Copter: guided uses AP_Motors set_desired_spool_state
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@ -271,7 +271,7 @@ void Copter::guided_takeoff_run()
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attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw_smooth(0, 0, 0, get_smoothing_gain());
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attitude_control.set_throttle_out(0,false,g.throttle_filt);
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#else
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_SPIN_WHEN_ARMED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
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// multicopters do not stabilize roll/pitch/yaw when disarmed
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attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt);
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#endif
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@ -286,7 +286,7 @@ void Copter::guided_takeoff_run()
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}
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// set motors to full range
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
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// run waypoint controller
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wp_nav.update_wpnav();
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@ -309,7 +309,7 @@ void Copter::guided_pos_control_run()
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attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw_smooth(0, 0, 0, get_smoothing_gain());
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attitude_control.set_throttle_out(0,false,g.throttle_filt);
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#else
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_SPIN_WHEN_ARMED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
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// multicopters do not stabilize roll/pitch/yaw when disarmed
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attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt);
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#endif
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@ -327,7 +327,7 @@ void Copter::guided_pos_control_run()
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}
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// set motors to full range
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
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// run waypoint controller
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wp_nav.update_wpnav();
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@ -358,7 +358,7 @@ void Copter::guided_vel_control_run()
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attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw_smooth(0, 0, 0, get_smoothing_gain());
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attitude_control.set_throttle_out(0,false,g.throttle_filt);
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#else
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_SPIN_WHEN_ARMED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
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// multicopters do not stabilize roll/pitch/yaw when disarmed
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attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt);
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#endif
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@ -376,7 +376,7 @@ void Copter::guided_vel_control_run()
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}
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// set motors to full range
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
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// set velocity to zero if no updates received for 3 seconds
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uint32_t tnow = millis();
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@ -411,7 +411,7 @@ void Copter::guided_posvel_control_run()
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attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw_smooth(0, 0, 0, get_smoothing_gain());
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attitude_control.set_throttle_out(0,false,g.throttle_filt);
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#else
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_SPIN_WHEN_ARMED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
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// multicopters do not stabilize roll/pitch/yaw when disarmed
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attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt);
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#endif
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@ -430,7 +430,7 @@ void Copter::guided_posvel_control_run()
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}
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// set motors to full range
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
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// set velocity to zero if no updates received for 3 seconds
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uint32_t tnow = millis();
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@ -483,7 +483,7 @@ void Copter::guided_angle_control_run()
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attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw_smooth(0.0f, 0.0f, 0.0f, get_smoothing_gain());
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attitude_control.set_throttle_out(0.0f,false,g.throttle_filt);
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#else
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_SPIN_WHEN_ARMED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
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// multicopters do not stabilize roll/pitch/yaw when disarmed
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attitude_control.set_throttle_out_unstabilized(0.0f,true,g.throttle_filt);
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#endif
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@ -517,7 +517,7 @@ void Copter::guided_angle_control_run()
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}
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// set motors to full range
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motors.set_desired_spool_state(AP_MotorsMulticopter::DESIRED_THROTTLE_UNLIMITED);
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motors.set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
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// call attitude controller
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attitude_control.input_euler_angle_roll_pitch_yaw(roll_in, pitch_in, yaw_in, true);
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