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Merge remote-tracking branch 'multiwii/master'
Conflicts: obj/baseflight.hex src/sensors.c
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commit
c493a1579c
12 changed files with 69 additions and 42 deletions
6
README.md
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6
README.md
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@ -0,0 +1,6 @@
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baseflight
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==========
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32 bit fork of the MultiWii RC flight controller firmware
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Before making any contributions, take a note of the https://github.com/multiwii/baseflight/wiki/CodingStyle
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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 = 61;
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static const uint8_t EEPROM_CONF_VERSION = 62;
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static uint32_t enabledSensors = 0;
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static void resetConf(void);
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@ -279,7 +279,8 @@ static void resetConf(void)
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cfg.yawdeadband = 0;
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cfg.alt_hold_throttle_neutral = 40;
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cfg.alt_hold_fast_change = 1;
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cfg.throttle_angle_correction = 0; // could be 40
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cfg.throttle_correction_value = 0; // could 10 with althold or 40 for fpv
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cfg.throttle_correction_angle = 800; // could be 80.0 deg with atlhold or 45.0 for fpv
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// Failsafe Variables
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cfg.failsafe_delay = 10; // 1sec
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@ -21,6 +21,7 @@ int32_t vario = 0; // variometer in cm/s
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int16_t throttleAngleCorrection = 0; // correction of throttle in lateral wind,
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float magneticDeclination = 0.0f; // calculated at startup from config
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float accVelScale;
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float throttleAngleScale;
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// **************
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// gyro+acc IMU
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@ -36,6 +37,7 @@ void imuInit(void)
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{
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accZ_25deg = acc_1G * cosf(RAD * 25.0f);
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accVelScale = 9.80665f / acc_1G / 10000.0f;
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throttleAngleScale = (1800.0f / M_PI) * (900.0f / cfg.throttle_correction_angle);
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#ifdef MAG
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// if mag sensor is enabled, use it
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@ -303,9 +305,19 @@ static void getEstimatedAttitude(void)
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acc_calc(deltaT); // rotate acc vector into earth frame
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if (cfg.throttle_angle_correction) {
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int cosZ = ((int32_t)(EstG.V.Z * 100.0f)) / acc_1G;
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throttleAngleCorrection = cfg.throttle_angle_correction * constrain(100 - cosZ, 0, 100) / 8;
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if (cfg.throttle_correction_value) {
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float cosZ = EstG.V.Z / sqrtf(EstG.V.X * EstG.V.X + EstG.V.Y * EstG.V.Y + EstG.V.Z * EstG.V.Z);
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if (cosZ <= 0.015f) { // we are inverted, vertical or with a small angle < 0.86 deg
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throttleAngleCorrection = 0;
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} else {
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int angle = lrintf(acosf(cosZ) * throttleAngleScale);
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if (angle > 900)
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angle = 900;
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throttleAngleCorrection = lrintf(cfg.throttle_correction_value * sinf(angle / 900.0f * M_PI / 2.0f)) ;
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}
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}
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}
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@ -91,7 +91,8 @@ void gpsInit(uint8_t baudrateIndex)
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mode = MODE_RX;
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gpsSetPIDs();
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core.gpsport = uartOpen(USART2, gpsNewData, gpsInitData[baudrateIndex].baudrate, mode);
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// Open GPS UART, no callback - buffer will be read out in gpsThread()
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core.gpsport = uartOpen(USART2, NULL, gpsInitData[baudrateIndex].baudrate, mode);
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// signal GPS "thread" to initialize when it gets to it
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gpsSetState(GPS_INITIALIZING);
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}
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@ -156,6 +157,12 @@ void gpsInitHardware(void)
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void gpsThread(void)
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{
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// read out available GPS bytes
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if (core.gpsport) {
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while (serialTotalBytesWaiting(core.gpsport))
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gpsNewData(serialRead(core.gpsport));
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}
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switch (gpsData.state) {
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case GPS_UNKNOWN:
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break;
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@ -534,9 +541,6 @@ int8_t gpsSetPassthrough(void)
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if (gpsData.state != GPS_RECEIVINGDATA)
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return -1;
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// get rid of callback
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core.gpsport->callback = NULL;
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LED0_OFF;
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LED1_OFF;
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@ -844,8 +848,10 @@ uint32_t GPS_coord_to_degrees(char* s)
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int i;
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// scan for decimal point or end of field
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for (p = s; isdigit((unsigned char)*p); p++)
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;
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for (p = s; isdigit((unsigned char)*p); p++) {
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if (p >= s + 15)
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return 0; // stop potential fail
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}
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q = s;
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// convert degrees
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@ -890,6 +896,8 @@ static uint32_t grab_fields(char *src, uint8_t mult)
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tmp *= 10;
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if (src[i] >= '0' && src[i] <= '9')
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tmp += src[i] - '0';
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if (i >= 15)
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return 0; // out of bounds
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}
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return tmp;
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}
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6
src/mw.c
6
src/mw.c
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@ -768,8 +768,6 @@ void loop(void)
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}
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} else { // not in rc loop
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static int taskOrder = 0; // never call all function in the same loop, to avoid high delay spikes
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if (taskOrder > 4)
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taskOrder -= 5;
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switch (taskOrder) {
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case 0:
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taskOrder++;
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break;
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}
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case 4:
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taskOrder++;
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taskOrder = 0;
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#ifdef SONAR
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if (sensors(SENSOR_SONAR)) {
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Sonar_update();
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}
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#endif
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if (cfg.throttle_angle_correction && (f.ANGLE_MODE || f.HORIZON_MODE)) {
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if (cfg.throttle_correction_value && (f.ANGLE_MODE || f.HORIZON_MODE)) {
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rcCommand[THROTTLE] += throttleAngleCorrection;
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}
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3
src/mw.h
3
src/mw.h
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@ -186,7 +186,8 @@ typedef struct config_t {
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uint8_t yawdeadband; // introduce a deadband around the stick center for yaw axis. Must be greater than zero.
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uint8_t alt_hold_throttle_neutral; // defines the neutral zone of throttle stick during altitude hold, default setting is +/-40
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uint8_t alt_hold_fast_change; // when disabled, turn off the althold when throttle stick is out of deadband defined with alt_hold_throttle_neutral; when enabled, altitude changes slowly proportional to stick movement
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uint8_t throttle_angle_correction; //
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uint16_t throttle_correction_angle; // the angle when the throttle correction is maximal. in 0.1 degres, ex 225 = 22.5 ,30.0, 450 = 45.0 deg
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uint8_t throttle_correction_value; // the correction that will be applied at throttle_correction_angle.
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// Servo-related stuff
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servoParam_t servoConf[8]; // servo configuration
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@ -161,7 +161,8 @@ const clivalue_t valueTable[] = {
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{ "yawdeadband", VAR_UINT8, &cfg.yawdeadband, 0, 100 },
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{ "alt_hold_throttle_neutral", VAR_UINT8, &cfg.alt_hold_throttle_neutral, 1, 250 },
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{ "alt_hold_fast_change", VAR_UINT8, &cfg.alt_hold_fast_change, 0, 1 },
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{ "throttle_angle_correction", VAR_UINT8, &cfg.throttle_angle_correction, 0, 100 },
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{ "throttle_correction_value", VAR_UINT8, &cfg.throttle_correction_value, 0, 150 },
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{ "throttle_correction_angle", VAR_UINT16, &cfg.throttle_correction_angle, 1, 900 },
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{ "rc_rate", VAR_UINT8, &cfg.rcRate8, 0, 250 },
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{ "rc_expo", VAR_UINT8, &cfg.rcExpo8, 0, 100 },
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{ "thr_mid", VAR_UINT8, &cfg.thrMid8, 0, 100 },
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