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author | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-15 07:24:42 +0200 |
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committer | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-15 07:24:42 +0200 |
commit | 1744bf6e123f7870055daddedddd2e911d18e335 (patch) | |
tree | 284dc92de393942d1c99671d7b48015855d7865f /src/modules/ekf_att_pos_estimator | |
parent | f219c05f0f53ee8b8f5dbe24318678be6c255dd9 (diff) | |
parent | 23fe3b64be085b3a756a754478931867c5c25049 (diff) | |
download | px4-firmware-1744bf6e123f7870055daddedddd2e911d18e335.tar.gz px4-firmware-1744bf6e123f7870055daddedddd2e911d18e335.tar.bz2 px4-firmware-1744bf6e123f7870055daddedddd2e911d18e335.zip |
Merge branch 'master' of github.com:PX4/Firmware into eff_plus_plus
Diffstat (limited to 'src/modules/ekf_att_pos_estimator')
3 files changed, 83 insertions, 83 deletions
diff --git a/src/modules/ekf_att_pos_estimator/InertialNav b/src/modules/ekf_att_pos_estimator/InertialNav deleted file mode 160000 -Subproject 8b65d755b8c4834f90a323172c25d91c45068e2 diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp index bc40ce3c4..b3eb816f9 100644 --- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp @@ -129,6 +129,13 @@ public: int start(); /** + * Task status + * + * @return true if the mainloop is running + */ + bool task_running() { return _task_running; } + + /** * Print the current status. */ void print_status(); @@ -155,7 +162,8 @@ public: private: bool _task_should_exit; /**< if true, sensor task should exit */ - int _estimator_task; /**< task handle for sensor task */ + bool _task_running; /**< if true, task is running in its mainloop */ + int _estimator_task; /**< task handle for sensor task */ #ifndef SENSOR_COMBINED_SUB int _gyro_sub; /**< gyro sensor subscription */ int _accel_sub; /**< accel sensor subscription */ @@ -317,12 +325,13 @@ namespace estimator #endif static const int ERROR = -1; -FixedwingEstimator *g_estimator; +FixedwingEstimator *g_estimator = nullptr; } FixedwingEstimator::FixedwingEstimator() : _task_should_exit(false), + _task_running(false), _estimator_task(-1), /* subscriptions */ @@ -570,61 +579,26 @@ FixedwingEstimator::check_filter_state() int check = _ekf->CheckAndBound(&ekf_report); - const char* ekfname = "att pos estimator: "; - - switch (check) { - case 0: - /* all ok */ - break; - case 1: - { - const char* str = "NaN in states, resetting"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 2: - { - const char* str = "stale IMU data, resetting"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 3: - { - const char* str = "switching to dynamic state"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 4: - { - const char* str = "excessive gyro offsets"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 5: - { - const char* str = "GPS velocity divergence"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; - } - case 6: - { - const char* str = "excessive covariances"; - warnx("%s", str); - mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); - break; + const char* const feedback[] = { 0, + "NaN in states, resetting", + "stale IMU data, resetting", + "got initial position lock", + "excessive gyro offsets", + "GPS velocity divergence", + "excessive covariances", + "unknown condition"}; + + // Print out error condition + if (check) { + unsigned warn_index = static_cast<unsigned>(check); + unsigned max_warn_index = (sizeof(feedback) / sizeof(feedback[0])); + + if (max_warn_index < warn_index) { + warn_index = max_warn_index; } - default: - { - const char* str = "unknown reset condition"; - warnx("%s", str); - mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); - } + warnx("reset: %s", feedback[warn_index]); + mavlink_log_critical(_mavlink_fd, "[ekf] re-init: %s", feedback[warn_index]); } struct estimator_status_report rep; @@ -656,6 +630,10 @@ FixedwingEstimator::check_filter_state() rep.health_flags |= (((uint8_t)ekf_report.posHealth) << 1); rep.health_flags |= (((uint8_t)ekf_report.hgtHealth) << 2); rep.health_flags |= (((uint8_t)!ekf_report.gyroOffsetsExcessive) << 3); + // rep.health_flags |= (((uint8_t)ekf_report.onGround) << 4); + // rep.health_flags |= (((uint8_t)ekf_report.staticMode) << 5); + // rep.health_flags |= (((uint8_t)ekf_report.useCompass) << 6); + // rep.health_flags |= (((uint8_t)ekf_report.useAirspeed) << 7); rep.timeout_flags |= (((uint8_t)ekf_report.velTimeout) << 0); rep.timeout_flags |= (((uint8_t)ekf_report.posTimeout) << 1); @@ -783,6 +761,8 @@ FixedwingEstimator::task_main() _gps.vel_e_m_s = 0.0f; _gps.vel_d_m_s = 0.0f; + _task_running = true; + while (!_task_should_exit) { /* wait for up to 500ms for data */ @@ -1213,10 +1193,10 @@ FixedwingEstimator::task_main() _baro_gps_offset = 0.0f; _ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f); + } else if (_ekf->statesInitialised) { // We're apparently initialized in this case now - int check = check_filter_state(); if (check) { @@ -1224,7 +1204,6 @@ FixedwingEstimator::task_main() continue; } - // Run the strapdown INS equations every IMU update _ekf->UpdateStrapdownEquationsNED(); #if 0 @@ -1292,7 +1271,11 @@ FixedwingEstimator::task_main() // run the fusion step _ekf->FuseVelposNED(); - } else if (_ekf->statesInitialised) { + } else if (!_gps_initialized) { + + // force static mode + _ekf->staticMode = true; + // Convert GPS measurements to Pos NE, hgt and Vel NED _ekf->velNED[0] = 0.0f; _ekf->velNED[1] = 0.0f; @@ -1314,7 +1297,7 @@ FixedwingEstimator::task_main() _ekf->fusePosData = false; } - if (newHgtData && _ekf->statesInitialised) { + if (newHgtData) { // Could use a blend of GPS and baro alt data if desired _ekf->hgtMea = 1.0f * (_ekf->baroHgt - _baro_ref); _ekf->fuseHgtData = true; @@ -1328,7 +1311,7 @@ FixedwingEstimator::task_main() } // Fuse Magnetometer Measurements - if (newDataMag && _ekf->statesInitialised) { + if (newDataMag) { _ekf->fuseMagData = true; _ekf->RecallStates(_ekf->statesAtMagMeasTime, (IMUmsec - _parameters.mag_delay_ms)); // Assume 50 msec avg delay for magnetometer data @@ -1342,7 +1325,7 @@ FixedwingEstimator::task_main() } // Fuse Airspeed Measurements - if (newAdsData && _ekf->statesInitialised && _ekf->VtasMeas > 8.0f) { + if (newAdsData && _ekf->VtasMeas > 7.0f) { _ekf->fuseVtasData = true; _ekf->RecallStates(_ekf->statesAtVtasMeasTime, (IMUmsec - _parameters.tas_delay_ms)); // assume 100 msec avg delay for airspeed data _ekf->FuseAirspeed(); @@ -1410,7 +1393,7 @@ FixedwingEstimator::task_main() _velocity_xy_filtered = 0.95f*_velocity_xy_filtered + 0.05f*sqrtf(_local_pos.vx*_local_pos.vx + _local_pos.vy*_local_pos.vy); _velocity_z_filtered = 0.95f*_velocity_z_filtered + 0.05f*fabsf(_local_pos.vz); - _airspeed_filtered = 0.95f*_airspeed_filtered + + 0.05f*_airspeed.true_airspeed_m_s; + _airspeed_filtered = 0.95f*_airspeed_filtered + 0.05f*_airspeed.true_airspeed_m_s; /* crude land detector for fixedwing only, @@ -1501,27 +1484,28 @@ FixedwingEstimator::task_main() } - } - - } + if (hrt_elapsed_time(&_wind.timestamp) > 99000) { + _wind.timestamp = _global_pos.timestamp; + _wind.windspeed_north = _ekf->states[14]; + _wind.windspeed_east = _ekf->states[15]; + _wind.covariance_north = _ekf->P[14][14]; + _wind.covariance_east = _ekf->P[15][15]; - if (hrt_elapsed_time(&_wind.timestamp) > 99000) { - _wind.timestamp = _global_pos.timestamp; - _wind.windspeed_north = _ekf->states[14]; - _wind.windspeed_east = _ekf->states[15]; - _wind.covariance_north = _ekf->P[14][14]; - _wind.covariance_east = _ekf->P[15][15]; + /* lazily publish the wind estimate only once available */ + if (_wind_pub > 0) { + /* publish the wind estimate */ + orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); - /* lazily publish the wind estimate only once available */ - if (_wind_pub > 0) { - /* publish the wind estimate */ - orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); + } else { + /* advertise and publish */ + _wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); + } + } - } else { - /* advertise and publish */ - _wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); } + } + } } @@ -1529,6 +1513,8 @@ FixedwingEstimator::task_main() perf_end(_loop_perf); } + _task_running = false; + warnx("exiting.\n"); _estimator_task = -1; @@ -1681,6 +1667,14 @@ int ekf_att_pos_estimator_main(int argc, char *argv[]) err(1, "start failed"); } + /* avoid memory fragmentation by not exiting start handler until the task has fully started */ + while (estimator::g_estimator == nullptr || !estimator::g_estimator->task_running()) { + usleep(50000); + printf("."); + fflush(stdout); + } + printf("\n"); + exit(0); } diff --git a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp index 7f9486eb5..768e0be35 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp @@ -2279,7 +2279,7 @@ void AttPosEKF::calcLLH(float posNED[3], double &lat, double &lon, float &hgt, d void AttPosEKF::OnGroundCheck() { - onGround = (((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f) && (VtasMeas < 6.0f)); + onGround = (((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f) && (VtasMeas < 8.0f)); if (staticMode) { staticMode = (!refSet || (GPSstatus < GPS_FIX_3D)); } @@ -2879,12 +2879,18 @@ void AttPosEKF::InitializeDynamic(float (&initvelNED)[3], float declination) current_ekf_state.statesNaN = false; current_ekf_state.velHealth = true; - //current_ekf_state.posHealth = ?; - //current_ekf_state.hgtHealth = ?; + current_ekf_state.posHealth = true; + current_ekf_state.hgtHealth = true; current_ekf_state.velTimeout = false; - //current_ekf_state.posTimeout = ?; - //current_ekf_state.hgtTimeout = ?; + current_ekf_state.posTimeout = false; + current_ekf_state.hgtTimeout = false; + + fuseVelData = false; + fusePosData = false; + fuseHgtData = false; + fuseMagData = false; + fuseVtasData = false; // Fill variables with valid data velNED[0] = initvelNED[0]; |