forked from Archive/PX4-Autopilot
Back out testing changes that are a bit too much ahead of time for master
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@ -503,8 +503,8 @@ void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *c
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current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL;
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current_status->flag_control_manual_enabled = true; //XXX
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/* enable attitude control per default */
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current_status->flag_control_attitude_enabled = false;
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current_status->flag_control_rates_enabled = true;
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current_status->flag_control_attitude_enabled = true;
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current_status->flag_control_rates_enabled = false;
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if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
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if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
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@ -518,8 +518,8 @@ void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_
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int old_mode = current_status->flight_mode;
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current_status->flight_mode = VEHICLE_FLIGHT_MODE_STABILIZED;
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current_status->flag_control_manual_enabled = true; //XXX
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current_status->flag_control_attitude_enabled = false;
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current_status->flag_control_rates_enabled = true;
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current_status->flag_control_attitude_enabled = true;
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current_status->flag_control_rates_enabled = false;
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if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
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if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) {
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@ -533,8 +533,8 @@ void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *cur
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int old_mode = current_status->flight_mode;
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current_status->flight_mode = VEHICLE_FLIGHT_MODE_AUTO;
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current_status->flag_control_manual_enabled = true; //XXX
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current_status->flag_control_attitude_enabled = false;
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current_status->flag_control_rates_enabled = true;
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current_status->flag_control_attitude_enabled = true;
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current_status->flag_control_rates_enabled = false;
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if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
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if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_STABILIZED) {
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@ -224,13 +224,13 @@ mc_thread_main(int argc, char *argv[])
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/** STEP 3: Identify the controller setup to run and set up the inputs correctly */
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/* run attitude controller */
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// if (state.flag_control_attitude_enabled && !state.flag_control_rates_enabled) {
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// multirotor_control_attitude(&att_sp, &att, NULL, &actuators);
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// orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
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// } else if (state.flag_control_attitude_enabled && state.flag_control_rates_enabled) {
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// multirotor_control_attitude(&att_sp, &att, &rates_sp, NULL);
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// orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
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// }
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if (state.flag_control_attitude_enabled && !state.flag_control_rates_enabled) {
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multirotor_control_attitude(&att_sp, &att, NULL, &actuators);
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orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
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} else if (state.flag_control_attitude_enabled && state.flag_control_rates_enabled) {
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multirotor_control_attitude(&att_sp, &att, &rates_sp, NULL);
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orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
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}
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if (state.flag_control_rates_enabled) {
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