mirror of https://github.com/ArduPilot/ardupilot
Copter: fixes for suggested changes
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@ -1631,6 +1631,7 @@ protected:
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private:
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void log_data() const;
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bool is_poscontrol_axis_type() const;
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enum class AxisType {
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NONE = 0, // none
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@ -80,17 +80,17 @@ bool ModeSystemId::init(bool ignore_checks)
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return false;
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}
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// if landed and the mode we're switching from does not have manual throttle and the throttle stick is too high
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if (motors->armed() && copter.ap.land_complete && (!copter.flightmode->has_manual_throttle() || copter.flightmode->mode_number() == Mode::Number::LOITER)) {
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// ensure we are flying
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if (!copter.motors->armed() || !copter.ap.auto_armed || copter.ap.land_complete) {
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gcs().send_text(MAV_SEVERITY_WARNING, "Aircraft must be flying");
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return false;
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}
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if ((AxisType)axis.get() != AxisType::DISTURB_POS_LAT && (AxisType)axis.get() != AxisType::DISTURB_POS_LONG
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&& (AxisType)axis.get() != AxisType::DISTURB_VEL_LAT && (AxisType)axis.get() != AxisType::DISTURB_VEL_LONG
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&& (AxisType)axis.get() != AxisType::INPUT_LOITER_LAT && (AxisType)axis.get() != AxisType::INPUT_LOITER_LONG) {
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if (!is_poscontrol_axis_type()) {
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// System ID is being done on the attitude control loops
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// Can only switch into System ID Axes 1-13 with a flight mode that has manual throttle
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if (!copter.flightmode->has_manual_throttle()) {
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gcs().send_text(MAV_SEVERITY_WARNING, "Axis requires manual throttle");
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return false;
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@ -104,6 +104,7 @@ bool ModeSystemId::init(bool ignore_checks)
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// System ID is being done on the position control loops
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// Can only switch into System ID Axes 14-19 from Loiter flight mode
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if (copter.flightmode->mode_number() != Mode::Number::LOITER) {
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gcs().send_text(MAV_SEVERITY_WARNING, "Axis requires switch from Loiter");
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return false;
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@ -162,9 +163,7 @@ void ModeSystemId::run()
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float target_climb_rate = 0.0f;
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Vector2f input_vel;
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if ((AxisType)axis.get() != AxisType::DISTURB_POS_LAT && (AxisType)axis.get() != AxisType::DISTURB_POS_LONG
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&& (AxisType)axis.get() != AxisType::DISTURB_VEL_LAT && (AxisType)axis.get() != AxisType::DISTURB_VEL_LONG
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&& (AxisType)axis.get() != AxisType::INPUT_LOITER_LAT && (AxisType)axis.get() != AxisType::INPUT_LOITER_LONG) {
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if (!is_poscontrol_axis_type()) {
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// apply simple mode transform to pilot inputs
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update_simple_mode();
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@ -343,9 +342,7 @@ void ModeSystemId::run()
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break;
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}
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if ((AxisType)axis.get() != AxisType::DISTURB_POS_LAT && (AxisType)axis.get() != AxisType::DISTURB_POS_LONG
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&& (AxisType)axis.get() != AxisType::DISTURB_VEL_LAT && (AxisType)axis.get() != AxisType::DISTURB_VEL_LONG
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&& (AxisType)axis.get() != AxisType::INPUT_LOITER_LAT && (AxisType)axis.get() != AxisType::INPUT_LOITER_LONG) {
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if (!is_poscontrol_axis_type()) {
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// call attitude controller
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attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(target_roll, target_pitch, target_yaw_rate);
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@ -410,9 +407,7 @@ void ModeSystemId::log_data() const
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copter.Log_Write_Attitude();
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copter.Log_Write_PIDS();
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if ((AxisType)axis.get() == AxisType::DISTURB_POS_LAT || (AxisType)axis.get() == AxisType::DISTURB_POS_LONG
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|| (AxisType)axis.get() == AxisType::DISTURB_VEL_LAT || (AxisType)axis.get() == AxisType::DISTURB_VEL_LONG
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|| (AxisType)axis.get() == AxisType::INPUT_LOITER_LAT || (AxisType)axis.get() == AxisType::INPUT_LOITER_LONG) {
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if (is_poscontrol_axis_type()) {
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pos_control->write_log();
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copter.logger.Write_PID(LOG_PIDN_MSG, pos_control->get_vel_xy_pid().get_pid_info_x());
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copter.logger.Write_PID(LOG_PIDE_MSG, pos_control->get_vel_xy_pid().get_pid_info_y());
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@ -420,4 +415,17 @@ void ModeSystemId::log_data() const
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}
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}
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bool ModeSystemId::is_poscontrol_axis_type() const
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{
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bool ret = false;
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if ((AxisType)axis.get() == AxisType::DISTURB_POS_LAT || (AxisType)axis.get() == AxisType::DISTURB_POS_LONG
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|| (AxisType)axis.get() == AxisType::DISTURB_VEL_LAT || (AxisType)axis.get() == AxisType::DISTURB_VEL_LONG
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|| (AxisType)axis.get() == AxisType::INPUT_LOITER_LAT || (AxisType)axis.get() == AxisType::INPUT_LOITER_LONG) {
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ret = true;
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}
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return ret;
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}
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#endif
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