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Rationalisation of sensor function names

This commit is contained in:
Martin Budden 2017-01-25 01:23:44 +00:00
parent 2725e6a9fc
commit 78350e829b
18 changed files with 67 additions and 66 deletions

View file

@ -420,8 +420,8 @@ static void activateConfig(void)
failsafeReset();
setAccelerationCalibrationValues();
setAccelerationFilter();
accSetCalibrationValues();
accInitFilters();
imuConfigure();

View file

@ -565,7 +565,7 @@ static bool mspFcProcessOutCommand(uint8_t cmdMSP, sbuf_t *dst, mspPostProcessFn
sbufWriteU8(dst, getConfigProfile());
sbufWriteU16(dst, averageSystemLoadPercent);
sbufWriteU16(dst, armingFlags);
sbufWriteU8(dst, getAccelerometerCalibrationAxisFlags());
sbufWriteU8(dst, accGetCalibrationAxisFlags());
break;
case MSP_STATUS:

View file

@ -103,7 +103,7 @@ void taskUpdateBattery(timeUs_t currentTimeUs)
if (cmpTimeUs(currentTimeUs, vbatLastServiced) >= VBATINTERVAL) {
timeUs_t vbatTimeDelta = currentTimeUs - vbatLastServiced;
vbatLastServiced = currentTimeUs;
updateBattery(vbatTimeDelta);
batteryUpdate(vbatTimeDelta);
}
}
@ -112,7 +112,7 @@ void taskUpdateBattery(timeUs_t currentTimeUs)
if (ibatTimeSinceLastServiced >= IBATINTERVAL) {
ibatLastServiced = currentTimeUs;
updateCurrentMeter(ibatTimeSinceLastServiced, flight3DConfig()->deadband3d_throttle);
currentMeterUpdate(ibatTimeSinceLastServiced, flight3DConfig()->deadband3d_throttle);
}
}
}

View file

@ -105,14 +105,14 @@ static bool isRXDataNew;
bool isCalibrating(void)
{
#ifdef BARO
if (sensors(SENSOR_BARO) && !isBaroCalibrationComplete()) {
if (sensors(SENSOR_BARO) && !baroIsCalibrationComplete()) {
return true;
}
#endif
// Note: compass calibration is handled completely differently, outside of the main loop, see f.CALIBRATE_MAG
return (!isAccelerationCalibrationComplete() && sensors(SENSOR_ACC)) || (!gyroIsCalibrationComplete());
return (!accIsCalibrationComplete() && sensors(SENSOR_ACC)) || (!gyroIsCalibrationComplete());
}
int16_t getAxisRcCommand(int16_t rawData, int16_t rate, int16_t deadband)

View file

@ -3275,6 +3275,13 @@ static void cliSet(char *cmdline)
}
}
static const char * getBatteryStateString(void)
{
static const char * const batteryStateStrings[] = {"OK", "WARNING", "CRITICAL", "NOT PRESENT"};
return batteryStateStrings[getBatteryState()];
}
static void cliStatus(char *cmdline)
{
UNUSED(cmdline);

View file

@ -610,12 +610,12 @@ void imuUpdateAccelerometer(void)
{
#ifdef HIL
if (sensors(SENSOR_ACC) && !hilActive) {
updateAccelerationReadings();
accUpdate();
isAccelUpdatedAtLeastOnce = true;
}
#else
if (sensors(SENSOR_ACC)) {
updateAccelerationReadings();
accUpdate();
isAccelUpdatedAtLeastOnce = true;
}
#endif

View file

@ -419,7 +419,7 @@ static void updateBaroTopic(timeUs_t currentTimeUs)
initialBaroAltitudeOffset = newBaroAlt;
}
if (sensors(SENSOR_BARO) && isBaroCalibrationComplete()) {
if (sensors(SENSOR_BARO) && baroIsCalibrationComplete()) {
posEstimator.baro.alt = newBaroAlt - initialBaroAltitudeOffset;
posEstimator.baro.epv = positionEstimationConfig()->baro_epv;
posEstimator.baro.lastUpdateTime = currentTimeUs;
@ -443,7 +443,7 @@ static void updatePitotTopic(timeUs_t currentTimeUs)
if (updateTimer(&pitotUpdateTimer, HZ2US(INAV_PITOT_UPDATE_RATE), currentTimeUs)) {
float newTAS = pitotCalculateAirSpeed();
if (sensors(SENSOR_PITOT) && isPitotCalibrationComplete()) {
if (sensors(SENSOR_PITOT) && pitotIsCalibrationComplete()) {
posEstimator.pitot.airspeed = newTAS;
}
else {

View file

@ -17,6 +17,8 @@
#pragma once
#include "config/parameter_group.h"
#if defined(USE_QUAD_MIXER_ONLY)
#define MAX_SUPPORTED_SERVOS 1
#else

View file

@ -264,7 +264,7 @@ bool accInit(uint32_t targetLooptime)
acc.dev.acc_1G = 256; // set default
acc.dev.init(&acc.dev);
acc.accTargetLooptime = targetLooptime;
setAccelerationFilter();
accInitFilters();
if (accelerometerConfig()->acc_align != ALIGN_DEFAULT) {
acc.dev.accAlign = accelerometerConfig()->acc_align;
}
@ -276,17 +276,17 @@ void accSetCalibrationCycles(uint16_t calibrationCyclesRequired)
calibratingA = calibrationCyclesRequired;
}
bool isAccelerationCalibrationComplete(void)
bool accIsCalibrationComplete(void)
{
return calibratingA == 0;
}
bool isOnFinalAccelerationCalibrationCycle(void)
static bool isOnFinalAccelerationCalibrationCycle(void)
{
return calibratingA == 1;
}
bool isOnFirstAccelerationCalibrationCycle(void)
static bool isOnFirstAccelerationCalibrationCycle(void)
{
return calibratingA == CALIBRATING_ACC_CYCLES;
}
@ -296,9 +296,9 @@ static bool calibratedAxis[6];
static int32_t accSamples[6][3];
static int calibratedAxisCount = 0;
bool getAccelerometerCalibrationAxisStatus(int axis)
bool accGetCalibrationAxisStatus(int axis)
{
if (isAccelerationCalibrationComplete()) {
if (accIsCalibrationComplete()) {
if (STATE(ACCELEROMETER_CALIBRATED)) {
return true; // if calibration is valid - all axis are calibrated
}
@ -311,11 +311,11 @@ bool getAccelerometerCalibrationAxisStatus(int axis)
}
}
uint8_t getAccelerometerCalibrationAxisFlags(void)
uint8_t accGetCalibrationAxisFlags(void)
{
uint8_t flags = 0;
for (int i = 0; i < 6; i++) {
if (getAccelerometerCalibrationAxisStatus(0)) {
if (accGetCalibrationAxisStatus(0)) {
flags |= (1 << i);
}
}
@ -342,7 +342,7 @@ int getPrimaryAxisIndex(int32_t sample[3])
return -1;
}
void performAcclerationCalibration(void)
static void performAcclerationCalibration(void)
{
int axisIndex = getPrimaryAxisIndex(acc.accADC);
@ -420,7 +420,7 @@ static void applyAccelerationZero(const flightDynamicsTrims_t * accZero, const f
acc.accADC[Z] = (acc.accADC[Z] - accZero->raw[Z]) * accGain->raw[Z] / 4096;
}
void updateAccelerationReadings(void)
void accUpdate(void)
{
if (!acc.dev.read(&acc.dev)) {
return;
@ -436,7 +436,7 @@ void updateAccelerationReadings(void)
}
}
if (!isAccelerationCalibrationComplete()) {
if (!accIsCalibrationComplete()) {
performAcclerationCalibration();
}
@ -445,7 +445,7 @@ void updateAccelerationReadings(void)
alignSensors(acc.accADC, acc.dev.accAlign);
}
void setAccelerationCalibrationValues(void)
void accSetCalibrationValues(void)
{
if ((accelerometerConfig()->accZero.raw[X] == 0) && (accelerometerConfig()->accZero.raw[Y] == 0) && (accelerometerConfig()->accZero.raw[Z] == 0) &&
(accelerometerConfig()->accGain.raw[X] == 4096) && (accelerometerConfig()->accGain.raw[Y] == 4096) &&(accelerometerConfig()->accGain.raw[Z] == 4096)) {
@ -456,7 +456,7 @@ void setAccelerationCalibrationValues(void)
}
}
void setAccelerationFilter(void)
void accInitFilters(void)
{
if (acc.accTargetLooptime && accelerometerConfig()->acc_lpf_hz) {
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
@ -465,7 +465,7 @@ void setAccelerationFilter(void)
}
}
bool isAccelerometerHealthy(void)
bool accIsHealthy(void)
{
return true;
}

View file

@ -56,11 +56,11 @@ typedef struct accelerometerConfig_s {
PG_DECLARE(accelerometerConfig_t, accelerometerConfig);
bool accInit(uint32_t accTargetLooptime);
bool isAccelerationCalibrationComplete(void);
bool accIsCalibrationComplete(void);
void accSetCalibrationCycles(uint16_t calibrationCyclesRequired);
void updateAccelerationReadings(void);
void setAccelerationCalibrationValues(void);
void setAccelerationFilter(void);
bool isAccelerometerHealthy(void);
bool getAccelerometerCalibrationAxisStatus(int axis);
uint8_t getAccelerometerCalibrationAxisFlags(void);
void accUpdate(void);
void accSetCalibrationValues(void);
void accInitFilters(void);
bool accIsHealthy(void);
bool accGetCalibrationAxisStatus(int axis);
uint8_t accGetCalibrationAxisFlags(void);

View file

@ -166,7 +166,7 @@ bool baroInit(void)
return true;
}
bool isBaroCalibrationComplete(void)
bool baroIsCalibrationComplete(void)
{
return calibratingB == 0;
}
@ -207,7 +207,7 @@ typedef enum {
BAROMETER_NEEDS_CALCULATION
} barometerState_e;
bool isBaroReady(void)
bool baroIsReady(void)
{
return baroReady;
}
@ -249,7 +249,7 @@ static void performBaroCalibrationCycle(void)
int32_t baroCalculateAltitude(void)
{
if (!isBaroCalibrationComplete()) {
if (!baroIsCalibrationComplete()) {
performBaroCalibrationCycle();
baro.BaroAlt = 0;
}
@ -269,7 +269,7 @@ int32_t baroCalculateAltitude(void)
return baro.BaroAlt;
}
bool isBarometerHealthy(void)
bool baroIsHealthy(void)
{
return true;
}

View file

@ -47,9 +47,9 @@ typedef struct baro_s {
extern baro_t baro;
bool baroInit(void);
bool isBaroCalibrationComplete(void);
bool baroIsCalibrationComplete(void);
void baroSetCalibrationCycles(uint16_t calibrationCyclesRequired);
uint32_t baroUpdate(void);
bool isBaroReady(void);
bool baroIsReady(void);
int32_t baroCalculateAltitude(void);
bool isBarometerHealthy(void);
bool baroIsHealthy(void);

View file

@ -96,7 +96,7 @@ static void updateBatteryVoltage(uint32_t vbatTimeDelta)
/* Batt Hysteresis of +/-100mV */
#define VBATT_HYSTERESIS 1
void updateBattery(uint32_t vbatTimeDelta)
void batteryUpdate(uint32_t vbatTimeDelta)
{
updateBatteryVoltage(vbatTimeDelta);
@ -166,13 +166,6 @@ batteryState_e getBatteryState(void)
return batteryState;
}
const char * const batteryStateStrings[] = {"OK", "WARNING", "CRITICAL", "NOT PRESENT"};
const char * getBatteryStateString(void)
{
return batteryStateStrings[batteryState];
}
void batteryInit(void)
{
batteryState = BATTERY_NOT_PRESENT;
@ -192,7 +185,7 @@ int32_t currentSensorToCentiamps(uint16_t src)
return (millivolts * 1000) / (int32_t)batteryConfig()->currentMeterScale; // current in 0.01A steps
}
void updateCurrentMeter(int32_t lastUpdateAt, uint16_t deadband3d_throttle)
void currentMeterUpdate(int32_t lastUpdateAt, uint16_t deadband3d_throttle)
{
static int32_t amperageRaw = 0;
static int64_t mAhdrawnRaw = 0;

View file

@ -71,11 +71,10 @@ extern int32_t mAhDrawn;
uint16_t batteryAdcToVoltage(uint16_t src);
batteryState_e getBatteryState(void);
const char * getBatteryStateString(void);
void updateBattery(uint32_t vbatTimeDelta);
void batteryUpdate(uint32_t vbatTimeDelta);
void batteryInit(void);
void updateCurrentMeter(int32_t lastUpdateAt, uint16_t deadband3d_throttle);
void currentMeterUpdate(int32_t lastUpdateAt, uint16_t deadband3d_throttle);
int32_t currentMeterToCentiamps(uint16_t src);
uint8_t calculateBatteryPercentage(void);

View file

@ -37,7 +37,7 @@ hardwareSensorStatus_e getHwAccelerometerStatus(void)
{
#if defined(ACC)
if (detectedSensors[SENSOR_INDEX_ACC] != ACC_NONE) {
if (isAccelerometerHealthy()) {
if (accIsHealthy()) {
return HW_SENSOR_OK;
}
else {
@ -89,7 +89,7 @@ hardwareSensorStatus_e getHwBarometerStatus(void)
{
#if defined(BARO)
if (detectedSensors[SENSOR_INDEX_BARO] != BARO_NONE) {
if (isBarometerHealthy()) {
if (baroIsHealthy()) {
return HW_SENSOR_OK;
}
else {
@ -115,7 +115,7 @@ hardwareSensorStatus_e getHwRangefinderStatus(void)
{
#if defined(SONAR)
if (detectedSensors[SENSOR_INDEX_RANGEFINDER] != RANGEFINDER_NONE) {
if (isRangefinderHealthy()) {
if (rangefinderIsHealthy()) {
return HW_SENSOR_OK;
}
else {
@ -141,7 +141,7 @@ hardwareSensorStatus_e getHwPitotmeterStatus(void)
{
#if defined(PITOT)
if (detectedSensors[SENSOR_INDEX_PITOT] != PITOT_NONE) {
if (isPitotmeterHealthy()) {
if (pitotIsHealthy()) {
return HW_SENSOR_OK;
}
else {

View file

@ -118,7 +118,7 @@ bool pitotInit(void)
return true;
}
bool isPitotCalibrationComplete(void)
bool pitotIsCalibrationComplete(void)
{
return calibratingP == 0;
}
@ -160,7 +160,7 @@ typedef enum {
} pitotmeterState_e;
bool isPitotReady(void) {
bool pitotIsReady(void) {
return pitotReady;
}
@ -202,10 +202,7 @@ static void performPitotCalibrationCycle(void)
int32_t pitotCalculateAirSpeed(void)
{
if (!isPitotCalibrationComplete()) {
performPitotCalibrationCycle();
pitot.airSpeed = 0;
} else {
if (pitotIsCalibrationComplete()) {
const float CalibratedAirspeed_tmp = pitotmeterConfig()->pitot_scale * CASFACTOR * sqrtf(powf(fabsf(pitotPressure - pitotPressureZero) / P0 + 1.0f, CCEXPONENT) - 1.0f);
CalibratedAirspeed = CalibratedAirspeed * pitotmeterConfig()->pitot_noise_lpf + CalibratedAirspeed_tmp * (1.0f - pitotmeterConfig()->pitot_noise_lpf); // additional LPF to reduce baro noise
float TrueAirspeed = CalibratedAirspeed * TASFACTOR * sqrtf(pitotTemperature);
@ -215,11 +212,14 @@ int32_t pitotCalculateAirSpeed(void)
//debug[1] = (int16_t)(TrueAirspeed*100);
//debug[2] = (int16_t)((pitotTemperature-273.15f)*100);
//debug[3] = AirSpeed;
} else {
performPitotCalibrationCycle();
pitot.airSpeed = 0;
}
return pitot.airSpeed;
}
bool isPitotmeterHealthy(void)
bool pitotIsHealthy(void)
{
return true;
}

View file

@ -48,9 +48,9 @@ typedef struct pito_s {
extern pitot_t pitot;
bool pitotInit(void);
bool isPitotCalibrationComplete(void);
bool pitotIsCalibrationComplete(void);
void pitotSetCalibrationCycles(uint16_t calibrationCyclesRequired);
uint32_t pitotUpdate(void);
bool isPitotReady(void);
bool pitotIsReady(void);
int32_t pitotCalculateAirSpeed(void);
bool isPitotmeterHealthy(void);
bool pitotIsHealthy(void);

View file

@ -243,7 +243,7 @@ int32_t rangefinderGetLatestAltitude(void)
return calculatedAltitude;
}
bool isRangefinderHealthy(void)
bool rangefinderIsHealthy(void)
{
return true;
}