mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-15 10:23:33 +08:00
Replaces poshold/althold with posctrl/altctrl
This commit is contained in:
@@ -434,13 +434,13 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
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/* MANUAL */
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main_res = main_state_transition(status, MAIN_STATE_MANUAL);
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} else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_ALTHOLD) {
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/* ALTHOLD */
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main_res = main_state_transition(status, MAIN_STATE_ALTHOLD);
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} else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_ALTCTRL) {
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/* ALTCTRL */
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main_res = main_state_transition(status, MAIN_STATE_ALTCTRL);
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} else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_POSHOLD) {
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/* POSHOLD */
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main_res = main_state_transition(status, MAIN_STATE_POSHOLD);
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} else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_POSCTRL) {
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/* POSCTRL */
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main_res = main_state_transition(status, MAIN_STATE_POSCTRL);
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} else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_AUTO) {
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/* AUTO */
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@@ -455,8 +455,8 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
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} else if (base_mode & MAV_MODE_FLAG_MANUAL_INPUT_ENABLED) {
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if (base_mode & MAV_MODE_FLAG_GUIDED_ENABLED) {
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/* POSHOLD */
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main_res = main_state_transition(status, MAIN_STATE_POSHOLD);
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/* POSCTRL */
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main_res = main_state_transition(status, MAIN_STATE_POSCTRL);
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} else if (base_mode & MAV_MODE_FLAG_STABILIZE_ENABLED) {
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/* MANUAL */
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@@ -628,8 +628,8 @@ int commander_thread_main(int argc, char *argv[])
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char *main_states_str[MAIN_STATE_MAX];
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main_states_str[0] = "MANUAL";
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main_states_str[1] = "ALTHOLD";
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main_states_str[2] = "POSHOLD";
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main_states_str[1] = "ALTCTRL";
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main_states_str[2] = "POSCTRL";
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main_states_str[3] = "AUTO";
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char *arming_states_str[ARMING_STATE_MAX];
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@@ -1299,8 +1299,8 @@ int commander_thread_main(int argc, char *argv[])
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}
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// TODO remove this hack
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/* flight termination in manual mode if assisted switch is on poshold position */
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if (!status.is_rotary_wing && parachute_enabled && armed.armed && status.main_state == MAIN_STATE_MANUAL && sp_man.poshold_switch == SWITCH_POS_ON) {
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/* flight termination in manual mode if assisted switch is on posctrl position */
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if (!status.is_rotary_wing && parachute_enabled && armed.armed && status.main_state == MAIN_STATE_MANUAL && sp_man.posctrl_switch == SWITCH_POS_ON) {
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if (TRANSITION_CHANGED == failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION)) {
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tune_positive(armed.armed);
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}
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@@ -1557,25 +1557,25 @@ set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoin
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break;
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case SWITCH_POS_MIDDLE: // ASSISTED
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if (sp_man->poshold_switch == SWITCH_POS_ON) {
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res = main_state_transition(status, MAIN_STATE_POSHOLD);
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if (sp_man->posctrl_switch == SWITCH_POS_ON) {
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res = main_state_transition(status, MAIN_STATE_POSCTRL);
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if (res != TRANSITION_DENIED) {
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break; // changed successfully or already in this state
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}
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// else fallback to ALTHOLD
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print_reject_mode(status, "POSHOLD");
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// else fallback to ALTCTRL
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print_reject_mode(status, "POSCTRL");
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}
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res = main_state_transition(status, MAIN_STATE_ALTHOLD);
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res = main_state_transition(status, MAIN_STATE_ALTCTRL);
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if (res != TRANSITION_DENIED) {
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break; // changed successfully or already in this mode
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}
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if (sp_man->poshold_switch != SWITCH_POS_ON) {
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print_reject_mode(status, "ALTHOLD");
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if (sp_man->posctrl_switch != SWITCH_POS_ON) {
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print_reject_mode(status, "ALTCTRL");
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}
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// else fallback to MANUAL
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@@ -1590,9 +1590,9 @@ set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoin
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break; // changed successfully or already in this state
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}
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// else fallback to ALTHOLD (POSHOLD likely will not work too)
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// else fallback to ALTCTRL (POSCTRL likely will not work too)
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print_reject_mode(status, "AUTO");
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res = main_state_transition(status, MAIN_STATE_ALTHOLD);
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res = main_state_transition(status, MAIN_STATE_ALTCTRL);
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if (res != TRANSITION_DENIED) {
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break; // changed successfully or already in this state
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@@ -1638,7 +1638,7 @@ set_control_mode()
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control_mode.flag_control_velocity_enabled = false;
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break;
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case MAIN_STATE_ALTHOLD:
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case MAIN_STATE_ALTCTRL:
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control_mode.flag_control_manual_enabled = true;
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control_mode.flag_control_auto_enabled = false;
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control_mode.flag_control_rates_enabled = true;
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@@ -1649,7 +1649,7 @@ set_control_mode()
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control_mode.flag_control_velocity_enabled = false;
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break;
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case MAIN_STATE_POSHOLD:
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case MAIN_STATE_POSCTRL:
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control_mode.flag_control_manual_enabled = true;
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control_mode.flag_control_auto_enabled = false;
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control_mode.flag_control_rates_enabled = true;
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@@ -317,34 +317,34 @@ bool StateMachineHelperTest::mainStateTransitionTest(void)
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TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state));
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ut_assert("new state: manual", MAIN_STATE_MANUAL == current_state.main_state);
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// MANUAL to ALTHOLD.
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// MANUAL to ALTCTRL.
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current_state.main_state = MAIN_STATE_MANUAL;
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current_state.condition_local_altitude_valid = true;
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new_main_state = MAIN_STATE_ALTHOLD;
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ut_assert("tranisition: manual to althold",
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new_main_state = MAIN_STATE_ALTCTRL;
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ut_assert("tranisition: manual to altctrl",
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TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state));
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ut_assert("new state: althold", MAIN_STATE_ALTHOLD == current_state.main_state);
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ut_assert("new state: altctrl", MAIN_STATE_ALTCTRL == current_state.main_state);
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// MANUAL to ALTHOLD, invalid local altitude.
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// MANUAL to ALTCTRL, invalid local altitude.
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current_state.main_state = MAIN_STATE_MANUAL;
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current_state.condition_local_altitude_valid = false;
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new_main_state = MAIN_STATE_ALTHOLD;
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new_main_state = MAIN_STATE_ALTCTRL;
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ut_assert("no transition: invalid local altitude",
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TRANSITION_DENIED == main_state_transition(¤t_state, new_main_state));
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ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state);
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// MANUAL to POSHOLD.
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// MANUAL to POSCTRL.
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current_state.main_state = MAIN_STATE_MANUAL;
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current_state.condition_local_position_valid = true;
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new_main_state = MAIN_STATE_POSHOLD;
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ut_assert("transition: manual to poshold",
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new_main_state = MAIN_STATE_POSCTRL;
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ut_assert("transition: manual to posctrl",
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TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state));
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ut_assert("current state: poshold", MAIN_STATE_POSHOLD == current_state.main_state);
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ut_assert("current state: posctrl", MAIN_STATE_POSCTRL == current_state.main_state);
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// MANUAL to POSHOLD, invalid local position.
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// MANUAL to POSCTRL, invalid local position.
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current_state.main_state = MAIN_STATE_MANUAL;
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current_state.condition_local_position_valid = false;
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new_main_state = MAIN_STATE_POSHOLD;
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new_main_state = MAIN_STATE_POSCTRL;
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ut_assert("no transition: invalid position",
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TRANSITION_DENIED == main_state_transition(¤t_state, new_main_state));
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ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state);
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@@ -12,8 +12,8 @@
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enum PX4_CUSTOM_MAIN_MODE {
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PX4_CUSTOM_MAIN_MODE_MANUAL = 1,
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PX4_CUSTOM_MAIN_MODE_ALTHOLD,
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PX4_CUSTOM_MAIN_MODE_POSHOLD,
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PX4_CUSTOM_MAIN_MODE_ALTCTRL,
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PX4_CUSTOM_MAIN_MODE_POSCTRL,
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PX4_CUSTOM_MAIN_MODE_AUTO,
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};
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@@ -215,7 +215,7 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta
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ret = TRANSITION_CHANGED;
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break;
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case MAIN_STATE_ALTHOLD:
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case MAIN_STATE_ALTCTRL:
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/* need at minimum altitude estimate */
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if (!status->is_rotary_wing ||
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@@ -226,7 +226,7 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta
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break;
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case MAIN_STATE_POSHOLD:
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case MAIN_STATE_POSCTRL:
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/* need at minimum local position estimate */
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if (status->condition_local_position_valid ||
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