag.magADC[axis] - magPrev[axis]) * (mag.magADC[axis] - magPrev[axis]);
|
||||||
avgMag += (mag.magADC[axis] + magPrev[axis]) * (mag.magADC[axis] + magPrev[axis]) / 4.0f;
|
avgMag += (mag.magADC[axis] + magPrev[axis]) * (mag.magADC[axis] + magPrev[axis]) / 4.0f;
|
||||||
|
|
||||||
const int32_t sample = ABS(mag.magADC[axis]);
|
// Find the biggest sample deviation together with sample' sign
|
||||||
if (sample > magGain[axis]) {
|
if (ABS(mag.magADC[axis]) > ABS(magAxisDeviation[axis])) {
|
||||||
magGain[axis] = sample;
|
magAxisDeviation[axis] = mag.magADC[axis];
|
||||||
}
|
}
|
||||||
|
|
||||||
}
|
}
|
||||||
|
@ -429,7 +430,7 @@ void compassUpdate(timeUs_t currentTimeUs)
|
||||||
* It is dirty, but worth checking if this will solve the problem of changing mag vector when UAV is tilted
|
* It is dirty, but worth checking if this will solve the problem of changing mag vector when UAV is tilted
|
||||||
*/
|
*/
|
||||||
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
|
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
|
||||||
compassConfigMutable()->magGain[axis] = magGain[axis] - compassConfig()->magZero.raw[axis];
|
compassConfigMutable()->magGain[axis] = ABS(magAxisDeviation[axis] - compassConfig()->magZero.raw[axis]);
|
||||||
}
|
}
|
||||||
|
|
||||||
calStartedAt = 0;
|
calStartedAt = 0;
|
||||||
|
|
1
src/main/target/RUSH_BLADE_F7/CMakeLists.txt
Normal file
1
src/main/target/RUSH_BLADE_F7/CMakeLists.txt
Normal file
|
@ -0,0 +1 @@
|
||||||
|
target_stm32f722xe(RUSH_BLADE_F7 SKIP_RELEASES)
|
37
src/main/target/RUSH_BLADE_F7/target.c
Normal file
37
src/main/target/RUSH_BLADE_F7/target.c
Normal file
|
@ -0,0 +1,37 @@
|
||||||
|
/*
|
||||||
|
* This file is part of INAV.
|
||||||
|
*
|
||||||
|
* INAV 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.
|
||||||
|
*
|
||||||
|
* INAV 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 INAV. If not, see <http://www.gnu.org/licenses/>.
|
||||||
|
*/
|
||||||
|
|
||||||
|
#include <stdint.h>
|
||||||
|
#include "platform.h"
|
||||||
|
#include "drivers/bus.h"
|
||||||
|
#include "drivers/io.h"
|
||||||
|
#include "drivers/pwm_mapping.h"
|
||||||
|
#include "drivers/timer.h"
|
||||||
|
|
||||||
|
const timerHardware_t timerHardware[] = {
|
||||||
|
|
||||||
|
DEF_TIM(TIM8, CH3, PC8, TIM_USE_MC_MOTOR | TIM_USE_FW_SERVO, 0, 0), // S1 UP2-1 D(2, 4, 7)
|
||||||
|
DEF_TIM(TIM8, CH4, PC9, TIM_USE_MC_MOTOR | TIM_USE_FW_SERVO, 0, 0), // S2 UP2-1 D(2, 7, 7)
|
||||||
|
DEF_TIM(TIM3, CH4, PB1, TIM_USE_MC_MOTOR | TIM_USE_FW_MOTOR, 0, 0), // S6 UP1-2 D(1, 2, 5)
|
||||||
|
DEF_TIM(TIM3, CH3, PB0, TIM_USE_MC_MOTOR | TIM_USE_FW_MOTOR, 0, 0), // S5 UP1-2 D(1, 7, 5)
|
||||||
|
DEF_TIM(TIM8, CH2, PC7, TIM_USE_MC_MOTOR | TIM_USE_FW_SERVO, 0, 0), // S5 D(2, 3, 7)
|
||||||
|
DEF_TIM(TIM8, CH1, PC6, TIM_USE_MC_MOTOR | TIM_USE_FW_SERVO, 0, 0), // S6 D(1, 4, 5)
|
||||||
|
|
||||||
|
DEF_TIM(TIM2, CH1, PA15, TIM_USE_LED, 0, 0), // LED
|
||||||
|
};
|
||||||
|
|
||||||
|
const int timerHardwareCount = sizeof(timerHardware) / sizeof(timerHardware[0]);
|
147
src/main/target/RUSH_BLADE_F7/target.h
Normal file
147
src/main/target/RUSH_BLADE_F7/target.h
Normal file
|
@ -0,0 +1,147 @@
|
||||||
|
/*
|
||||||
|
* This file is part of INAV.
|
||||||
|
*
|
||||||
|
* INAV 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.
|
||||||
|
*
|
||||||
|
* INAV 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 INAV. If not, see <http://www.gnu.org/licenses/>.
|
||||||
|
*/
|
||||||
|
|
||||||
|
|
||||||
|
#pragma once
|
||||||
|
|
||||||
|
#define TARGET_BOARD_IDENTIFIER "RBF7"
|
||||||
|
#define USBD_PRODUCT_STRING "RUSH_BLADE_F7"
|
||||||
|
|
||||||
|
#define LED0 PB10 //Blue SWCLK
|
||||||
|
// #define LED1 PA13 //Green SWDIO
|
||||||
|
|
||||||
|
#define BEEPER PB2
|
||||||
|
#define BEEPER_INVERTED
|
||||||
|
|
||||||
|
// *************** SPI1 Gyro & ACC *******************
|
||||||
|
#define USE_SPI
|
||||||
|
#define USE_SPI_DEVICE_1
|
||||||
|
#define SPI1_SCK_PIN PA5
|
||||||
|
#define SPI1_MISO_PIN PA6
|
||||||
|
#define SPI1_MOSI_PIN PA7
|
||||||
|
|
||||||
|
#define USE_EXTI
|
||||||
|
#define USE_MPU_DATA_READY_SIGNAL
|
||||||
|
#define GYRO_INT_EXTI PA4
|
||||||
|
|
||||||
|
#define USE_IMU_MPU6000
|
||||||
|
#define IMU_MPU6000_ALIGN CW270_DEG
|
||||||
|
#define MPU6000_CS_PIN PC4
|
||||||
|
#define MPU6000_SPI_BUS BUS_SPI1
|
||||||
|
|
||||||
|
// *************** I2C /Baro/Mag *********************
|
||||||
|
#define USE_I2C
|
||||||
|
#define USE_I2C_DEVICE_1
|
||||||
|
#define I2C1_SCL PB8
|
||||||
|
#define I2C1_SDA PB9
|
||||||
|
|
||||||
|
#define USE_BARO
|
||||||
|
#define BARO_I2C_BUS BUS_I2C1
|
||||||
|
#define USE_BARO_BMP280
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||||||
|
#define USE_BARO_MS5611
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||||||
|
#define USE_BARO_DPS310
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||||||
|
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||||||
|
#define USE_MAG
|
||||||
|
#define MAG_I2C_BUS BUS_I2C1
|
||||||
|
#define USE_MAG_AK8975
|
||||||
|
#define USE_MAG_HMC5883
|
||||||
|
#define USE_MAG_QMC5883
|
||||||
|
#define USE_MAG_IST8310
|
||||||
|
#define USE_MAG_IST8308
|
||||||
|
#define USE_MAG_MAG3110
|
||||||
|
#define USE_MAG_LIS3MDL
|
||||||
|
|
||||||
|
#define TEMPERATURE_I2C_BUS BUS_I2C1
|
||||||
|
|
||||||
|
#define PITOT_I2C_BUS BUS_I2C1
|
||||||
|
|
||||||
|
#define USE_RANGEFINDER
|
||||||
|
#define RANGEFINDER_I2C_BUS BUS_I2C1
|
||||||
|
|
||||||
|
// *************** SPI2 Flash ***********************
|
||||||
|
#define USE_SPI_DEVICE_2
|
||||||
|
#define SPI2_SCK_PIN PB13
|
||||||
|
#define SPI2_MISO_PIN PB14
|
||||||
|
#define SPI2_MOSI_PIN PB15
|
||||||
|
|
||||||
|
#define USE_FLASHFS
|
||||||
|
#define USE_FLASH_M25P16
|
||||||
|
#define M25P16_SPI_BUS BUS_SPI2
|
||||||
|
#define M25P16_CS_PIN PB12
|
||||||
|
#define ENABLE_BLACKBOX_LOGGING_ON_SPIFLASH_BY_DEFAULT
|
||||||
|
|
||||||
|
// *************** UART *****************************
|
||||||
|
#define USE_VCP
|
||||||
|
#define USB_DETECT_PIN PC14
|
||||||
|
#define USE_USB_DETECT
|
||||||
|
|
||||||
|
#define USE_UART1
|
||||||
|
#define UART1_TX_PIN PA9
|
||||||
|
#define UART1_RX_PIN PA10
|
||||||
|
|
||||||
|
#define USE_UART2
|
||||||
|
#define UART2_TX_PIN PA2
|
||||||
|
#define UART2_RX_PIN PA3
|
||||||
|
|
||||||
|
#define USE_UART3
|
||||||
|
#define UART3_TX_PIN PC10
|
||||||
|
#define UART3_RX_PIN PC11
|
||||||
|
|
||||||
|
#define USE_UART4
|
||||||
|
#define UART4_TX_PIN PA0
|
||||||
|
#define UART4_RX_PIN PA1
|
||||||
|
|
||||||
|
#define USE_UART5
|
||||||
|
#define UART5_TX_PIN PC12
|
||||||
|
#define UART5_RX_PIN PD2
|
||||||
|
|
||||||
|
#define SERIAL_PORT_COUNT 6
|
||||||
|
|
||||||
|
#define DEFAULT_RX_TYPE RX_TYPE_SERIAL
|
||||||
|
#define SERIALRX_PROVIDER SERIALRX_SBUS
|
||||||
|
#define SERIALRX_UART SERIAL_PORT_USART2
|
||||||
|
|
||||||
|
// *************** ADC *****************************
|
||||||
|
#define USE_ADC
|
||||||
|
#define ADC_INSTANCE ADC1
|
||||||
|
#define ADC1_DMA_STREAM DMA2_Stream0
|
||||||
|
|
||||||
|
#define ADC_CHANNEL_1_PIN PC0
|
||||||
|
#define ADC_CHANNEL_2_PIN PC1
|
||||||
|
|
||||||
|
#define VBAT_ADC_CHANNEL ADC_CHN_1
|
||||||
|
#define CURRENT_METER_ADC_CHANNEL ADC_CHN_2
|
||||||
|
|
||||||
|
// *************** LEDSTRIP ************************
|
||||||
|
#define USE_LED_STRIP
|
||||||
|
#define WS2811_PIN PA8
|
||||||
|
|
||||||
|
#define DEFAULT_FEATURES (FEATURE_OSD | FEATURE_TELEMETRY | FEATURE_CURRENT_METER | FEATURE_VBAT | FEATURE_TX_PROF_SEL)
|
||||||
|
#define CURRENT_METER_SCALE 179
|
||||||
|
|
||||||
|
#define USE_SERIAL_4WAY_BLHELI_INTERFACE
|
||||||
|
|
||||||
|
#define TARGET_IO_PORTA 0xffff
|
||||||
|
#define TARGET_IO_PORTB 0xffff
|
||||||
|
#define TARGET_IO_PORTC 0xffff
|
||||||
|
#define TARGET_IO_PORTD 0xffff
|
||||||
|
|
||||||
|
#define MAX_PWM_OUTPUT_PORTS 10
|
||||||
|
#define USE_OSD
|
||||||
|
#define USE_DSHOT
|
||||||
|
#define USE_SERIALSHOT
|
||||||
|
#define USE_ESC_SENSOR
|
Loading…
Add table
Add a link
Reference in a new issue