From a4c99225c02e719d7900a533b777fd682eb5bd5c Mon Sep 17 00:00:00 2001 From: Thomas Gubler Date: Sun, 3 Nov 2013 16:49:02 +0100 Subject: initialize _vel_dot and _STEdotErrLast --- src/lib/external_lgpl/tecs/tecs.h | 4 +++- 1 file changed, 3 insertions(+), 1 deletion(-) diff --git a/src/lib/external_lgpl/tecs/tecs.h b/src/lib/external_lgpl/tecs/tecs.h index 4a98c8e97..f8f832ed7 100644 --- a/src/lib/external_lgpl/tecs/tecs.h +++ b/src/lib/external_lgpl/tecs/tecs.h @@ -54,7 +54,9 @@ public: _SPE_est(0.0f), _SKE_est(0.0f), _SPEdot(0.0f), - _SKEdot(0.0f) { + _SKEdot(0.0f), + _vel_dot(0.0f), + _STEdotErrLast(0.0f) { } -- cgit v1.2.3 From 98f5a77574fde4b2c41d28cc0d694f6ca250fba1 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 17:52:27 +0100 Subject: Fix to cancel pending callbacks for closing ORB topics --- src/modules/uORB/uORB.cpp | 5 +++-- 1 file changed, 3 insertions(+), 2 deletions(-) diff --git a/src/modules/uORB/uORB.cpp b/src/modules/uORB/uORB.cpp index 7abbf42ae..50e433ec3 100644 --- a/src/modules/uORB/uORB.cpp +++ b/src/modules/uORB/uORB.cpp @@ -249,9 +249,10 @@ ORBDevNode::close(struct file *filp) } else { SubscriberData *sd = filp_to_sd(filp); - if (sd != nullptr) + if (sd != nullptr) { + hrt_cancel(&sd->update_call); delete sd; - } + } return CDev::close(filp); } -- cgit v1.2.3 From 4865814f92c4a085972e317204c37042b609fdf8 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 17:58:28 +0100 Subject: Fixed typo, added testing - previous corner case now cleanly prevented --- src/modules/uORB/uORB.cpp | 1 + 1 file changed, 1 insertion(+) diff --git a/src/modules/uORB/uORB.cpp b/src/modules/uORB/uORB.cpp index 50e433ec3..149b8f6d2 100644 --- a/src/modules/uORB/uORB.cpp +++ b/src/modules/uORB/uORB.cpp @@ -253,6 +253,7 @@ ORBDevNode::close(struct file *filp) hrt_cancel(&sd->update_call); delete sd; } + } return CDev::close(filp); } -- cgit v1.2.3 From ba0687bc5e471809ae311ef98f3ddda3c29713b4 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 18:06:58 +0100 Subject: Matrix and Vector printing cleanup --- src/lib/mathlib/math/arm/Matrix.hpp | 6 +++--- src/lib/mathlib/math/arm/Vector.hpp | 6 +++--- 2 files changed, 6 insertions(+), 6 deletions(-) diff --git a/src/lib/mathlib/math/arm/Matrix.hpp b/src/lib/mathlib/math/arm/Matrix.hpp index 715fd3a5e..1945bb02d 100644 --- a/src/lib/mathlib/math/arm/Matrix.hpp +++ b/src/lib/mathlib/math/arm/Matrix.hpp @@ -121,10 +121,10 @@ public: for (size_t i = 0; i < getRows(); i++) { for (size_t j = 0; j < getCols(); j++) { float sig; - int exp; + int exponent; float num = (*this)(i, j); - float2SigExp(num, sig, exp); - printf("%6.3fe%03.3d,", (double)sig, exp); + float2SigExp(num, sig, exponent); + printf("%6.3fe%03d ", (double)sig, exponent); } printf("\n"); diff --git a/src/lib/mathlib/math/arm/Vector.hpp b/src/lib/mathlib/math/arm/Vector.hpp index 4155800e8..52220fc15 100644 --- a/src/lib/mathlib/math/arm/Vector.hpp +++ b/src/lib/mathlib/math/arm/Vector.hpp @@ -109,10 +109,10 @@ public: inline void print() const { for (size_t i = 0; i < getRows(); i++) { float sig; - int exp; + int exponent; float num = (*this)(i); - float2SigExp(num, sig, exp); - printf("%6.3fe%03.3d,", (double)sig, exp); + float2SigExp(num, sig, exponent); + printf("%6.3fe%03d ", (double)sig, exponent); } printf("\n"); -- cgit v1.2.3 From b53d86ed681eb6c9f979bb10d5f487fa9c94d81b Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 18:26:02 +0100 Subject: Hotfix for mag calibration --- src/modules/commander/mag_calibration.cpp | 29 +++++++++++++++++++---------- 1 file changed, 19 insertions(+), 10 deletions(-) diff --git a/src/modules/commander/mag_calibration.cpp b/src/modules/commander/mag_calibration.cpp index 09f4104f8..4ebf266f4 100644 --- a/src/modules/commander/mag_calibration.cpp +++ b/src/modules/commander/mag_calibration.cpp @@ -73,7 +73,7 @@ int do_mag_calibration(int mavlink_fd) /* maximum 500 values */ const unsigned int calibration_maxcount = 500; - unsigned int calibration_counter = 0; + unsigned int calibration_counter; struct mag_scale mscale_null = { 0.0f, @@ -99,28 +99,34 @@ int do_mag_calibration(int mavlink_fd) res = ioctl(fd, MAGIOCCALIBRATE, fd); if (res != OK) { - mavlink_log_critical(mavlink_fd, "ERROR: failed to calibrate scale"); + mavlink_log_critical(mavlink_fd, "Skipped scale calibration"); + /* this is non-fatal - mark it accordingly */ + res = OK; } } close(fd); - float *x; - float *y; - float *z; + float *x = NULL; + float *y = NULL; + float *z = NULL; if (res == OK) { /* allocate memory */ mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 20); - x = (float *)malloc(sizeof(float) * calibration_maxcount); - y = (float *)malloc(sizeof(float) * calibration_maxcount); - z = (float *)malloc(sizeof(float) * calibration_maxcount); + x = reinterpret_cast(malloc(sizeof(float) * calibration_maxcount)); + y = reinterpret_cast(malloc(sizeof(float) * calibration_maxcount)); + z = reinterpret_cast(malloc(sizeof(float) * calibration_maxcount)); if (x == NULL || y == NULL || z == NULL) { mavlink_log_critical(mavlink_fd, "ERROR: out of memory"); res = ERROR; + return res; } + } else { + /* exit */ + return ERROR; } if (res == OK) { @@ -136,6 +142,8 @@ int do_mag_calibration(int mavlink_fd) mavlink_log_info(mavlink_fd, "rotate in a figure 8 around all axis"); + calibration_counter = 0; + while (hrt_absolute_time() < calibration_deadline && calibration_counter < calibration_maxcount) { @@ -178,6 +186,7 @@ int do_mag_calibration(int mavlink_fd) float sphere_radius; if (res == OK) { + /* sphere fit */ mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 70); sphere_fit_least_squares(x, y, z, calibration_counter, 100, 0.0f, &sphere_x, &sphere_y, &sphere_z, &sphere_radius); @@ -270,7 +279,7 @@ int do_mag_calibration(int mavlink_fd) } else { mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); } - - return res; } + + return res; } -- cgit v1.2.3 From 791695ccd008859f6abe1a12d86b7be2ba811fec Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 18:26:39 +0100 Subject: Hotfix: Check for out of range accel values --- src/systemcmds/preflight_check/preflight_check.c | 28 ++++++++++++++++++++++-- 1 file changed, 26 insertions(+), 2 deletions(-) diff --git a/src/systemcmds/preflight_check/preflight_check.c b/src/systemcmds/preflight_check/preflight_check.c index 1c58a2db6..07581459b 100644 --- a/src/systemcmds/preflight_check/preflight_check.c +++ b/src/systemcmds/preflight_check/preflight_check.c @@ -109,7 +109,7 @@ int preflight_check_main(int argc, char *argv[]) /* ---- ACCEL ---- */ close(fd); - fd = open(ACCEL_DEVICE_PATH, 0); + fd = open(ACCEL_DEVICE_PATH, O_RDONLY); ret = ioctl(fd, ACCELIOCSELFTEST, 0); if (ret != OK) { @@ -119,6 +119,29 @@ int preflight_check_main(int argc, char *argv[]) goto system_eval; } + /* check measurement result range */ + struct accel_report acc; + ret = read(fd, &acc, sizeof(acc)); + + if (ret == sizeof(acc)) { + /* evaluate values */ + if (sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z) > 30.0f /* m/s^2 */) { + warnx("accel with spurious values"); + mavlink_log_critical(mavlink_fd, "SENSOR FAIL: |ACCEL| > 30 m/s^2"); + /* this is frickin' fatal */ + fail_on_error = true; + system_ok = false; + goto system_eval; + } + } else { + warnx("accel read failed"); + mavlink_log_critical(mavlink_fd, "SENSOR FAIL: ACCEL READ"); + /* this is frickin' fatal */ + fail_on_error = true; + system_ok = false; + goto system_eval; + } + /* ---- GYRO ---- */ close(fd); @@ -193,9 +216,10 @@ system_eval: /* stop alarm */ ioctl(buzzer, TONE_SET_ALARM, TONE_STOP_TUNE); - /* switch on leds */ + /* switch off leds */ led_on(leds, LED_BLUE); led_on(leds, LED_AMBER); + close(leds); if (fail_on_error) { /* exit with error message */ -- cgit v1.2.3 From 3042731d26e94b3c126e61e422b98fcd7df4694c Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 3 Nov 2013 18:27:26 +0100 Subject: Smaller hotfixes for att pos estimator --- src/modules/att_pos_estimator_ekf/KalmanNav.cpp | 9 +++------ 1 file changed, 3 insertions(+), 6 deletions(-) diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp b/src/modules/att_pos_estimator_ekf/KalmanNav.cpp index 33879892e..18fb6dcbc 100644 --- a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp +++ b/src/modules/att_pos_estimator_ekf/KalmanNav.cpp @@ -34,7 +34,7 @@ /** * @file KalmanNav.cpp * - * kalman filter navigation code + * Kalman filter navigation code */ #include @@ -228,10 +228,7 @@ void KalmanNav::update() updateSubscriptions(); // initialize attitude when sensors online - if (!_attitudeInitialized && sensorsUpdate && - _sensors.accelerometer_counter > 10 && - _sensors.gyro_counter > 10 && - _sensors.magnetometer_counter > 10) { + if (!_attitudeInitialized && sensorsUpdate) { if (correctAtt() == ret_ok) _attitudeInitCounter++; if (_attitudeInitCounter > 100) { @@ -643,7 +640,7 @@ int KalmanNav::correctAtt() if (beta > _faultAtt.get()) { warnx("fault in attitude: beta = %8.4f", (double)beta); - warnx("y:\n"); y.print(); + warnx("y:"); y.print(); } // update quaternions from euler -- cgit v1.2.3 From ed60dc50fcf2ab4dde76e937244bfb6eae81c709 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Tue, 5 Nov 2013 07:43:08 +0100 Subject: Hotfix: forbid integrator to accumulate NaN values if they ever would occur --- src/modules/fw_att_control/fw_att_control_main.cpp | 61 ++++++++++++---------- 1 file changed, 32 insertions(+), 29 deletions(-) diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index eb67874db..b3973084f 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -635,43 +635,46 @@ FixedwingAttitudeControl::task_main() } } - float roll_rad = _roll_ctrl.control(roll_sp, _att.roll, _att.rollspeed, - airspeed_scaling, lock_integrator, _parameters.airspeed_min, _parameters.airspeed_max, airspeed); - _actuators.control[0] = (isfinite(roll_rad)) ? roll_rad * actuator_scaling : 0.0f; + if (isfinite(roll_sp) && isfinite(pitch_sp)) { - float pitch_rad = _pitch_ctrl.control(pitch_sp, _att.pitch, _att.pitchspeed, _att.roll, airspeed_scaling, - lock_integrator, _parameters.airspeed_min, _parameters.airspeed_max, airspeed); - _actuators.control[1] = (isfinite(pitch_rad)) ? pitch_rad * actuator_scaling : 0.0f; + float roll_rad = _roll_ctrl.control(roll_sp, _att.roll, _att.rollspeed, + airspeed_scaling, lock_integrator, _parameters.airspeed_min, _parameters.airspeed_max, airspeed); + _actuators.control[0] = (isfinite(roll_rad)) ? roll_rad * actuator_scaling : 0.0f; - float yaw_rad = _yaw_ctrl.control(_att.roll, _att.yawspeed, _accel.y, airspeed_scaling, lock_integrator, - _parameters.airspeed_min, _parameters.airspeed_max, airspeed); - _actuators.control[2] = (isfinite(yaw_rad)) ? yaw_rad * actuator_scaling : 0.0f; + float pitch_rad = _pitch_ctrl.control(pitch_sp, _att.pitch, _att.pitchspeed, _att.roll, airspeed_scaling, + lock_integrator, _parameters.airspeed_min, _parameters.airspeed_max, airspeed); + _actuators.control[1] = (isfinite(pitch_rad)) ? pitch_rad * actuator_scaling : 0.0f; - /* throttle passed through */ - _actuators.control[3] = (isfinite(throttle_sp)) ? throttle_sp : 0.0f; + float yaw_rad = _yaw_ctrl.control(_att.roll, _att.yawspeed, _accel.y, airspeed_scaling, lock_integrator, + _parameters.airspeed_min, _parameters.airspeed_max, airspeed); + _actuators.control[2] = (isfinite(yaw_rad)) ? yaw_rad * actuator_scaling : 0.0f; - // warnx("aspd: %s: %6.2f, aspd scaling: %6.2f, controls: %5.2f %5.2f %5.2f %5.2f", (_airspeed_valid) ? "valid" : "unknown", - // airspeed, airspeed_scaling, _actuators.control[0], _actuators.control[1], - // _actuators.control[2], _actuators.control[3]); + /* throttle passed through */ + _actuators.control[3] = (isfinite(throttle_sp)) ? throttle_sp : 0.0f; - /* - * Lazily publish the rate setpoint (for analysis, the actuators are published below) - * only once available - */ - vehicle_rates_setpoint_s rates_sp; - rates_sp.roll = _roll_ctrl.get_desired_rate(); - rates_sp.pitch = _pitch_ctrl.get_desired_rate(); - rates_sp.yaw = 0.0f; // XXX not yet implemented + // warnx("aspd: %s: %6.2f, aspd scaling: %6.2f, controls: %5.2f %5.2f %5.2f %5.2f", (_airspeed_valid) ? "valid" : "unknown", + // airspeed, airspeed_scaling, _actuators.control[0], _actuators.control[1], + // _actuators.control[2], _actuators.control[3]); - rates_sp.timestamp = hrt_absolute_time(); + /* + * Lazily publish the rate setpoint (for analysis, the actuators are published below) + * only once available + */ + vehicle_rates_setpoint_s rates_sp; + rates_sp.roll = _roll_ctrl.get_desired_rate(); + rates_sp.pitch = _pitch_ctrl.get_desired_rate(); + rates_sp.yaw = 0.0f; // XXX not yet implemented - if (_rate_sp_pub > 0) { - /* publish the attitude setpoint */ - orb_publish(ORB_ID(vehicle_rates_setpoint), _rate_sp_pub, &rates_sp); + rates_sp.timestamp = hrt_absolute_time(); - } else { - /* advertise and publish */ - _rate_sp_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint), &rates_sp); + if (_rate_sp_pub > 0) { + /* publish the attitude setpoint */ + orb_publish(ORB_ID(vehicle_rates_setpoint), _rate_sp_pub, &rates_sp); + + } else { + /* advertise and publish */ + _rate_sp_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint), &rates_sp); + } } } else { -- cgit v1.2.3 From 1358d4cb88e70370014410353faf3e51afb1ceb6 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Tue, 5 Nov 2013 07:44:16 +0100 Subject: Hotfix: Fix integrator parameters --- src/modules/fw_att_control/fw_att_control_main.cpp | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index b3973084f..00a0dcd61 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -279,20 +279,20 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() : _parameter_handles.p_i = param_find("FW_P_I"); _parameter_handles.p_rmax_pos = param_find("FW_P_RMAX_POS"); _parameter_handles.p_rmax_neg = param_find("FW_P_RMAX_NEG"); - _parameter_handles.p_integrator_max = param_find("FW_P_integrator_max"); + _parameter_handles.p_integrator_max = param_find("FW_P_IMAX"); _parameter_handles.p_roll_feedforward = param_find("FW_P_ROLLFF"); _parameter_handles.r_p = param_find("FW_R_P"); _parameter_handles.r_d = param_find("FW_R_D"); _parameter_handles.r_i = param_find("FW_R_I"); - _parameter_handles.r_integrator_max = param_find("FW_R_integrator_max"); + _parameter_handles.r_integrator_max = param_find("FW_R_IMAX"); _parameter_handles.r_rmax = param_find("FW_R_RMAX"); _parameter_handles.y_p = param_find("FW_Y_P"); _parameter_handles.y_i = param_find("FW_Y_I"); _parameter_handles.y_d = param_find("FW_Y_D"); _parameter_handles.y_roll_feedforward = param_find("FW_Y_ROLLFF"); - _parameter_handles.y_integrator_max = param_find("FW_Y_integrator_max"); + _parameter_handles.y_integrator_max = param_find("FW_Y_IMAX"); _parameter_handles.airspeed_min = param_find("FW_AIRSPD_MIN"); _parameter_handles.airspeed_trim = param_find("FW_AIRSPD_TRIM"); -- cgit v1.2.3 From d3b267c06e53aaf119b66717ac33e78834ea0d69 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Tue, 5 Nov 2013 09:20:07 +0100 Subject: Integral fixes, last parts --- src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp | 5 ++--- src/lib/ecl/attitude_fw/ecl_roll_controller.cpp | 7 +++++-- 2 files changed, 7 insertions(+), 5 deletions(-) diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp index d876f1a39..2eb58abd6 100644 --- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp @@ -62,8 +62,7 @@ float ECL_PitchController::control(float pitch_setpoint, float pitch, float pitc /* get the usual dt estimate */ uint64_t dt_micros = ecl_elapsed_time(&_last_run); _last_run = ecl_absolute_time(); - - float dt = dt_micros / 1000000; + float dt = (float)dt_micros * 1e-6f; /* lock integral for long intervals */ if (dt_micros > 500000) @@ -115,7 +114,7 @@ float ECL_PitchController::control(float pitch_setpoint, float pitch, float pitc _rate_error = _rate_setpoint - pitch_rate; - float ilimit_scaled = 0.0f; + float ilimit_scaled = _integrator_max * scaler; if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5f * airspeed_min) { diff --git a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp index b9a73fc02..0b1ffa7a4 100644 --- a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp @@ -64,8 +64,11 @@ float ECL_RollController::control(float roll_setpoint, float roll, float roll_ra /* get the usual dt estimate */ uint64_t dt_micros = ecl_elapsed_time(&_last_run); _last_run = ecl_absolute_time(); + float dt = (float)dt_micros * 1e-6f; - float dt = (dt_micros > 500000) ? 0.0f : dt_micros / 1000000; + /* lock integral for long intervals */ + if (dt_micros > 500000) + lock_integrator = true; float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f); float k_i_rate = _k_i * _tc; @@ -90,7 +93,7 @@ float ECL_RollController::control(float roll_setpoint, float roll, float roll_ra _rate_error = _rate_setpoint - roll_rate; - float ilimit_scaled = 0.0f; + float ilimit_scaled = _integrator_max * scaler; if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5f * airspeed_min) { -- cgit v1.2.3 From 857c3d2efd49085dfd28827b06d96776340e5a09 Mon Sep 17 00:00:00 2001 From: Julian Oes Date: Tue, 5 Nov 2013 16:59:34 +0100 Subject: Startup scripts: Corrected cases where commander was not started, updated several outdated scripts --- ROMFS/px4fmu_common/init.d/100_mpx_easystar | 35 ++++-------------- ROMFS/px4fmu_common/init.d/101_hk_bixler | 36 ++++++------------ ROMFS/px4fmu_common/init.d/10_dji_f330 | 5 +-- ROMFS/px4fmu_common/init.d/11_dji_f450 | 2 +- ROMFS/px4fmu_common/init.d/12-13_hex | 15 +++++--- ROMFS/px4fmu_common/init.d/15_tbs_discovery | 10 ++--- ROMFS/px4fmu_common/init.d/16_3dr_iris | 4 +- ROMFS/px4fmu_common/init.d/30_io_camflyer | 38 ++++++------------- ROMFS/px4fmu_common/init.d/31_io_phantom | 38 ++++++------------- ROMFS/px4fmu_common/init.d/32_skywalker_x5 | 31 +++------------- ROMFS/px4fmu_common/init.d/666_fmu_q_x550 | 43 ++++++++++++++++------ .../init.d/rc.custom_dji_f330_mkblctrl | 2 +- ROMFS/px4fmu_common/init.d/rc.custom_io_esc | 4 +- ROMFS/px4fmu_common/init.d/rc.fixedwing | 39 ++++++++++++++++++++ ROMFS/px4fmu_common/init.d/rc.multirotor | 7 +++- 15 files changed, 141 insertions(+), 168 deletions(-) create mode 100644 ROMFS/px4fmu_common/init.d/rc.fixedwing diff --git a/ROMFS/px4fmu_common/init.d/100_mpx_easystar b/ROMFS/px4fmu_common/init.d/100_mpx_easystar index 4f843e9aa..b797ceebc 100644 --- a/ROMFS/px4fmu_common/init.d/100_mpx_easystar +++ b/ROMFS/px4fmu_common/init.d/100_mpx_easystar @@ -52,8 +52,6 @@ then # Start MAVLink (depends on orb) mavlink start - commander start - sh /etc/init.d/rc.io # Limit to 100 Hz updates and (implicit) 50 Hz PWM px4io limit 100 @@ -61,46 +59,27 @@ else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 - commander start - fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi -# -# Start the sensors and test them. -# -sh /etc/init.d/rc.sensors - -# -# Start logging (depends on sensors) -# -sh /etc/init.d/rc.logging - -# -# Start GPS interface (depends on orb) -# -gps start - -# -# Start the attitude and position estimator -# -att_pos_estimator_ekf start - # # Load mixer and start controllers (depends on px4io) # if [ -f /fs/microsd/etc/mixers/FMU_RET.mix ] then - echo "Using FMU_RET mixer from sd card" + echo "Using /fs/microsd/etc/mixers/FMU_RET.mix" mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_RET.mix else - echo "Using standard FMU_RET mixer" + echo "Using /etc/mixers/FMU_RET.mix" mixer load /dev/pwm_output /etc/mixers/FMU_RET.mix fi -fw_att_control start -fw_pos_control_l1 start + +# +Start common fixedwing apps +# +sh /etc/init.d/rc.fixedwing if [ $EXIT_ON_END == yes ] then diff --git a/ROMFS/px4fmu_common/init.d/101_hk_bixler b/ROMFS/px4fmu_common/init.d/101_hk_bixler index cef86c34d..920a24e2f 100644 --- a/ROMFS/px4fmu_common/init.d/101_hk_bixler +++ b/ROMFS/px4fmu_common/init.d/101_hk_bixler @@ -52,8 +52,6 @@ then # Start MAVLink (depends on orb) mavlink start - commander start - sh /etc/init.d/rc.io # Limit to 100 Hz updates and (implicit) 50 Hz PWM px4io limit 100 @@ -61,39 +59,27 @@ else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 - commander start - fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi - -# -# Start the sensors and test them. -# -sh /etc/init.d/rc.sensors # -# Start logging (depends on sensors) +# Load mixer and start controllers (depends on px4io) # -sh /etc/init.d/rc.logging +if [ -f /fs/microsd/etc/mixers/FMU_AERT.mix ] +then + echo "Using /fs/microsd/etc/mixers/FMU_AERT.mix" + mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_AERT.mix +else + echo "Using /etc/mixers/FMU_Q.mix" + mixer load /dev/pwm_output /etc/mixers/FMU_AERT.mix +fi # -# Start GPS interface (depends on orb) -# -gps start - -# -# Start the attitude and position estimator -# -att_pos_estimator_ekf start - -# -# Load mixer and start controllers (depends on px4io) +Start common fixedwing apps # -mixer load /dev/pwm_output /etc/mixers/FMU_AERT.mix -fw_att_control start -fw_pos_control_l1 start +sh /etc/init.d/rc.fixedwing if [ $EXIT_ON_END == yes ] then diff --git a/ROMFS/px4fmu_common/init.d/10_dji_f330 b/ROMFS/px4fmu_common/init.d/10_dji_f330 index 81ea292aa..467b56bbf 100644 --- a/ROMFS/px4fmu_common/init.d/10_dji_f330 +++ b/ROMFS/px4fmu_common/init.d/10_dji_f330 @@ -59,10 +59,7 @@ then mavlink start usleep 5000 - commander start - sh /etc/init.d/rc.io - # Set PWM values for DJI ESCs else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 @@ -83,7 +80,7 @@ mixer load /dev/pwm_output /etc/mixers/FMU_quad_x.mix pwm rate -c 1234 -r 400 # -# Set disarmed, min and max PWM signals +# Set disarmed, min and max PWM signals (for DJI ESCs) # pwm disarmed -c 1234 -p 900 pwm min -c 1234 -p 1200 diff --git a/ROMFS/px4fmu_common/init.d/11_dji_f450 b/ROMFS/px4fmu_common/init.d/11_dji_f450 index 4dbf76cee..818f9375e 100644 --- a/ROMFS/px4fmu_common/init.d/11_dji_f450 +++ b/ROMFS/px4fmu_common/init.d/11_dji_f450 @@ -73,7 +73,7 @@ pwm min -c 1234 -p 1200 pwm max -c 1234 -p 1800 # -# Start common for all multirotors apps +# Start common multirotor apps # sh /etc/init.d/rc.multirotor diff --git a/ROMFS/px4fmu_common/init.d/12-13_hex b/ROMFS/px4fmu_common/init.d/12-13_hex index 0f0bb05ce..f83f6cfd0 100644 --- a/ROMFS/px4fmu_common/init.d/12-13_hex +++ b/ROMFS/px4fmu_common/init.d/12-13_hex @@ -61,10 +61,6 @@ then usleep 5000 sh /etc/init.d/rc.io - # Set PWM values for DJI ESCs - px4io idle 900 900 900 900 900 900 - px4io min 1200 1200 1200 1200 1200 1200 - px4io max 1900 1900 1900 1900 1900 1900 else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 @@ -77,12 +73,19 @@ fi # # Load mixer # -mixer load /dev/pwm_output $MIXER +mixer load /dev/pwm_output /etc/mixers/FMU_hex_x.mix # # Set PWM output frequency to 400 Hz # -pwm -u 400 -m 0xff +pwm rate -c 123456 -r 400 + +# +# Set disarmed, min and max PWM signals +# +pwm disarmed -c 123456 -p 900 +pwm min -c 123456 -p 1100 +pwm max -c 123456 -p 1900 # # Start common for all multirotors apps diff --git a/ROMFS/px4fmu_common/init.d/15_tbs_discovery b/ROMFS/px4fmu_common/init.d/15_tbs_discovery index bd6189a6d..c79e9d283 100644 --- a/ROMFS/px4fmu_common/init.d/15_tbs_discovery +++ b/ROMFS/px4fmu_common/init.d/15_tbs_discovery @@ -31,7 +31,7 @@ fi # MAV_TYPE 2 = quadrotor # param set MAV_TYPE 2 - + set EXIT_ON_END no # @@ -43,8 +43,6 @@ then mavlink start usleep 5000 - commander start - sh /etc/init.d/rc.io else # Start MAVLink (on UART1 / ttyS0) @@ -66,11 +64,11 @@ mixer load /dev/pwm_output /etc/mixers/FMU_quad_w.mix pwm rate -c 1234 -r 400 # -# Set disarmed, min and max PWM signals (for DJI ESCs) +# Set disarmed, min and max PWM signals # pwm disarmed -c 1234 -p 900 -pwm min -c 1234 -p 1200 -pwm max -c 1234 -p 1800 +pwm min -c 1234 -p 1100 +pwm max -c 1234 -p 1900 # # Start common for all multirotors apps diff --git a/ROMFS/px4fmu_common/init.d/16_3dr_iris b/ROMFS/px4fmu_common/init.d/16_3dr_iris index d8cc0e913..6be917878 100644 --- a/ROMFS/px4fmu_common/init.d/16_3dr_iris +++ b/ROMFS/px4fmu_common/init.d/16_3dr_iris @@ -31,7 +31,7 @@ fi # MAV_TYPE 2 = quadrotor # param set MAV_TYPE 2 - + set EXIT_ON_END no # @@ -43,8 +43,6 @@ then mavlink start usleep 5000 - commander start - sh /etc/init.d/rc.io else # Start MAVLink (on UART1 / ttyS0) diff --git a/ROMFS/px4fmu_common/init.d/30_io_camflyer b/ROMFS/px4fmu_common/init.d/30_io_camflyer index 191d8cd95..ffab26c38 100644 --- a/ROMFS/px4fmu_common/init.d/30_io_camflyer +++ b/ROMFS/px4fmu_common/init.d/30_io_camflyer @@ -30,8 +30,6 @@ then # Start MAVLink (depends on orb) mavlink start - commander start - sh /etc/init.d/rc.io # Limit to 100 Hz updates and (implicit) 50 Hz PWM px4io limit 100 @@ -39,41 +37,29 @@ else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 - commander start - fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi - -# -# Start the sensors and test them. -# -sh /etc/init.d/rc.sensors # -# Start logging (depends on sensors) +# Load mixer and start controllers (depends on px4io) # -sh /etc/init.d/rc.logging +if [ -f /fs/microsd/etc/mixers/FMU_Q.mix ] +then + echo "Using /fs/microsd/etc/mixers/FMU_Q.mix" + mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_Q.mix +else + echo "Using /etc/mixers/FMU_Q.mix" + mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix +fi # -# Start GPS interface (depends on orb) +Start common fixedwing apps # -gps start - -# -# Start the attitude and position estimator -# -att_pos_estimator_ekf start - -# -# Load mixer and start controllers (depends on px4io) -# -mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix -fw_att_control start -fw_pos_control_l1 start +sh /etc/init.d/rc.fixedwing if [ $EXIT_ON_END == yes ] then exit -fi +fi \ No newline at end of file diff --git a/ROMFS/px4fmu_common/init.d/31_io_phantom b/ROMFS/px4fmu_common/init.d/31_io_phantom index 652833745..14607e2df 100644 --- a/ROMFS/px4fmu_common/init.d/31_io_phantom +++ b/ROMFS/px4fmu_common/init.d/31_io_phantom @@ -52,8 +52,6 @@ then # Start MAVLink (depends on orb) mavlink start - commander start - sh /etc/init.d/rc.io # Limit to 100 Hz updates and (implicit) 50 Hz PWM px4io limit 100 @@ -61,41 +59,29 @@ else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 - commander start - fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi - -# -# Start the sensors and test them. -# -sh /etc/init.d/rc.sensors # -# Start logging (depends on sensors) +# Load mixer and start controllers (depends on px4io) # -sh /etc/init.d/rc.logging +if [ -f /fs/microsd/etc/mixers/FMU_Q.mix ] +then + echo "Using /fs/microsd/etc/mixers/FMU_Q.mix" + mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_Q.mix +else + echo "Using /etc/mixers/FMU_Q.mix" + mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix +fi # -# Start GPS interface (depends on orb) +Start common fixedwing apps # -gps start - -# -# Start the attitude and position estimator -# -att_pos_estimator_ekf start - -# -# Load mixer and start controllers (depends on px4io) -# -mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix -fw_att_control start -fw_pos_control_l1 start +sh /etc/init.d/rc.fixedwing if [ $EXIT_ON_END == yes ] then exit -fi +fi \ No newline at end of file diff --git a/ROMFS/px4fmu_common/init.d/32_skywalker_x5 b/ROMFS/px4fmu_common/init.d/32_skywalker_x5 index cd7677112..11071613c 100644 --- a/ROMFS/px4fmu_common/init.d/32_skywalker_x5 +++ b/ROMFS/px4fmu_common/init.d/32_skywalker_x5 @@ -30,8 +30,6 @@ then # Start MAVLink (depends on orb) mavlink start - commander start - sh /etc/init.d/rc.io # Limit to 100 Hz updates and (implicit) 50 Hz PWM px4io limit 100 @@ -39,32 +37,10 @@ else # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 - commander start - fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi - -# -# Start the sensors and test them. -# -sh /etc/init.d/rc.sensors - -# -# Start logging (depends on sensors) -# -sh /etc/init.d/rc.logging - -# -# Start GPS interface (depends on orb) -# -gps start - -# -# Start the attitude and position estimator -# -att_pos_estimator_ekf start # # Load mixer and start controllers (depends on px4io) @@ -77,8 +53,11 @@ else echo "Using /etc/mixers/FMU_Q.mix" mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix fi -fw_att_control start -fw_pos_control_l1 start + +# +Start common fixedwing apps +# +sh /etc/init.d/rc.fixedwing if [ $EXIT_ON_END == yes ] then diff --git a/ROMFS/px4fmu_common/init.d/666_fmu_q_x550 b/ROMFS/px4fmu_common/init.d/666_fmu_q_x550 index eae37098b..1ee84b9b0 100644 --- a/ROMFS/px4fmu_common/init.d/666_fmu_q_x550 +++ b/ROMFS/px4fmu_common/init.d/666_fmu_q_x550 @@ -1,6 +1,6 @@ #!nsh -echo "[init] 666_fmu_q_x550: PX4FMU Quad X550 with PWM outputs" +echo "[init] 666_fmu_q_x550: PX4FMU Quad X550 with or without IO" # # Load default params for this platform @@ -33,17 +33,27 @@ fi # MAV_TYPE 2 = quadrotor # param set MAV_TYPE 2 - -# -# Start MAVLink -# -mavlink start -d /dev/ttyS0 -b 57600 -usleep 5000 + +set EXIT_ON_END no # -# Start PWM output +# Start and configure PX4IO or FMU interface # -fmu mode_pwm +if px4io detect +then + # Start MAVLink (depends on orb) + mavlink start + usleep 5000 + + sh /etc/init.d/rc.io +else + # Start MAVLink (on UART1 / ttyS0) + mavlink start -d /dev/ttyS0 + usleep 5000 + fmu mode_pwm + param set BAT_V_SCALING 0.004593 + set EXIT_ON_END yes +fi # # Load mixer @@ -55,10 +65,19 @@ mixer load /dev/pwm_output /etc/mixers/FMU_quad_x.mix # pwm rate -c 1234 -r 400 +# +# Set disarmed, min and max PWM signals +# +pwm disarmed -c 1234 -p 900 +pwm min -c 1234 -p 1100 +pwm max -c 1234 -p 1900 + # # Start common for all multirotors apps # sh /etc/init.d/rc.multirotor - -# Exit, because /dev/ttyS0 is needed for MAVLink -exit + +if [ $EXIT_ON_END == yes ] +then + exit +fi diff --git a/ROMFS/px4fmu_common/init.d/rc.custom_dji_f330_mkblctrl b/ROMFS/px4fmu_common/init.d/rc.custom_dji_f330_mkblctrl index a63d0e5f1..4686382ca 100644 --- a/ROMFS/px4fmu_common/init.d/rc.custom_dji_f330_mkblctrl +++ b/ROMFS/px4fmu_common/init.d/rc.custom_dji_f330_mkblctrl @@ -84,10 +84,10 @@ then sh /etc/init.d/rc.io else - fmu mode_pwm # Start MAVLink (on UART1 / ttyS0) mavlink start -d /dev/ttyS0 usleep 5000 + fmu mode_pwm param set BAT_V_SCALING 0.004593 set EXIT_ON_END yes fi diff --git a/ROMFS/px4fmu_common/init.d/rc.custom_io_esc b/ROMFS/px4fmu_common/init.d/rc.custom_io_esc index 0c0cfa53d..045e41e52 100644 --- a/ROMFS/px4fmu_common/init.d/rc.custom_io_esc +++ b/ROMFS/px4fmu_common/init.d/rc.custom_io_esc @@ -60,9 +60,7 @@ then # Start MAVLink (depends on orb) mavlink start -d /dev/ttyS1 -b 57600 usleep 5000 - - commander start - + sh /etc/init.d/rc.io else fmu mode_pwm diff --git a/ROMFS/px4fmu_common/init.d/rc.fixedwing b/ROMFS/px4fmu_common/init.d/rc.fixedwing new file mode 100644 index 000000000..79e34a3b9 --- /dev/null +++ b/ROMFS/px4fmu_common/init.d/rc.fixedwing @@ -0,0 +1,39 @@ +#!nsh +# +# Standard everything needed for fixedwing except mixer, actuator output and mavlink +# + +# +# Start the Commander +# +commander start + +# +# Start the sensors and test them. +# +sh /etc/init.d/rc.sensors + +# +# Start logging (depends on sensors) +# +sh /etc/init.d/rc.logging + +# +# Start GPS interface (depends on orb) +# +gps start + +# +# Start the attitude and position estimator +# +att_pos_estimator_ekf start + +# +# Start attitude controller +# +fw_att_control start + +# +# Start the position controller +# +fw_pos_control_l1 start diff --git a/ROMFS/px4fmu_common/init.d/rc.multirotor b/ROMFS/px4fmu_common/init.d/rc.multirotor index dfff07198..6bae99175 100644 --- a/ROMFS/px4fmu_common/init.d/rc.multirotor +++ b/ROMFS/px4fmu_common/init.d/rc.multirotor @@ -1,8 +1,13 @@ #!nsh # -# Standard everything needed for multirotors except mixer, output and mavlink +# Standard everything needed for multirotors except mixer, actuator output and mavlink # +# +# Start the Commander +# +commander start + # # Start the sensors and test them. # -- cgit v1.2.3 From 4502c285eb8b284b7c08666b6d0e3e81035bace3 Mon Sep 17 00:00:00 2001 From: Julian Oes Date: Tue, 5 Nov 2013 19:56:33 +0100 Subject: Startup scripts: Start the commander early and let it try to open the mavlink_fd with 20Hz --- ROMFS/px4fmu_common/init.d/rc.fixedwing | 5 ----- ROMFS/px4fmu_common/init.d/rc.multirotor | 5 ----- ROMFS/px4fmu_common/init.d/rcS | 5 +++++ src/modules/commander/commander.cpp | 17 +++++++---------- 4 files changed, 12 insertions(+), 20 deletions(-) diff --git a/ROMFS/px4fmu_common/init.d/rc.fixedwing b/ROMFS/px4fmu_common/init.d/rc.fixedwing index 79e34a3b9..f02851006 100644 --- a/ROMFS/px4fmu_common/init.d/rc.fixedwing +++ b/ROMFS/px4fmu_common/init.d/rc.fixedwing @@ -3,11 +3,6 @@ # Standard everything needed for fixedwing except mixer, actuator output and mavlink # -# -# Start the Commander -# -commander start - # # Start the sensors and test them. # diff --git a/ROMFS/px4fmu_common/init.d/rc.multirotor b/ROMFS/px4fmu_common/init.d/rc.multirotor index 6bae99175..bc550ac5a 100644 --- a/ROMFS/px4fmu_common/init.d/rc.multirotor +++ b/ROMFS/px4fmu_common/init.d/rc.multirotor @@ -3,11 +3,6 @@ # Standard everything needed for multirotors except mixer, actuator output and mavlink # -# -# Start the Commander -# -commander start - # # Start the sensors and test them. # diff --git a/ROMFS/px4fmu_common/init.d/rcS b/ROMFS/px4fmu_common/init.d/rcS index cff8446a6..d8b5cb608 100755 --- a/ROMFS/px4fmu_common/init.d/rcS +++ b/ROMFS/px4fmu_common/init.d/rcS @@ -105,6 +105,11 @@ then blinkm systemstate fi fi + + # + # Start the Commander (needs to be this early for in-air-restarts) + # + commander start if param compare SYS_AUTOSTART 1000 then diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index ed090271c..ace13bb78 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -116,6 +116,8 @@ extern struct system_load_s system_load; #define LOW_VOLTAGE_BATTERY_COUNTER_LIMIT (LOW_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS*COMMANDER_MONITORING_LOOPSPERMSEC) #define CRITICAL_VOLTAGE_BATTERY_COUNTER_LIMIT (CRITICAL_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS*COMMANDER_MONITORING_LOOPSPERMSEC) +#define MAVLINK_OPEN_INTERVAL 50000 + #define STICK_ON_OFF_LIMIT 0.75f #define STICK_THRUST_RANGE 1.0f #define STICK_ON_OFF_HYSTERESIS_TIME_MS 1000 @@ -582,16 +584,6 @@ int commander_thread_main(int argc, char *argv[]) mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); - if (mavlink_fd < 0) { - /* try again later */ - usleep(20000); - mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); - - if (mavlink_fd < 0) { - warnx("ERROR: Failed to open MAVLink log stream again, start mavlink app first."); - } - } - /* Main state machine */ /* make sure we are in preflight state */ memset(&status, 0, sizeof(status)); @@ -770,6 +762,11 @@ int commander_thread_main(int argc, char *argv[]) while (!thread_should_exit) { + if (mavlink_fd < 0 && counter % (1000000 / MAVLINK_OPEN_INTERVAL) == 0) { + /* try to open the mavlink log device every once in a while */ + mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); + } + /* update parameters */ orb_check(param_changed_sub, &updated); -- cgit v1.2.3 From 9b08923cd2422117d8c1e05fb0ccddc4bf00528f Mon Sep 17 00:00:00 2001 From: Thomas Gubler Date: Wed, 6 Nov 2013 17:01:29 +0100 Subject: remove commander from hil startup scripts --- ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil | 5 ----- ROMFS/px4fmu_common/init.d/1001_rc_quad.hil | 5 ----- ROMFS/px4fmu_common/init.d/1002_rc_fw_state.hil | 5 ----- ROMFS/px4fmu_common/init.d/1003_rc_quad_+.hil | 5 ----- ROMFS/px4fmu_common/init.d/1004_rc_fw_Rascal110.hil | 5 ----- 5 files changed, 25 deletions(-) diff --git a/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil b/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil index 5e4028bbb..40a13b5d1 100644 --- a/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil +++ b/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil @@ -55,11 +55,6 @@ hil mode_pwm # param set MAV_TYPE 1 -# -# Start the commander (depends on orb, mavlink) -# -commander start - # # Check if we got an IO # diff --git a/ROMFS/px4fmu_common/init.d/1001_rc_quad.hil b/ROMFS/px4fmu_common/init.d/1001_rc_quad.hil index bbe3b7e28..9b664d63e 100644 --- a/ROMFS/px4fmu_common/init.d/1001_rc_quad.hil +++ b/ROMFS/px4fmu_common/init.d/1001_rc_quad.hil @@ -60,11 +60,6 @@ hil mode_pwm # param set MAV_TYPE 2 -# -# Start the commander (depends on orb, mavlink) -# -commander start - # # Check if we got an IO # diff --git a/ROMFS/px4fmu_common/init.d/1002_rc_fw_state.hil b/ROMFS/px4fmu_common/init.d/1002_rc_fw_state.hil index d5782a89b..7b9f41bf6 100644 --- a/ROMFS/px4fmu_common/init.d/1002_rc_fw_state.hil +++ b/ROMFS/px4fmu_common/init.d/1002_rc_fw_state.hil @@ -52,11 +52,6 @@ hil mode_pwm # param set MAV_TYPE 1 -# -# Start the commander (depends on orb, mavlink) -# -commander start - # # Check if we got an IO # diff --git a/ROMFS/px4fmu_common/init.d/1003_rc_quad_+.hil b/ROMFS/px4fmu_common/init.d/1003_rc_quad_+.hil index 1c85e04f2..0cc07ad34 100644 --- a/ROMFS/px4fmu_common/init.d/1003_rc_quad_+.hil +++ b/ROMFS/px4fmu_common/init.d/1003_rc_quad_+.hil @@ -60,11 +60,6 @@ hil mode_pwm # param set MAV_TYPE 2 -# -# Start the commander (depends on orb, mavlink) -# -commander start - # # Check if we got an IO # diff --git a/ROMFS/px4fmu_common/init.d/1004_rc_fw_Rascal110.hil b/ROMFS/px4fmu_common/init.d/1004_rc_fw_Rascal110.hil index 8c5e4b6a8..344d78422 100644 --- a/ROMFS/px4fmu_common/init.d/1004_rc_fw_Rascal110.hil +++ b/ROMFS/px4fmu_common/init.d/1004_rc_fw_Rascal110.hil @@ -55,11 +55,6 @@ hil mode_pwm # param set MAV_TYPE 1 -# -# Start the commander (depends on orb, mavlink) -# -commander start - # # Check if we got an IO # -- cgit v1.2.3 From 2af2bacc4fe081852da40a329b275d17629a705c Mon Sep 17 00:00:00 2001 From: Julian Oes Date: Wed, 6 Nov 2013 23:41:15 +0100 Subject: Startup scripts: fixed stupid typo --- ROMFS/px4fmu_common/init.d/100_mpx_easystar | 2 +- ROMFS/px4fmu_common/init.d/101_hk_bixler | 2 +- ROMFS/px4fmu_common/init.d/30_io_camflyer | 2 +- ROMFS/px4fmu_common/init.d/31_io_phantom | 2 +- ROMFS/px4fmu_common/init.d/32_skywalker_x5 | 2 +- 5 files changed, 5 insertions(+), 5 deletions(-) diff --git a/ROMFS/px4fmu_common/init.d/100_mpx_easystar b/ROMFS/px4fmu_common/init.d/100_mpx_easystar index b797ceebc..abe378b22 100644 --- a/ROMFS/px4fmu_common/init.d/100_mpx_easystar +++ b/ROMFS/px4fmu_common/init.d/100_mpx_easystar @@ -77,7 +77,7 @@ else fi # -Start common fixedwing apps +# Start common fixedwing apps # sh /etc/init.d/rc.fixedwing diff --git a/ROMFS/px4fmu_common/init.d/101_hk_bixler b/ROMFS/px4fmu_common/init.d/101_hk_bixler index 920a24e2f..c616da988 100644 --- a/ROMFS/px4fmu_common/init.d/101_hk_bixler +++ b/ROMFS/px4fmu_common/init.d/101_hk_bixler @@ -77,7 +77,7 @@ else fi # -Start common fixedwing apps +# Start common fixedwing apps # sh /etc/init.d/rc.fixedwing diff --git a/ROMFS/px4fmu_common/init.d/30_io_camflyer b/ROMFS/px4fmu_common/init.d/30_io_camflyer index ffab26c38..8a8bc1590 100644 --- a/ROMFS/px4fmu_common/init.d/30_io_camflyer +++ b/ROMFS/px4fmu_common/init.d/30_io_camflyer @@ -55,7 +55,7 @@ else fi # -Start common fixedwing apps +# Start common fixedwing apps # sh /etc/init.d/rc.fixedwing diff --git a/ROMFS/px4fmu_common/init.d/31_io_phantom b/ROMFS/px4fmu_common/init.d/31_io_phantom index 14607e2df..63cd7f9b2 100644 --- a/ROMFS/px4fmu_common/init.d/31_io_phantom +++ b/ROMFS/px4fmu_common/init.d/31_io_phantom @@ -77,7 +77,7 @@ else fi # -Start common fixedwing apps +# Start common fixedwing apps # sh /etc/init.d/rc.fixedwing diff --git a/ROMFS/px4fmu_common/init.d/32_skywalker_x5 b/ROMFS/px4fmu_common/init.d/32_skywalker_x5 index 11071613c..1e752f13a 100644 --- a/ROMFS/px4fmu_common/init.d/32_skywalker_x5 +++ b/ROMFS/px4fmu_common/init.d/32_skywalker_x5 @@ -55,7 +55,7 @@ else fi # -Start common fixedwing apps +# Start common fixedwing apps # sh /etc/init.d/rc.fixedwing -- cgit v1.2.3 From c63995e91c188b476aa2608b42a366f68dced423 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Fri, 8 Nov 2013 14:22:27 +0100 Subject: Hotfix: Be more aggressive about SPI2 init on v1 boards --- src/drivers/boards/px4fmu-v1/px4fmu_init.c | 17 +++++++++-------- 1 file changed, 9 insertions(+), 8 deletions(-) diff --git a/src/drivers/boards/px4fmu-v1/px4fmu_init.c b/src/drivers/boards/px4fmu-v1/px4fmu_init.c index 964f5069c..4b12b75f9 100644 --- a/src/drivers/boards/px4fmu-v1/px4fmu_init.c +++ b/src/drivers/boards/px4fmu-v1/px4fmu_init.c @@ -222,14 +222,9 @@ __EXPORT int nsh_archinitialize(void) * If SPI2 is enabled in the defconfig, we loose some ADC pins as chip selects. * Keep the SPI2 init optional and conditionally initialize the ADC pins */ - spi2 = up_spiinitialize(2); - if (!spi2) { - message("[boot] Enabling IN12/13 instead of SPI2\n"); - /* no SPI2, use pins for ADC */ - stm32_configgpio(GPIO_ADC1_IN12); - stm32_configgpio(GPIO_ADC1_IN13); // jumperable to MPU6000 DRDY on some boards - } else { + #ifdef CONFIG_STM32_SPI2 + spi2 = up_spiinitialize(2); /* Default SPI2 to 1MHz and de-assert the known chip selects. */ SPI_SETFREQUENCY(spi2, 10000000); SPI_SETBITS(spi2, 8); @@ -238,7 +233,13 @@ __EXPORT int nsh_archinitialize(void) SPI_SELECT(spi2, PX4_SPIDEV_ACCEL_MAG, false); message("[boot] Initialized SPI port2 (ADC IN12/13 blocked)\n"); - } + #else + spi2 = NULL; + message("[boot] Enabling IN12/13 instead of SPI2\n"); + /* no SPI2, use pins for ADC */ + stm32_configgpio(GPIO_ADC1_IN12); + stm32_configgpio(GPIO_ADC1_IN13); // jumperable to MPU6000 DRDY on some boards + #endif /* Get the SPI port for the microSD slot */ -- cgit v1.2.3 From 64431a45bad777512a3d308bb7bc5e7815fe45f3 Mon Sep 17 00:00:00 2001 From: Julian Oes Date: Sat, 9 Nov 2013 11:59:23 +0100 Subject: missionlib: Added geo.h include, without this the _wrap_pi function returned garbage (e.g. for the yaw setpoint in auto) --- src/modules/mavlink/missionlib.c | 1 + 1 file changed, 1 insertion(+) diff --git a/src/modules/mavlink/missionlib.c b/src/modules/mavlink/missionlib.c index d37b18a19..fa23f996f 100644 --- a/src/modules/mavlink/missionlib.c +++ b/src/modules/mavlink/missionlib.c @@ -64,6 +64,7 @@ #include #include +#include "geo/geo.h" #include "waypoints.h" #include "orb_topics.h" #include "missionlib.h" -- cgit v1.2.3