1
0
Fork 0
mirror of https://github.com/iNavFlight/inav.git synced 2025-07-26 17:55:28 +03:00

Merge pull request #8858 from RomanLut/submit-simulator-sensor-failures

Enable possibility to simulate HW sensor failures in HITL
This commit is contained in:
Paweł Spychalski 2023-06-28 11:03:55 -07:00 committed by GitHub
commit cbb4b5f311
No known key found for this signature in database
GPG key ID: 4AEE18F83AFDEB23
5 changed files with 61 additions and 25 deletions

View file

@ -2526,6 +2526,7 @@ static mspResult_e mspFcProcessInCommand(uint16_t cmdMSP, sbuf_t *src)
gpsSol.flags.validVelNE = false; gpsSol.flags.validVelNE = false;
gpsSol.flags.validVelD = false; gpsSol.flags.validVelD = false;
gpsSol.flags.validEPE = false; gpsSol.flags.validEPE = false;
gpsSol.flags.validTime = false;
gpsSol.numSat = sbufReadU8(src); gpsSol.numSat = sbufReadU8(src);
gpsSol.llh.lat = sbufReadU32(src); gpsSol.llh.lat = sbufReadU32(src);
gpsSol.llh.lon = sbufReadU32(src); gpsSol.llh.lon = sbufReadU32(src);
@ -3533,6 +3534,7 @@ bool mspFCProcessInOutCommand(uint16_t cmdMSP, sbuf_t *dst, sbuf_t *src, mspResu
gpsSol.flags.validVelNE = true; gpsSol.flags.validVelNE = true;
gpsSol.flags.validVelD = true; gpsSol.flags.validVelD = true;
gpsSol.flags.validEPE = true; gpsSol.flags.validEPE = true;
gpsSol.flags.validTime = false;
gpsSol.llh.lat = sbufReadU32(src); gpsSol.llh.lat = sbufReadU32(src);
gpsSol.llh.lon = sbufReadU32(src); gpsSol.llh.lon = sbufReadU32(src);
@ -3587,7 +3589,7 @@ bool mspFCProcessInOutCommand(uint16_t cmdMSP, sbuf_t *dst, sbuf_t *src, mspResu
if (sensors(SENSOR_MAG)) { if (sensors(SENSOR_MAG)) {
mag.magADC[X] = ((int16_t)sbufReadU16(src)) / 20; // 16000 / 20 = 800uT mag.magADC[X] = ((int16_t)sbufReadU16(src)) / 20; // 16000 / 20 = 800uT
mag.magADC[Y] = ((int16_t)sbufReadU16(src)) / 20; mag.magADC[Y] = ((int16_t)sbufReadU16(src)) / 20; //note that mag failure is simulated by setting all readings to zero
mag.magADC[Z] = ((int16_t)sbufReadU16(src)) / 20; mag.magADC[Z] = ((int16_t)sbufReadU16(src)) / 20;
} else { } else {
sbufAdvance(src, sizeof(uint16_t) * XYZ_AXIS_COUNT); sbufAdvance(src, sizeof(uint16_t) * XYZ_AXIS_COUNT);
@ -3605,6 +3607,14 @@ bool mspFCProcessInOutCommand(uint16_t cmdMSP, sbuf_t *dst, sbuf_t *src, mspResu
if (SIMULATOR_HAS_OPTION(HITL_AIRSPEED)) { if (SIMULATOR_HAS_OPTION(HITL_AIRSPEED)) {
simulatorData.airSpeed = sbufReadU16(src); simulatorData.airSpeed = sbufReadU16(src);
} else {
if (SIMULATOR_HAS_OPTION(HITL_EXTENDED_FLAGS)) {
sbufReadU16(src);
}
}
if (SIMULATOR_HAS_OPTION(HITL_EXTENDED_FLAGS)) {
simulatorData.flags |= ((uint16_t)sbufReadU8(src)) << 8;
} }
} else { } else {
DISABLE_STATE(GPS_FIX); DISABLE_STATE(GPS_FIX);

View file

@ -181,7 +181,10 @@ typedef enum {
HITL_USE_IMU = (1 << 3), // Use the Acc and Gyro data provided by XPlane to calculate Attitude (i.e. 100% of the calculations made by AHRS from INAV) HITL_USE_IMU = (1 << 3), // Use the Acc and Gyro data provided by XPlane to calculate Attitude (i.e. 100% of the calculations made by AHRS from INAV)
HITL_HAS_NEW_GPS_DATA = (1 << 4), HITL_HAS_NEW_GPS_DATA = (1 << 4),
HITL_EXT_BATTERY_VOLTAGE = (1 << 5), // Extend MSP_SIMULATOR format 2 HITL_EXT_BATTERY_VOLTAGE = (1 << 5), // Extend MSP_SIMULATOR format 2
HITL_AIRSPEED = (1 << 6) HITL_AIRSPEED = (1 << 6),
HITL_EXTENDED_FLAGS = (1 << 7), // Extend MSP_SIMULATOR format 2
HITL_GPS_TIMEOUT = (1 << 8),
HITL_PITOT_FAILURE = (1 << 9)
} simulatorFlags_t; } simulatorFlags_t;
typedef struct { typedef struct {

View file

@ -343,10 +343,21 @@ bool gpsUpdate(void)
#ifdef USE_SIMULATOR #ifdef USE_SIMULATOR
if (ARMING_FLAG(SIMULATOR_MODE_HITL)) { if (ARMING_FLAG(SIMULATOR_MODE_HITL)) {
gpsUpdateTime(); if ( SIMULATOR_HAS_OPTION(HITL_GPS_TIMEOUT))
{
gpsSetState(GPS_LOST_COMMUNICATION);
sensorsClear(SENSOR_GPS);
gpsStats.timeouts = 5;
return false;
}
else
{
gpsSetState(GPS_RUNNING); gpsSetState(GPS_RUNNING);
sensorsSet(SENSOR_GPS); sensorsSet(SENSOR_GPS);
return gpsSol.flags.hasNewData; bool res = gpsSol.flags.hasNewData;
gpsSol.flags.hasNewData = false;
return res;
}
} }
#endif #endif

View file

@ -62,12 +62,17 @@ hardwareSensorStatus_e getHwAccelerometerStatus(void)
hardwareSensorStatus_e getHwCompassStatus(void) hardwareSensorStatus_e getHwCompassStatus(void)
{ {
#if defined(USE_MAG)
#ifdef USE_SIMULATOR #ifdef USE_SIMULATOR
if ((ARMING_FLAG(SIMULATOR_MODE_HITL) || ARMING_FLAG(SIMULATOR_MODE_SITL)) && sensors(SENSOR_MAG)) { if ((ARMING_FLAG(SIMULATOR_MODE_HITL) || ARMING_FLAG(SIMULATOR_MODE_SITL)) && sensors(SENSOR_MAG)) {
if (compassIsHealthy()) {
return HW_SENSOR_OK; return HW_SENSOR_OK;
} }
else {
return HW_SENSOR_UNHEALTHY;
}
}
#endif #endif
#if defined(USE_MAG)
if (detectedSensors[SENSOR_INDEX_MAG] != MAG_NONE) { if (detectedSensors[SENSOR_INDEX_MAG] != MAG_NONE) {
if (compassIsHealthy()) { if (compassIsHealthy()) {
return HW_SENSOR_OK; return HW_SENSOR_OK;

View file

@ -194,6 +194,13 @@ STATIC_PROTOTHREAD(pitotThread)
pt1FilterInit(&pitot.lpfState, pitotmeterConfig()->pitot_lpf_milli_hz / 1000.0f, 0.0f); pt1FilterInit(&pitot.lpfState, pitotmeterConfig()->pitot_lpf_milli_hz / 1000.0f, 0.0f);
while(1) { while(1) {
#ifdef USE_SIMULATOR
while (SIMULATOR_HAS_OPTION(HITL_AIRSPEED) && SIMULATOR_HAS_OPTION(HITL_PITOT_FAILURE))
{
ptDelayUs(10000);
}
#endif
// Start measurement // Start measurement
if (pitot.dev.start(&pitot.dev)) { if (pitot.dev.start(&pitot.dev)) {
pitot.lastSeenHealthyMs = millis(); pitot.lastSeenHealthyMs = millis();