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authorThomas Gubler <thomasgubler@gmail.com>2013-12-08 16:52:41 +0100
committerThomas Gubler <thomasgubler@gmail.com>2013-12-08 16:52:41 +0100
commit278e05e425f6aca75e2d6b43a17945b095176997 (patch)
treea34782d0ca8f528d589ec18b3f037c5a84242354 /src/modules/commander
parent4d846b480c9118090fe60a887fb1eb0824b38f56 (diff)
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added simple flight termination state machine which enbales parachute on request
Diffstat (limited to 'src/modules/commander')
-rw-r--r--src/modules/commander/commander.cpp19
-rw-r--r--src/modules/commander/state_machine_helper.cpp51
-rw-r--r--src/modules/commander/state_machine_helper.h4
3 files changed, 73 insertions, 1 deletions
diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp
index dfd4d2f73..40562a4e1 100644
--- a/src/modules/commander/commander.cpp
+++ b/src/modules/commander/commander.cpp
@@ -509,6 +509,21 @@ void handle_command(struct vehicle_status_s *status, const struct safety_s *safe
}
break;
+ /* Flight termination */
+ case VEHICLE_CMD_DO_SET_SERVO: { //xxx: needs its own mavlink command
+
+ if (armed->armed && cmd->param3 > 0.5) { //xxx: for safety only for now, param3 is unused by VEHICLE_CMD_DO_SET_SERVO
+ transition_result_t flighttermination_res = flighttermination_state_transition(status, FLIGHTTERMINATION_STATE_ON, control_mode);
+ result = VEHICLE_CMD_RESULT_ACCEPTED;
+
+ } else {
+ /* reject parachute depoyment not armed */
+ result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
+ }
+
+ }
+ break;
+
default:
break;
}
@@ -1199,6 +1214,7 @@ int commander_thread_main(int argc, char *argv[])
bool arming_state_changed = check_arming_state_changed();
bool main_state_changed = check_main_state_changed();
bool navigation_state_changed = check_navigation_state_changed();
+ bool flighttermination_state_changed = check_flighttermination_state_changed();
hrt_abstime t1 = hrt_absolute_time();
@@ -1725,7 +1741,8 @@ void *commander_low_prio_loop(void *arg)
/* ignore commands the high-prio loop handles */
if (cmd.command == VEHICLE_CMD_DO_SET_MODE ||
cmd.command == VEHICLE_CMD_COMPONENT_ARM_DISARM ||
- cmd.command == VEHICLE_CMD_NAV_TAKEOFF)
+ cmd.command == VEHICLE_CMD_NAV_TAKEOFF ||
+ cmd.command == VEHICLE_CMD_DO_SET_SERVO)
continue;
/* only handle low-priority commands here */
diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp
index a50af7daf..6c21dfab0 100644
--- a/src/modules/commander/state_machine_helper.cpp
+++ b/src/modules/commander/state_machine_helper.cpp
@@ -65,6 +65,7 @@ static const int ERROR = -1;
static bool arming_state_changed = true;
static bool main_state_changed = true;
static bool navigation_state_changed = true;
+static bool flighttermination_state_changed = true;
transition_result_t
arming_state_transition(struct vehicle_status_s *status, const struct safety_s *safety,
@@ -451,6 +452,18 @@ check_navigation_state_changed()
}
}
+bool
+check_flighttermination_state_changed()
+{
+ if (flighttermination_state_changed) {
+ flighttermination_state_changed = false;
+ return true;
+
+ } else {
+ return false;
+ }
+}
+
void
set_navigation_state_changed()
{
@@ -523,6 +536,44 @@ int hil_state_transition(hil_state_t new_state, int status_pub, struct vehicle_s
}
+/**
+* Transition from one flightermination state to another
+*/
+transition_result_t flighttermination_state_transition(struct vehicle_status_s *status, flighttermination_state_t new_flighttermination_state, struct vehicle_control_mode_s *control_mode)
+{
+ transition_result_t ret = TRANSITION_DENIED;
+
+ /* only check transition if the new state is actually different from the current one */
+ if (new_flighttermination_state == status->navigation_state) {
+ ret = TRANSITION_NOT_CHANGED;
+
+ } else {
+
+ switch (new_flighttermination_state) {
+ case FLIGHTTERMINATION_STATE_ON:
+ ret = TRANSITION_CHANGED;
+ status->flighttermination_state = FLIGHTTERMINATION_STATE_ON;
+ warnx("state machine helper: change to FLIGHTTERMINATION_STATE_ON");
+ break;
+ case FLIGHTTERMINATION_STATE_OFF:
+ ret = TRANSITION_CHANGED;
+ status->flighttermination_state = FLIGHTTERMINATION_STATE_OFF;
+ break;
+
+ default:
+ break;
+ }
+
+ if (ret == TRANSITION_CHANGED) {
+ flighttermination_state_changed = true;
+ control_mode->flag_control_flighttermination_enabled = status->flighttermination_state == FLIGHTTERMINATION_STATE_ON;
+ }
+ }
+
+ return ret;
+}
+
+
// /*
// * Wrapper functions (to be used in the commander), all functions assume lock on current_status
diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h
index 0bfdf36a8..e1ec9d4ad 100644
--- a/src/modules/commander/state_machine_helper.h
+++ b/src/modules/commander/state_machine_helper.h
@@ -70,8 +70,12 @@ bool check_main_state_changed();
transition_result_t navigation_state_transition(struct vehicle_status_s *status, navigation_state_t new_navigation_state, struct vehicle_control_mode_s *control_mode);
+transition_result_t flighttermination_state_transition(struct vehicle_status_s *status, flighttermination_state_t new_flighttermination_state, struct vehicle_control_mode_s *control_mode);
+
bool check_navigation_state_changed();
+bool check_flighttermination_state_changed();
+
void set_navigation_state_changed();
int hil_state_transition(hil_state_t new_state, int status_pub, struct vehicle_status_s *current_state, int control_mode_pub, struct vehicle_control_mode_s *current_control_mode, const int mavlink_fd);