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This commit is contained in:
treymarc 2014-04-12 02:51:42 +00:00
parent aa253a387d
commit cabf7eaac3
7 changed files with 25 additions and 26 deletions
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4
src/imu.c
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@ -358,8 +358,8 @@ int getEstimatedAltitude(void)
vel_acc = accZ_tmp * accVelScale * (float)accTimeSum;
// Integrator - Altitude in cm
accAlt += (vel_acc * 0.5f) * dt + vel * dt; // integrate velocity to get distance (x= a/2 * t^2)
accAlt = accAlt * cfg.baro_cf_alt + (float) BaroAlt *(1.0f - cfg.baro_cf_alt); // complementary filter for Altitude estimation (baro & acc)
accAlt += (vel_acc * 0.5f) * dt + vel * dt; // integrate velocity to get distance (x= a/2 * t^2)
accAlt = accAlt * cfg.baro_cf_alt + (float)BaroAlt * (1.0f - cfg.baro_cf_alt); // complementary filter for Altitude estimation (baro & acc)
EstAlt = accAlt;
vel += vel_acc;

2
src/main.c
View file

@ -88,7 +88,7 @@ int main(void)
break;
default:
pwm_params.adcChannel = 0;
break;
break;
}
pwmInit(&pwm_params);

16
src/mw.c
View file

@ -51,11 +51,11 @@ uint16_t GPS_ground_course = 0; // degrees * 10
int16_t nav[2];
int16_t nav_rated[2]; // Adding a rate controller to the navigation to make it smoother
int8_t nav_mode = NAV_MODE_NONE; // Navigation mode
uint8_t GPS_numCh; // Number of channels
uint8_t GPS_svinfo_chn[16]; // Channel number
uint8_t GPS_svinfo_svid[16]; // Satellite ID
uint8_t GPS_svinfo_quality[16]; // Bitfield Qualtity
uint8_t GPS_svinfo_cno[16]; // Carrier to Noise Ratio (Signal Strength)
uint8_t GPS_numCh; // Number of channels
uint8_t GPS_svinfo_chn[16]; // Channel number
uint8_t GPS_svinfo_svid[16]; // Satellite ID
uint8_t GPS_svinfo_quality[16]; // Bitfield Qualtity
uint8_t GPS_svinfo_cno[16]; // Carrier to Noise Ratio (Signal Strength)
// Automatic ACC Offset Calibration
uint16_t InflightcalibratingA = 0;
@ -103,7 +103,7 @@ void annexCode(void)
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t) cfg.dynThrPID * (rcData[THROTTLE] - cfg.tpaBreakPoint) / (2000 - cfg.tpaBreakPoint);
prop2 = 100 - (uint16_t)cfg.dynThrPID * (rcData[THROTTLE] - cfg.tpaBreakPoint) / (2000 - cfg.tpaBreakPoint);
} else {
prop2 = 100 - cfg.dynThrPID;
}
@ -143,7 +143,7 @@ void annexCode(void)
}
tmp = constrain(rcData[THROTTLE], mcfg.mincheck, 2000);
tmp = (uint32_t) (tmp - mcfg.mincheck) * 1000 / (2000 - mcfg.mincheck); // [MINCHECK;2000] -> [0;1000]
tmp = (uint32_t)(tmp - mcfg.mincheck) * 1000 / (2000 - mcfg.mincheck); // [MINCHECK;2000] -> [0;1000]
tmp2 = tmp / 100;
rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100; // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]
@ -363,7 +363,7 @@ static void pidRewrite(void)
// ----------PID controller----------
for (axis = 0; axis < 3; axis++) {
// -----Get the desired angle rate depending on flight mode
if ((f.ANGLE_MODE || f.HORIZON_MODE) && axis < 2 ) { // MODE relying on ACC
if ((f.ANGLE_MODE || f.HORIZON_MODE) && axis < 2) { // MODE relying on ACC
// calculate error and limit the angle to max configured inclination
errorAngle = constrain((rcCommand[axis] << 1) + GPS_angle[axis], -((int)mcfg.max_angle_inclination), +mcfg.max_angle_inclination) - angle[axis] + cfg.angleTrim[axis]; // 16 bits is ok here
}

2
src/sbus.c
View file

@ -20,7 +20,7 @@ static uint32_t sbusChannelData[SBUS_MAX_CHANNEL];
void sbusInit(rcReadRawDataPtr *callback)
{
int b;
for (b = 0; b < SBUS_MAX_CHANNEL; b ++)
for (b = 0; b < SBUS_MAX_CHANNEL; b++)
sbusChannelData[b] = 2 * (mcfg.midrc - SBUS_OFFSET);
core.rcvrport = uartOpen(USART2, sbusDataReceive, 100000, (portMode_t)(MODE_RX | MODE_SBUS));
if (callback)

5
src/sensors.c
View file

@ -179,8 +179,8 @@ static void ACC_Common(void)
// Calculate average, shift Z down by acc_1G and store values in EEPROM at end of calibration
if (calibratingA == 1) {
mcfg.accZero[ROLL] = (a[ROLL] + (CALIBRATING_ACC_CYCLES / 2)) / CALIBRATING_ACC_CYCLES;
mcfg.accZero[PITCH] = (a[PITCH] + (CALIBRATING_ACC_CYCLES / 2)) / CALIBRATING_ACC_CYCLES;
mcfg.accZero[YAW] = (a[YAW] + (CALIBRATING_ACC_CYCLES / 2)) / CALIBRATING_ACC_CYCLES - acc_1G;
mcfg.accZero[PITCH] = (a[PITCH] + (CALIBRATING_ACC_CYCLES / 2)) / CALIBRATING_ACC_CYCLES;
mcfg.accZero[YAW] = (a[YAW] + (CALIBRATING_ACC_CYCLES / 2)) / CALIBRATING_ACC_CYCLES - acc_1G;
cfg.angleTrim[ROLL] = 0;
cfg.angleTrim[PITCH] = 0;
writeEEPROM(1, true); // write accZero in EEPROM
@ -264,7 +264,6 @@ void Baro_Common(void)
baroHistIdx = indexplus1;
}
int Baro_update(void)
{
static uint32_t baroDeadline = 0;