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path: root/src/modules/commander/state_machine_helper.cpp
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Diffstat (limited to 'src/modules/commander/state_machine_helper.cpp')
-rw-r--r--src/modules/commander/state_machine_helper.cpp142
1 files changed, 85 insertions, 57 deletions
diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp
index 244513375..f8589d24b 100644
--- a/src/modules/commander/state_machine_helper.cpp
+++ b/src/modules/commander/state_machine_helper.cpp
@@ -52,6 +52,7 @@
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/differential_pressure.h>
+#include <uORB/topics/airspeed.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>
@@ -70,8 +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
@@ -89,7 +88,7 @@ static const bool arming_transitions[ARMING_STATE_MAX][ARMING_STATE_MAX] = {
};
// You can index into the array with an arming_state_t in order to get it's textual representation
-static const char *state_names[ARMING_STATE_MAX] = {
+static const char * const state_names[ARMING_STATE_MAX] = {
"ARMING_STATE_INIT",
"ARMING_STATE_STANDBY",
"ARMING_STATE_ARMED",
@@ -100,19 +99,20 @@ static const char *state_names[ARMING_STATE_MAX] = {
};
transition_result_t
-arming_state_transition(struct vehicle_status_s *status, /// current vehicle status
- const struct safety_s *safety, /// current safety settings
- arming_state_t new_arming_state, /// arming state requested
- struct actuator_armed_s *armed, /// current armed status
- const int mavlink_fd) /// mavlink fd for error reporting, 0 for none
+arming_state_transition(struct vehicle_status_s *status, ///< current vehicle status
+ const struct safety_s *safety, ///< current safety settings
+ arming_state_t new_arming_state, ///< arming state requested
+ struct actuator_armed_s *armed, ///< current armed status
+ bool fRunPreArmChecks, ///< true: run the pre-arm checks, false: no pre-arm checks, for unit testing
+ const int mavlink_fd) ///< mavlink fd for error reporting, 0 for none
{
// Double check that our static arrays are still valid
ASSERT(ARMING_STATE_INIT == 0);
ASSERT(ARMING_STATE_IN_AIR_RESTORE == ARMING_STATE_MAX - 1);
transition_result_t ret = TRANSITION_DENIED;
-
arming_state_t current_arming_state = status->arming_state;
+ bool feedback_provided = false;
/* only check transition if the new state is actually different from the current one */
if (new_arming_state == current_arming_state) {
@@ -126,7 +126,7 @@ arming_state_transition(struct vehicle_status_s *status, /// current
int prearm_ret = OK;
/* only perform the check if we have to */
- if (new_arming_state == ARMING_STATE_ARMED) {
+ if (fRunPreArmChecks && new_arming_state == ARMING_STATE_ARMED) {
prearm_ret = prearm_check(status, mavlink_fd);
}
@@ -157,13 +157,15 @@ arming_state_transition(struct vehicle_status_s *status, /// current
// Fail transition if pre-arm check fails
if (prearm_ret) {
+ /* the prearm check already prints the reject reason */
+ feedback_provided = true;
valid_transition = false;
// Fail transition if we need safety switch press
} else if (safety->safety_switch_available && !safety->safety_off) {
- mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Press safety switch!");
-
+ mavlink_log_critical(mavlink_fd, "NOT ARMING: Press safety switch first!");
+ feedback_provided = true;
valid_transition = false;
}
@@ -173,16 +175,18 @@ arming_state_transition(struct vehicle_status_s *status, /// current
// Fail transition if power is not good
if (!status->condition_power_input_valid) {
- mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Connect power module.");
+ mavlink_log_critical(mavlink_fd, "NOT ARMING: Connect power module.");
+ feedback_provided = true;
valid_transition = false;
}
// Fail transition if power levels on the avionics rail
// are measured but are insufficient
- if (status->condition_power_input_valid && (status->avionics_power_rail_voltage > 0.0f) &&
- (status->avionics_power_rail_voltage < 4.9f)) {
+ if (status->condition_power_input_valid && ((status->avionics_power_rail_voltage > 0.0f) &&
+ (status->avionics_power_rail_voltage < 4.9f))) {
- mavlink_log_critical(mavlink_fd, "#audio: NOT ARMING: Avionics power low: %6.2f V.", status->avionics_power_rail_voltage);
+ mavlink_log_critical(mavlink_fd, "NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage);
+ feedback_provided = true;
valid_transition = false;
}
}
@@ -201,6 +205,8 @@ arming_state_transition(struct vehicle_status_s *status, /// current
/* Sensors need to be initialized for STANDBY state */
if (new_arming_state == ARMING_STATE_STANDBY && !status->condition_system_sensors_initialized) {
+ mavlink_log_critical(mavlink_fd, "NOT ARMING: Sensors not operational.");
+ feedback_provided = true;
valid_transition = false;
}
@@ -217,11 +223,14 @@ arming_state_transition(struct vehicle_status_s *status, /// current
}
if (ret == TRANSITION_DENIED) {
- static const char *errMsg = "INVAL: %s - %s";
+ const char * str = "INVAL: %s - %s";
+ /* only print to console here by default as this is too technical to be useful during operation */
+ warnx(str, state_names[status->arming_state], state_names[new_arming_state]);
- mavlink_log_critical(mavlink_fd, errMsg, state_names[status->arming_state], state_names[new_arming_state]);
-
- warnx(errMsg, state_names[status->arming_state], state_names[new_arming_state]);
+ /* print to MAVLink if we didn't provide any feedback yet */
+ if (!feedback_provided) {
+ mavlink_log_critical(mavlink_fd, str, state_names[status->arming_state], state_names[new_arming_state]);
+ }
}
return ret;
@@ -271,7 +280,6 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta
}
break;
- case MAIN_STATE_AUTO_MISSION:
case MAIN_STATE_AUTO_LOITER:
/* need global position estimate */
if (status->condition_global_position_valid) {
@@ -279,6 +287,7 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta
}
break;
+ case MAIN_STATE_AUTO_MISSION:
case MAIN_STATE_AUTO_RTL:
/* need global position and home position */
if (status->condition_global_position_valid && status->condition_home_position_valid) {
@@ -286,6 +295,15 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta
}
break;
+ case MAIN_STATE_OFFBOARD:
+
+ /* need offboard signal */
+ if (!status->offboard_control_signal_lost) {
+ ret = TRANSITION_CHANGED;
+ }
+
+ break;
+
case MAIN_STATE_MAX:
default:
break;
@@ -584,6 +602,25 @@ bool set_nav_state(struct vehicle_status_s *status, const bool data_link_loss_en
}
break;
+ case MAIN_STATE_OFFBOARD:
+ /* require offboard control, otherwise stay where you are */
+ if (status->offboard_control_signal_lost && !status->rc_signal_lost) {
+ status->failsafe = true;
+
+ status->nav_state = NAVIGATION_STATE_POSCTL;
+ } else if (status->offboard_control_signal_lost && status->rc_signal_lost) {
+ status->failsafe = true;
+
+ if (status->condition_local_position_valid) {
+ status->nav_state = NAVIGATION_STATE_LAND;
+ } else if (status->condition_local_altitude_valid) {
+ status->nav_state = NAVIGATION_STATE_DESCEND;
+ } else {
+ status->nav_state = NAVIGATION_STATE_TERMINATION;
+ }
+ } else {
+ status->nav_state = NAVIGATION_STATE_OFFBOARD;
+ }
default:
break;
}
@@ -594,19 +631,21 @@ 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;
+ mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL SENSOR MISSING");
+ failed = true;
goto system_eval;
}
ret = ioctl(fd, ACCELIOCSELFTEST, 0);
if (ret != OK) {
- mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL CALIBRATION");
+ mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL CALIBRATION");
+ failed = true;
goto system_eval;
}
@@ -616,55 +655,44 @@ 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);
-
- if (accel_scale < 9.78f || accel_scale > 9.83f) {
- mavlink_log_info(mavlink_fd, "#audio: Accelerometer calibration recommended.");
- }
+ float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z);
- if (accel_scale > 30.0f /* m/s^2 */) {
- mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL RANGE");
+ if (accel_magnitude < 4.0f || accel_magnitude > 15.0f /* m/s^2 */) {
+ mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL RANGE, hold still");
/* this is frickin' fatal */
- ret = ERROR;
+ failed = true;
goto system_eval;
- } else {
- ret = OK;
}
} else {
- mavlink_log_critical(mavlink_fd, "#audio: FAIL: ACCEL READ");
+ mavlink_log_critical(mavlink_fd, "ARM FAIL: ACCEL READ");
/* this is frickin' fatal */
- ret = ERROR;
+ failed = true;
goto system_eval;
}
- if (!status->is_rotary_wing) {
- int fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
+ /* Perform airspeed check only if circuit breaker is not
+ * engaged and it's not a rotary wing */
+ if (!status->circuit_breaker_engaged_airspd_check && !status->is_rotary_wing) {
+ /* accel done, close it */
+ close(fd);
+ fd = orb_subscribe(ORB_ID(airspeed));
+
+ struct airspeed_s airspeed;
- if (fd < 0) {
- mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED SENSOR MISSING");
- ret = fd;
+ if ((ret = orb_copy(ORB_ID(airspeed), fd, &airspeed)) ||
+ (hrt_elapsed_time(&airspeed.timestamp) > (50 * 1000))) {
+ mavlink_log_critical(mavlink_fd, "ARM FAIL: AIRSPEED SENSOR MISSING");
+ failed = true;
goto system_eval;
}
- struct differential_pressure_s diff_pres;
-
- ret = read(fd, &diff_pres, sizeof(diff_pres));
-
- if (ret == sizeof(diff_pres)) {
- if (fabsf(diff_pres.differential_pressure_filtered_pa > 5.0f)) {
- mavlink_log_critical(mavlink_fd, "#audio: WARNING AIRSPEED CALIBRATION MISSING");
- // XXX do not make this fatal yet
- ret = OK;
- }
- } else {
- mavlink_log_critical(mavlink_fd, "#audio: FAIL: AIRSPEED READ");
- /* this is frickin' fatal */
- ret = ERROR;
- goto system_eval;
+ if (fabsf(airspeed.indicated_airspeed_m_s > 6.0f)) {
+ mavlink_log_critical(mavlink_fd, "AIRSPEED WARNING: WIND OR CALIBRATION MISSING");
+ // XXX do not make this fatal yet
}
}
system_eval:
close(fd);
- return ret;
+ return (failed);
}