mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-21 04:47:35 +08:00
Merged
This commit is contained in:
@@ -661,10 +661,10 @@ int KalmanNav::correctPos()
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Vector y(6);
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y(0) = _gps.vel_n_m_s - vN;
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y(1) = _gps.vel_e_m_s - vE;
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y(2) = double(_gps.lat) - lat * 1.0e7 * M_RAD_TO_DEG;
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y(3) = double(_gps.lon) - lon * 1.0e7 * M_RAD_TO_DEG;
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y(4) = double(_gps.alt) / 1.0e3 - alt;
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y(5) = double(_sensors.baro_alt_meter) - alt;
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y(2) = double(_gps.lat) - double(lat) * 1.0e7 * M_RAD_TO_DEG;
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y(3) = double(_gps.lon) - double(lon) * 1.0e7 * M_RAD_TO_DEG;
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y(4) = _gps.alt / 1.0e3f - alt;
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y(5) = _sensors.baro_alt_meter - alt;
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// compute correction
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// http://en.wikipedia.org/wiki/Extended_Kalman_filter
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@@ -698,7 +698,7 @@ int KalmanNav::correctPos()
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vD += xCorrect(VD);
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lat += double(xCorrect(LAT));
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lon += double(xCorrect(LON));
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alt += double(xCorrect(ALT));
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alt += xCorrect(ALT);
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// update state covariance
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// http://en.wikipedia.org/wiki/Extended_Kalman_filter
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@@ -710,7 +710,7 @@ int KalmanNav::correctPos()
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static int counter = 0;
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if (beta > _faultPos.get() && (counter % 10 == 0)) {
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warnx("fault in gps: beta = %8.4f", (double)beta);
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warnx("Y/N: vN: %8.4f, vE: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f",
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warnx("Y/N: vN: %8.4f, vE: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f, baro: %8.4f",
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double(y(0) / sqrtf(RPos(0, 0))),
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double(y(1) / sqrtf(RPos(1, 1))),
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double(y(2) / sqrtf(RPos(2, 2))),
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@@ -1389,6 +1389,7 @@ int commander_thread_main(int argc, char *argv[])
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uint64_t start_time = hrt_absolute_time();
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uint64_t failsave_ll_start_time = 0;
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enum VEHICLE_MANUAL_SAS_MODE manual_sas_mode;
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bool state_changed = true;
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bool param_init_forced = true;
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@@ -1828,8 +1829,9 @@ int commander_thread_main(int argc, char *argv[])
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} else if (sp_man.manual_sas_switch < -STICK_ON_OFF_LIMIT) {
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/* bottom stick position, set altitude hold */
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current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ALTITUDE;
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/* bottom stick position, set default */
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/* this MUST be mapped to extremal position to switch easy in case of emergency */
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current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS;
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} else if (sp_man.manual_sas_switch > STICK_ON_OFF_LIMIT) {
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@@ -1837,8 +1839,14 @@ int commander_thread_main(int argc, char *argv[])
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current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_SIMPLE;
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} else {
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/* center stick position, set default */
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current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS;
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/* center stick position, set altitude hold */
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current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ALTITUDE;
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}
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if (current_status.manual_sas_mode != manual_sas_mode) {
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/* publish SAS mode changes immediately */
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manual_sas_mode = current_status.manual_sas_mode;
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state_changed = true;
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}
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/*
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@@ -1849,8 +1857,10 @@ int commander_thread_main(int argc, char *argv[])
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(current_status.system_type == VEHICLE_TYPE_HEXAROTOR) ||
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(current_status.system_type == VEHICLE_TYPE_OCTOROTOR)
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) &&
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((sp_man.yaw < -STICK_ON_OFF_LIMIT)) &&
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(sp_man.throttle < STICK_THRUST_RANGE * 0.2f)) {
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current_status.flag_control_manual_enabled &&
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current_status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS &&
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sp_man.yaw < -STICK_ON_OFF_LIMIT &&
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sp_man.throttle < STICK_THRUST_RANGE * 0.1f) {
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if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) {
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update_state_machine_disarm(stat_pub, ¤t_status, mavlink_fd);
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stick_on_counter = 0;
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@@ -1862,7 +1872,10 @@ int commander_thread_main(int argc, char *argv[])
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}
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/* check if left stick is in lower right position --> arm */
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if (sp_man.yaw > STICK_ON_OFF_LIMIT && sp_man.throttle < STICK_THRUST_RANGE * 0.2f) {
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if (current_status.flag_control_manual_enabled &&
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current_status.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS &&
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sp_man.yaw > STICK_ON_OFF_LIMIT &&
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sp_man.throttle < STICK_THRUST_RANGE * 0.1f) {
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if (stick_on_counter > STICK_ON_OFF_COUNTER_LIMIT) {
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update_state_machine_arm(stat_pub, ¤t_status, mavlink_fd);
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stick_on_counter = 0;
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@@ -53,11 +53,7 @@
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#include <uORB/topics/vehicle_status.h>
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#include <poll.h>
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#include <drivers/drv_gpio.h>
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#define PX4IO_RELAY1 (1<<0)
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#define PX4IO_RELAY2 (1<<1)
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#define PX4IO_ACC1 (1<<2)
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#define PX4IO_ACC2 (1<<3)
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#include <modules/px4iofirmware/protocol.h>
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struct gpio_led_s {
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struct work_s work;
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@@ -186,10 +182,9 @@ void gpio_led_start(FAR void *arg)
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char *gpio_dev;
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if (priv->use_io) {
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gpio_dev = "/dev/px4io";
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gpio_dev = PX4IO_DEVICE_PATH;
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} else {
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gpio_dev = "/dev/px4fmu";
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gpio_dev = PX4FMU_DEVICE_PATH;
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}
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/* open GPIO device */
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@@ -203,6 +198,7 @@ void gpio_led_start(FAR void *arg)
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}
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/* configure GPIO pin */
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/* px4fmu only, px4io doesn't support GPIO_SET_OUTPUT and will ignore */
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ioctl(priv->gpio_fd, GPIO_SET_OUTPUT, priv->pin);
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/* subscribe to vehicle status topic */
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@@ -263,7 +259,6 @@ void gpio_led_cycle(FAR void *arg)
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if (led_state_new) {
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ioctl(priv->gpio_fd, GPIO_SET, priv->pin);
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} else {
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ioctl(priv->gpio_fd, GPIO_CLEAR, priv->pin);
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}
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@@ -373,7 +373,7 @@ void check_waypoints_reached(uint64_t now, const struct vehicle_global_position_
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dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, (float)global_pos->lat * 1e-7f, (float)global_pos->lon * 1e-7f, global_pos->alt);
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} else if (coordinate_frame == (int)MAV_FRAME_GLOBAL_RELATIVE_ALT) {
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dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, global_pos->lat, global_pos->lon, global_pos->relative_alt);
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dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, (float)global_pos->lat * 1e-7f, (float)global_pos->lon * 1e-7f, global_pos->relative_alt);
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} else if (coordinate_frame == (int)MAV_FRAME_LOCAL_ENU || coordinate_frame == (int)MAV_FRAME_LOCAL_NED) {
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dist = mavlink_wpm_distance_to_point_local(wpm->current_active_wp_id, local_pos->x, local_pos->y, local_pos->z);
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@@ -95,9 +95,16 @@ controls_tick() {
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*/
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perf_begin(c_gather_dsm);
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bool dsm_updated = dsm_input(r_raw_rc_values, &r_raw_rc_count);
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if (dsm_updated)
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uint16_t temp_count = r_raw_rc_count;
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bool dsm_updated = dsm_input(r_raw_rc_values, &temp_count);
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if (dsm_updated) {
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r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
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r_raw_rc_count = temp_count & 0x7fff;
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if (temp_count & 0x8000)
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r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM11;
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else
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r_status_flags &= ~PX4IO_P_STATUS_FLAGS_RC_DSM11;
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}
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perf_end(c_gather_dsm);
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perf_begin(c_gather_sbus);
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@@ -40,6 +40,7 @@
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*/
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#include <nuttx/config.h>
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#include <nuttx/arch.h>
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#include <fcntl.h>
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#include <unistd.h>
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@@ -101,6 +102,41 @@ dsm_init(const char *device)
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return dsm_fd;
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}
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void
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dsm_bind(uint16_t cmd, int pulses)
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{
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const uint32_t usart1RxAsOutp = GPIO_OUTPUT|GPIO_CNF_OUTPP|GPIO_MODE_50MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN10;
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if (dsm_fd < 0)
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return;
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switch (cmd) {
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case dsm_bind_power_down:
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// power down DSM satellite
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POWER_RELAY1(0);
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break;
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case dsm_bind_power_up:
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POWER_RELAY1(1);
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dsm_guess_format(true);
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break;
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case dsm_bind_set_rx_out:
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stm32_configgpio(usart1RxAsOutp);
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break;
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case dsm_bind_send_pulses:
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for (int i = 0; i < pulses; i++) {
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stm32_gpiowrite(usart1RxAsOutp, false);
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up_udelay(50);
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stm32_gpiowrite(usart1RxAsOutp, true);
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up_udelay(50);
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}
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break;
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case dsm_bind_reinit_uart:
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// Restore USART rx pin
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stm32_configgpio(GPIO_USART1_RX);
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break;
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}
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}
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bool
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dsm_input(uint16_t *values, uint16_t *num_values)
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{
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@@ -218,7 +254,7 @@ dsm_guess_format(bool reset)
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/*
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* Iterate the set of sensible sniffed channel sets and see whether
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* decoding in 10 or 11-bit mode has yielded anything we recognise.
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* decoding in 10 or 11-bit mode has yielded anything we recognize.
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*
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* XXX Note that due to what seem to be bugs in the DSM2 high-resolution
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* stream, we may want to sniff for longer in some cases when we think we
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@@ -349,6 +385,9 @@ dsm_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values)
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values[channel] = value;
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}
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if (channel_shift == 11)
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*num_values |= 0x8000;
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/*
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* XXX Note that we may be in failsafe here; we need to work out how to detect that.
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*/
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@@ -105,6 +105,7 @@
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#define PX4IO_P_STATUS_FLAGS_ARM_SYNC (1 << 9) /* the arming state between IO and FMU is in sync */
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#define PX4IO_P_STATUS_FLAGS_INIT_OK (1 << 10) /* initialisation of the IO completed without error */
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#define PX4IO_P_STATUS_FLAGS_FAILSAFE (1 << 11) /* failsafe is active */
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#define PX4IO_P_STATUS_FLAGS_RC_DSM11 (1 << 12) /* DSM input is 11 bit data */
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#define PX4IO_P_STATUS_ALARMS 3 /* alarm flags - alarms latch, write 1 to a bit to clear it */
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#define PX4IO_P_STATUS_ALARMS_VBATT_LOW (1 << 0) /* VBatt is very close to regulator dropout */
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@@ -156,7 +157,22 @@
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#define PX4IO_P_SETUP_PWM_DEFAULTRATE 3 /* 'low' PWM frame output rate in Hz */
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#define PX4IO_P_SETUP_PWM_ALTRATE 4 /* 'high' PWM frame output rate in Hz */
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#define PX4IO_P_SETUP_RELAYS 5 /* bitmask of relay/switch outputs, 0 = off, 1 = on */
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/* px4io relay bit definitions */
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#define PX4IO_RELAY1 (1<<0)
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#define PX4IO_RELAY2 (1<<1)
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#define PX4IO_ACC1 (1<<2)
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#define PX4IO_ACC2 (1<<3)
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#define PX4IO_P_SETUP_VBATT_SCALE 6 /* battery voltage correction factor (float) */
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#define PX4IO_P_SETUP_DSM 7 /* DSM bind state */
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enum { /* DSM bind states */
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dsm_bind_power_down = 0,
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dsm_bind_power_up,
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dsm_bind_set_rx_out,
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dsm_bind_send_pulses,
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dsm_bind_reinit_uart
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};
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#define PX4IO_P_SETUP_SET_DEBUG 9 /* debug level for IO board */
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/* autopilot control values, -10000..10000 */
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@@ -184,6 +184,7 @@ extern void controls_init(void);
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extern void controls_tick(void);
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extern int dsm_init(const char *device);
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extern bool dsm_input(uint16_t *values, uint16_t *num_values);
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extern void dsm_bind(uint16_t cmd, int pulses);
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extern int sbus_init(const char *device);
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extern bool sbus_input(uint16_t *values, uint16_t *num_values);
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@@ -349,10 +349,10 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
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case PX4IO_P_SETUP_RELAYS:
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value &= PX4IO_P_SETUP_RELAYS_VALID;
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r_setup_relays = value;
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POWER_RELAY1(value & (1 << 0) ? 1 : 0);
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POWER_RELAY2(value & (1 << 1) ? 1 : 0);
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POWER_ACC1(value & (1 << 2) ? 1 : 0);
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POWER_ACC2(value & (1 << 3) ? 1 : 0);
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POWER_RELAY1(value & PX4IO_RELAY1 ? 1 : 0);
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POWER_RELAY2(value & PX4IO_RELAY2 ? 1 : 0);
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POWER_ACC1(value & PX4IO_ACC1 ? 1 : 0);
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POWER_ACC2(value & PX4IO_ACC2 ? 1 : 0);
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break;
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case PX4IO_P_SETUP_SET_DEBUG:
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@@ -360,6 +360,10 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
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isr_debug(0, "set debug %u\n", (unsigned)r_page_setup[PX4IO_P_SETUP_SET_DEBUG]);
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break;
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case PX4IO_P_SETUP_DSM:
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dsm_bind(value & 0x0f, (value >> 4) & 7);
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break;
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default:
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return -1;
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}
|
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@@ -72,6 +72,7 @@
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#include <uORB/topics/vehicle_local_position.h>
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#include <uORB/topics/vehicle_local_position_setpoint.h>
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#include <uORB/topics/vehicle_global_position.h>
|
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#include <uORB/topics/vehicle_global_position_setpoint.h>
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#include <uORB/topics/vehicle_gps_position.h>
|
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#include <uORB/topics/vehicle_vicon_position.h>
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#include <uORB/topics/optical_flow.h>
|
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@@ -615,7 +616,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
|
||||
/* --- IMPORTANT: DEFINE NUMBER OF ORB STRUCTS TO WAIT FOR HERE --- */
|
||||
/* number of messages */
|
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const ssize_t fdsc = 18;
|
||||
const ssize_t fdsc = 19;
|
||||
/* Sanity check variable and index */
|
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ssize_t fdsc_count = 0;
|
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/* file descriptors to wait for */
|
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@@ -637,6 +638,7 @@ int sdlog2_thread_main(int argc, char *argv[])
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||||
struct vehicle_local_position_s local_pos;
|
||||
struct vehicle_local_position_setpoint_s local_pos_sp;
|
||||
struct vehicle_global_position_s global_pos;
|
||||
struct vehicle_global_position_setpoint_s global_pos_sp;
|
||||
struct vehicle_gps_position_s gps_pos;
|
||||
struct vehicle_vicon_position_s vicon_pos;
|
||||
struct optical_flow_s flow;
|
||||
@@ -660,6 +662,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
int local_pos_sub;
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int local_pos_sp_sub;
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||||
int global_pos_sub;
|
||||
int global_pos_sp_sub;
|
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int gps_pos_sub;
|
||||
int vicon_pos_sub;
|
||||
int flow_sub;
|
||||
@@ -689,6 +692,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
struct log_ARSP_s log_ARSP;
|
||||
struct log_FLOW_s log_FLOW;
|
||||
struct log_GPOS_s log_GPOS;
|
||||
struct log_GPSP_s log_GPSP;
|
||||
struct log_ESC_s log_ESC;
|
||||
} body;
|
||||
} log_msg = {
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||||
@@ -775,6 +779,12 @@ int sdlog2_thread_main(int argc, char *argv[])
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||||
fds[fdsc_count].events = POLLIN;
|
||||
fdsc_count++;
|
||||
|
||||
/* --- GLOBAL POSITION SETPOINT--- */
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||||
subs.global_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_global_position_setpoint));
|
||||
fds[fdsc_count].fd = subs.global_pos_sp_sub;
|
||||
fds[fdsc_count].events = POLLIN;
|
||||
fdsc_count++;
|
||||
|
||||
/* --- VICON POSITION --- */
|
||||
subs.vicon_pos_sub = orb_subscribe(ORB_ID(vehicle_vicon_position));
|
||||
fds[fdsc_count].fd = subs.vicon_pos_sub;
|
||||
@@ -1077,6 +1087,25 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
LOGBUFFER_WRITE_AND_COUNT(GPOS);
|
||||
}
|
||||
|
||||
/* --- GLOBAL POSITION SETPOINT --- */
|
||||
if (fds[ifds++].revents & POLLIN) {
|
||||
orb_copy(ORB_ID(vehicle_global_position_setpoint), subs.global_pos_sp_sub, &buf.global_pos_sp);
|
||||
log_msg.msg_type = LOG_GPSP_MSG;
|
||||
log_msg.body.log_GPSP.altitude_is_relative = buf.global_pos_sp.altitude_is_relative;
|
||||
log_msg.body.log_GPSP.lat = buf.global_pos_sp.lat;
|
||||
log_msg.body.log_GPSP.lon = buf.global_pos_sp.lon;
|
||||
log_msg.body.log_GPSP.altitude = buf.global_pos_sp.altitude;
|
||||
log_msg.body.log_GPSP.yaw = buf.global_pos_sp.yaw;
|
||||
log_msg.body.log_GPSP.loiter_radius = buf.global_pos_sp.loiter_radius;
|
||||
log_msg.body.log_GPSP.loiter_direction = buf.global_pos_sp.loiter_direction;
|
||||
log_msg.body.log_GPSP.nav_cmd = buf.global_pos_sp.nav_cmd;
|
||||
log_msg.body.log_GPSP.param1 = buf.global_pos_sp.param1;
|
||||
log_msg.body.log_GPSP.param2 = buf.global_pos_sp.param2;
|
||||
log_msg.body.log_GPSP.param3 = buf.global_pos_sp.param3;
|
||||
log_msg.body.log_GPSP.param4 = buf.global_pos_sp.param4;
|
||||
LOGBUFFER_WRITE_AND_COUNT(GPSP);
|
||||
}
|
||||
|
||||
/* --- VICON POSITION --- */
|
||||
if (fds[ifds++].revents & POLLIN) {
|
||||
orb_copy(ORB_ID(vehicle_vicon_position), subs.vicon_pos_sub, &buf.vicon_pos);
|
||||
|
||||
@@ -149,15 +149,15 @@ struct log_ATTC_s {
|
||||
/* --- STAT - VEHICLE STATE --- */
|
||||
#define LOG_STAT_MSG 10
|
||||
struct log_STAT_s {
|
||||
unsigned char state;
|
||||
unsigned char flight_mode;
|
||||
unsigned char manual_control_mode;
|
||||
unsigned char manual_sas_mode;
|
||||
unsigned char armed;
|
||||
uint8_t state;
|
||||
uint8_t flight_mode;
|
||||
uint8_t manual_control_mode;
|
||||
uint8_t manual_sas_mode;
|
||||
uint8_t armed;
|
||||
float battery_voltage;
|
||||
float battery_current;
|
||||
float battery_remaining;
|
||||
unsigned char battery_warning;
|
||||
uint8_t battery_warning;
|
||||
};
|
||||
|
||||
/* --- RC - RC INPUT CHANNELS --- */
|
||||
@@ -210,13 +210,29 @@ struct log_GPOS_s {
|
||||
float vel_d;
|
||||
};
|
||||
|
||||
/* --- GPSP - GLOBAL POSITION SETPOINT --- */
|
||||
#define LOG_GPSP_MSG 17
|
||||
struct log_GPSP_s {
|
||||
uint8_t altitude_is_relative;
|
||||
int32_t lat;
|
||||
int32_t lon;
|
||||
float altitude;
|
||||
float yaw;
|
||||
float loiter_radius;
|
||||
int8_t loiter_direction;
|
||||
uint8_t nav_cmd;
|
||||
float param1;
|
||||
float param2;
|
||||
float param3;
|
||||
float param4;
|
||||
};
|
||||
|
||||
/* --- ESC - ESC STATE --- */
|
||||
#define LOG_ESC_MSG 64
|
||||
#define LOG_ESC_MSG 18
|
||||
struct log_ESC_s {
|
||||
uint16_t counter;
|
||||
uint8_t esc_count;
|
||||
uint8_t esc_connectiontype;
|
||||
|
||||
uint8_t esc_num;
|
||||
uint16_t esc_address;
|
||||
uint16_t esc_version;
|
||||
@@ -227,6 +243,7 @@ struct log_ESC_s {
|
||||
float esc_setpoint;
|
||||
uint16_t esc_setpoint_raw;
|
||||
};
|
||||
|
||||
#pragma pack(pop)
|
||||
|
||||
/* construct list of all message formats */
|
||||
@@ -248,6 +265,7 @@ static const struct log_format_s log_formats[] = {
|
||||
LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"),
|
||||
LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"),
|
||||
LOG_FORMAT(GPOS, "LLffff", "Lat,Lon,Alt,VelN,VelE,VelD"),
|
||||
LOG_FORMAT(GPSP, "BLLfffbBffff", "AltRel,Lat,Lon,Alt,Yaw,LoiterR,LoiterDir,NavCmd,P1,P2,P3,P4"),
|
||||
LOG_FORMAT(ESC, "HBBBHHHHHHfH", "Counter,NumESC,Conn,No,Version,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"),
|
||||
};
|
||||
|
||||
|
||||
@@ -155,6 +155,7 @@ PARAM_DEFINE_FLOAT(RC14_REV, 1.0f);
|
||||
PARAM_DEFINE_FLOAT(RC14_DZ, 0.0f);
|
||||
|
||||
PARAM_DEFINE_INT32(RC_TYPE, 1); /** 1 = FUTABA, 2 = Spektrum, 3 = Graupner HoTT, 4 = Turnigy 9x */
|
||||
PARAM_DEFINE_INT32(RC_RL1_DSM_VCC, 0); /* Relay 1 controls DSM VCC */
|
||||
|
||||
/* default is conversion factor for the PX4IO / PX4IOAR board, the factor for PX4FMU standalone is different */
|
||||
PARAM_DEFINE_FLOAT(BAT_V_SCALING, (3.3f * 52.0f / 5.0f / 4095.0f));
|
||||
|
||||
@@ -232,7 +232,8 @@ private:
|
||||
|
||||
float battery_voltage_scaling;
|
||||
|
||||
int airspeed_offset;
|
||||
int rc_rl1_DSM_VCC_control;
|
||||
|
||||
} _parameters; /**< local copies of interesting parameters */
|
||||
|
||||
struct {
|
||||
@@ -282,7 +283,8 @@ private:
|
||||
|
||||
param_t battery_voltage_scaling;
|
||||
|
||||
param_t airspeed_offset;
|
||||
param_t rc_rl1_DSM_VCC_control;
|
||||
|
||||
} _parameter_handles; /**< handles for interesting parameters */
|
||||
|
||||
|
||||
@@ -519,6 +521,9 @@ Sensors::Sensors() :
|
||||
|
||||
_parameter_handles.battery_voltage_scaling = param_find("BAT_V_SCALING");
|
||||
|
||||
/* DSM VCC relay control */
|
||||
_parameter_handles.rc_rl1_DSM_VCC_control = param_find("RC_RL1_DSM_VCC");
|
||||
|
||||
/* fetch initial parameter values */
|
||||
parameters_update();
|
||||
}
|
||||
@@ -710,6 +715,11 @@ Sensors::parameters_update()
|
||||
warnx("Failed updating voltage scaling param");
|
||||
}
|
||||
|
||||
/* relay 1 DSM VCC control */
|
||||
if (param_get(_parameter_handles.rc_rl1_DSM_VCC_control, &(_parameters.rc_rl1_DSM_VCC_control)) != OK) {
|
||||
warnx("Failed updating relay 1 DSM VCC control");
|
||||
}
|
||||
|
||||
return OK;
|
||||
}
|
||||
|
||||
|
||||
@@ -63,7 +63,8 @@
|
||||
|
||||
enum ESC_VENDOR {
|
||||
ESC_VENDOR_GENERIC = 0, /**< generic ESC */
|
||||
ESC_VENDOR_MIKROKOPTER /**< Mikrokopter */
|
||||
ESC_VENDOR_MIKROKOPTER, /**< Mikrokopter */
|
||||
ESC_VENDOR_GRAUPNER_HOTT /**< Graupner HoTT ESC */
|
||||
};
|
||||
|
||||
enum ESC_CONNECTION_TYPE {
|
||||
|
||||
@@ -66,7 +66,7 @@ struct vehicle_global_position_setpoint_s
|
||||
float altitude; /**< altitude in meters */
|
||||
float yaw; /**< in radians NED -PI..+PI */
|
||||
float loiter_radius; /**< loiter radius in meters, 0 for a VTOL to hover */
|
||||
uint8_t loiter_direction; /**< 1: positive / clockwise, -1, negative. */
|
||||
int8_t loiter_direction; /**< 1: positive / clockwise, -1, negative. */
|
||||
enum NAV_CMD nav_cmd; /**< true if loitering is enabled */
|
||||
float param1;
|
||||
float param2;
|
||||
|
||||
Reference in New Issue
Block a user