diff --git a/ROMFS/px4fmu_common/init.d/3033_wingwing b/ROMFS/px4fmu_common/init.d/3033_wingwing index fff4b58df4..3cbbd555e3 100644 --- a/ROMFS/px4fmu_common/init.d/3033_wingwing +++ b/ROMFS/px4fmu_common/init.d/3033_wingwing @@ -32,7 +32,7 @@ then param set FW_THR_CRUISE 0.65 fi -set MIXER FMU_Q +set MIXER wingwing # Provide ESC a constant 1000 us pulse set PWM_OUTPUTS 4 set PWM_DISARMED 1000 diff --git a/ROMFS/px4fmu_common/mixers/wingwing.mix b/ROMFS/px4fmu_common/mixers/wingwing.mix new file mode 100644 index 0000000000..08333ba5cf --- /dev/null +++ b/ROMFS/px4fmu_common/mixers/wingwing.mix @@ -0,0 +1,51 @@ +Delta-wing mixer for PX4FMU +=========================== + +Designed for Wing Wing Z-84 + +This file defines mixers suitable for controlling a delta wing aircraft using +PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU +servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is +assumed to be unused. + +Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0 +(roll), 1 (pitch) and 3 (thrust). + +See the README for more information on the scaler format. + +Elevon mixers +------------- +Three scalers total (output, roll, pitch). + +On the assumption that the two elevon servos are physically reversed, the pitch +input is inverted between the two servos. + +The scaling factor for roll inputs is adjusted to implement differential travel +for the elevons. + +M: 2 +O: 10000 10000 0 -10000 10000 +S: 0 0 -6000 -6000 0 -10000 10000 +S: 0 1 6500 6500 0 -10000 10000 + +M: 2 +O: 10000 10000 0 -10000 10000 +S: 0 0 -6000 -6000 0 -10000 10000 +S: 0 1 -6500 -6500 0 -10000 10000 + +Output 2 +-------- +This mixer is empty. + +Z: + +Motor speed mixer +----------------- +Two scalers total (output, thrust). + +This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1) +range. Inputs below zero are treated as zero. + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 3 0 20000 -10000 -10000 10000 diff --git a/src/drivers/drv_px4flow.h b/src/drivers/drv_px4flow.h index bef02d54ef..76ec55c3e8 100644 --- a/src/drivers/drv_px4flow.h +++ b/src/drivers/drv_px4flow.h @@ -46,10 +46,18 @@ #define PX4FLOW_DEVICE_PATH "/dev/px4flow" +/** + * @addtogroup topics + * @{ + */ + /** * Optical flow in NED body frame in SI units. * * @see http://en.wikipedia.org/wiki/International_System_of_Units + * + * @warning If possible the usage of the raw flow and performing rotation-compensation + * using the autopilot angular rate estimate is recommended. */ struct px4flow_report { @@ -57,14 +65,18 @@ struct px4flow_report { int16_t flow_raw_x; /**< flow in pixels in X direction, not rotation-compensated */ int16_t flow_raw_y; /**< flow in pixels in Y direction, not rotation-compensated */ - float flow_comp_x_m; /**< speed over ground in meters, rotation-compensated */ - float flow_comp_y_m; /**< speed over ground in meters, rotation-compensated */ + float flow_comp_x_m; /**< speed over ground in meters per second, rotation-compensated */ + float flow_comp_y_m; /**< speed over ground in meters per second, rotation-compensated */ float ground_distance_m; /**< Altitude / distance to ground in meters */ uint8_t quality; /**< Quality of the measurement, 0: bad quality, 255: maximum quality */ uint8_t sensor_id; /**< id of the sensor emitting the flow value */ }; +/** + * @} + */ + /* * ObjDev tag for px4flow data. */ diff --git a/src/drivers/drv_range_finder.h b/src/drivers/drv_range_finder.h index e45939b371..0f8362f588 100644 --- a/src/drivers/drv_range_finder.h +++ b/src/drivers/drv_range_finder.h @@ -50,6 +50,11 @@ enum RANGE_FINDER_TYPE { RANGE_FINDER_TYPE_LASER = 0, }; +/** + * @addtogroup topics + * @{ + */ + /** * range finder report structure. Reads from the device must be in multiples of this * structure. @@ -64,6 +69,10 @@ struct range_finder_report { uint8_t valid; /**< 1 == within sensor range, 0 = outside sensor range */ }; +/** + * @} + */ + /* * ObjDev tag for raw range finder data. */ diff --git a/src/drivers/drv_rc_input.h b/src/drivers/drv_rc_input.h index 20763e2657..47fa8fa59a 100644 --- a/src/drivers/drv_rc_input.h +++ b/src/drivers/drv_rc_input.h @@ -67,6 +67,11 @@ */ #define RC_INPUT_RSSI_MAX 255 +/** + * @addtogroup topics + * @{ + */ + /** * Input signal type, value is a control position from zero to 100 * percent. @@ -141,6 +146,10 @@ struct rc_input_values { rc_input_t values[RC_INPUT_MAX_CHANNELS]; }; +/** + * @} + */ + /* * ObjDev tag for R/C inputs. */ diff --git a/src/drivers/gps/gps.cpp b/src/drivers/gps/gps.cpp index 401b65dd4f..34dd630866 100644 --- a/src/drivers/gps/gps.cpp +++ b/src/drivers/gps/gps.cpp @@ -127,7 +127,7 @@ private: /** * Try to configure the GPS, handle outgoing communication to the GPS */ - void config(); + void config(); /** * Trampoline to the worker task @@ -486,6 +486,8 @@ GPS::print_info() warnx("position lock: %dD, satellites: %d, last update: %8.4fms ago", (int)_report_gps_pos.fix_type, _report_gps_pos.satellites_used, (double)(hrt_absolute_time() - _report_gps_pos.timestamp_position) / 1000.0); warnx("lat: %d, lon: %d, alt: %d", _report_gps_pos.lat, _report_gps_pos.lon, _report_gps_pos.alt); + warnx("vel: %.2fm/s, %.2fm/s, %.2fm/s", (double)_report_gps_pos.vel_n_m_s, + (double)_report_gps_pos.vel_e_m_s, (double)_report_gps_pos.vel_d_m_s); warnx("eph: %.2fm, epv: %.2fm", (double)_report_gps_pos.eph, (double)_report_gps_pos.epv); warnx("rate position: \t%6.2f Hz", (double)_Helper->get_position_update_rate()); warnx("rate velocity: \t%6.2f Hz", (double)_Helper->get_velocity_update_rate()); diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index 2058cd92e2..18761665a2 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -286,15 +286,22 @@ int commander_main(int argc, char *argv[]) exit(0); } + /* commands needing the app to run below */ + if (!thread_running) { + warnx("\tcommander not started"); + exit(1); + } + if (!strcmp(argv[1], "status")) { - if (thread_running) { - warnx("\tcommander is running"); - print_status(); - - } else { - warnx("\tcommander not started"); - } + print_status(); + exit(0); + } + if (!strcmp(argv[1], "check")) { + int mavlink_fd_local = open(MAVLINK_LOG_DEVICE, 0); + int checkres = prearm_check(&status, mavlink_fd_local); + close(mavlink_fd_local); + warnx("FINAL RESULT: %s", (checkres == 0) ? "OK" : "FAILED"); exit(0); } @@ -303,7 +310,7 @@ int commander_main(int argc, char *argv[]) exit(0); } - if (!strcmp(argv[1], "2")) { + if (!strcmp(argv[1], "disarm")) { arm_disarm(false, mavlink_fd, "command line"); exit(0); } @@ -324,6 +331,7 @@ void usage(const char *reason) void print_status() { + warnx("type: %s", (status.is_rotary_wing) ? "ROTARY" : "PLANE"); warnx("usb powered: %s", (on_usb_power) ? "yes" : "no"); /* read all relevant states */ diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp index d894c9db09..e90c77af42 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -71,8 +71,6 @@ #endif static const int ERROR = -1; -static int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd); - // This array defines the arming state transitions. The rows are the new state, and the columns // are the current state. Using new state and current state you can index into the array which // will be true for a valid transition or false for a invalid transition. In some cases even @@ -623,12 +621,13 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) { int ret; + bool failed = false; int fd = open(ACCEL_DEVICE_PATH, O_RDONLY); if (fd < 0) { mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL SENSOR MISSING"); - ret = fd; + failed = true; goto system_eval; } @@ -636,6 +635,7 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) if (ret != OK) { mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL CALIBRATION"); + failed = true; goto system_eval; } @@ -645,29 +645,25 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) if (ret == sizeof(acc)) { /* evaluate values */ - float accel_scale = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); + float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); - if (accel_scale < 9.78f || accel_scale > 9.83f) { - mavlink_log_info(mavlink_fd, "#audio: Accelerometer calibration recommended."); - } - - if (accel_scale > 30.0f /* m/s^2 */) { + if (accel_magnitude < 4.0f || accel_magnitude > 15.0f /* m/s^2 */) { mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE"); + mavlink_log_info(mavlink_fd, "#audio: hold still while arming"); /* this is frickin' fatal */ - ret = ERROR; + failed = true; goto system_eval; - } else { - ret = OK; } } else { mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ"); /* this is frickin' fatal */ - ret = ERROR; + failed = true; goto system_eval; } if (!status->is_rotary_wing) { - + /* accel done, close it */ + close(fd); fd = orb_subscribe(ORB_ID(airspeed)); struct airspeed_s airspeed; @@ -675,17 +671,17 @@ int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd) if (ret = orb_copy(ORB_ID(airspeed), fd, &airspeed) || hrt_elapsed_time(&airspeed.timestamp) > 50 * 1000) { mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING"); + failed = true; goto system_eval; } - if (fabsf(airspeed.indicated_airspeed_m_s > 5.0f)) { - mavlink_log_critical(mavlink_fd, "#audio: WARNING AIRSPEED CALIBRATION MISSING"); + if (fabsf(airspeed.indicated_airspeed_m_s > 6.0f)) { + mavlink_log_critical(mavlink_fd, "#audio: WIND OR CALIBRATION MISSING"); // XXX do not make this fatal yet - ret = OK; } } system_eval: close(fd); - return ret; + return (failed); } diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h index 11072403ea..ddc5bf154c 100644 --- a/src/modules/commander/state_machine_helper.h +++ b/src/modules/commander/state_machine_helper.h @@ -67,4 +67,6 @@ transition_result_t hil_state_transition(hil_state_t new_state, int status_pub, bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_enabled, const bool mission_finished); +int prearm_check(const struct vehicle_status_s *status, const int mavlink_fd); + #endif /* STATE_MACHINE_HELPER_H_ */ diff --git a/src/modules/mavlink/mavlink_messages.cpp b/src/modules/mavlink/mavlink_messages.cpp index 667be87b70..c7ad605c5e 100644 --- a/src/modules/mavlink/mavlink_messages.cpp +++ b/src/modules/mavlink/mavlink_messages.cpp @@ -1051,10 +1051,16 @@ protected: uint32_t mavlink_custom_mode; get_mavlink_mode_state(&status, &pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode); + float out[8]; + + const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2; + + /* scale outputs depending on system type */ if (mavlink_system.type == MAV_TYPE_QUADROTOR || mavlink_system.type == MAV_TYPE_HEXAROTOR || mavlink_system.type == MAV_TYPE_OCTOROTOR) { - /* set number of valid outputs depending on vehicle type */ + /* multirotors: set number of rotor outputs depending on type */ + unsigned n; switch (mavlink_system.type) { @@ -1071,59 +1077,44 @@ protected: break; } - /* scale / assign outputs depending on system type */ - float out[8]; - for (unsigned i = 0; i < 8; i++) { - if (i < n) { - if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) { - /* scale fake PWM out 900..2100 us to 0..1 for normal multirotors */ + if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) { + if (i < n) { + /* scale PWM out 900..2100 us to 0..1 for rotors */ out[i] = (act.output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN); } else { - /* send 0 when disarmed */ - out[i] = 0.0f; + /* scale PWM out 900..2100 us to -1..1 for other channels */ + out[i] = (act.output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2); } } else { - out[i] = -1.0f; + /* send 0 when disarmed */ + out[i] = 0.0f; } } - mavlink_msg_hil_controls_send(_channel, - hrt_absolute_time(), - out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], - mavlink_base_mode, - 0); } else { - - /* fixed wing: scale all channels except throttle -1 .. 1 - * because we know that we set the mixers up this way - */ - - float out[8]; - - const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2; + /* fixed wing: scale throttle to 0..1 and other channels to -1..1 */ for (unsigned i = 0; i < 8; i++) { if (i != 3) { - /* scale fake PWM out 900..2100 us to -1..+1 for normal channels */ + /* scale PWM out 900..2100 us to -1..1 for normal channels */ out[i] = (act.output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2); } else { - - /* scale fake PWM out 900..2100 us to 0..1 for throttle */ + /* scale PWM out 900..2100 us to 0..1 for throttle */ out[i] = (act.output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN); } } - - mavlink_msg_hil_controls_send(_channel, - hrt_absolute_time(), - out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], - mavlink_base_mode, - 0); } + + mavlink_msg_hil_controls_send(_channel, + hrt_absolute_time(), + out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], + mavlink_base_mode, + 0); } } };