2016-06-26 01:07:27 -03:00
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#include "Sub.h"
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2023-04-03 09:11:21 -03:00
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bool ModeManual::init(bool ignore_checks) {
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2016-06-26 01:07:27 -03:00
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// set target altitude to zero for reporting
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2023-04-03 09:11:21 -03:00
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position_control->set_pos_target_z_cm(0);
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2016-06-26 01:07:27 -03:00
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2017-10-30 17:07:58 -03:00
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// attitude hold inputs become thrust inputs in manual mode
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// set to neutral to prevent chaotic behavior (esp. roll/pitch)
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2023-04-03 09:11:21 -03:00
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sub.set_neutral_controls();
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2017-10-30 17:07:58 -03:00
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2016-06-26 01:07:27 -03:00
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return true;
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}
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// manual_run - runs the manual (passthrough) controller
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// should be called at 100hz or more
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2023-04-03 09:11:21 -03:00
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void ModeManual::run()
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2016-06-26 01:07:27 -03:00
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{
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// if not armed set throttle to zero and exit immediately
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2023-04-03 09:11:21 -03:00
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if (!sub.motors.armed()) {
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sub.motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE);
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attitude_control->set_throttle_out(0,true,g.throttle_filt);
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attitude_control->relax_attitude_controllers();
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2016-06-26 01:07:27 -03:00
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return;
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}
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2023-04-03 09:11:21 -03:00
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sub.motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
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2016-06-26 01:07:27 -03:00
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2023-04-03 09:11:21 -03:00
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sub.motors.set_roll(channel_roll->norm_input());
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sub.motors.set_pitch(channel_pitch->norm_input());
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sub.motors.set_yaw(channel_yaw->norm_input() * g.acro_yaw_p / ACRO_YAW_P);
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sub.motors.set_throttle(channel_throttle->norm_input());
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sub.motors.set_forward(channel_forward->norm_input());
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sub.motors.set_lateral(channel_lateral->norm_input());
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2016-06-26 01:07:27 -03:00
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}
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