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fix small bug where roll instead of pitch was used
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@@ -442,7 +442,7 @@ FixedwingAttitudeControl::vehicle_airspeed_poll()
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if (airspeed_updated) {
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orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed);
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warnx("airspeed poll: ind: %.4f, true: %.4f", _airspeed.indicated_airspeed_m_s, _airspeed.true_airspeed_m_s);
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// warnx("airspeed poll: ind: %.4f, true: %.4f", _airspeed.indicated_airspeed_m_s, _airspeed.true_airspeed_m_s);
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return true;
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}
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@@ -698,7 +698,7 @@ FixedwingAttitudeControl::task_main()
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_att.pitchspeed, _att.yawspeed,
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_yaw_ctrl.get_desired_rate(),
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_parameters.airspeed_min, _parameters.airspeed_max, airspeed, airspeed_scaling, lock_integrator);
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_actuators.control[1] = (isfinite(roll_u)) ? roll_u : 0.0f;
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_actuators.control[1] = (isfinite(pitch_u)) ? pitch_u : 0.0f;
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float yaw_u = _yaw_ctrl.control_bodyrate( _att.roll, _att.pitch,
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_att.pitchspeed, _att.yawspeed,
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