From 00825aa3cf7a04de148f763b96ee69f977d2656f Mon Sep 17 00:00:00 2001 From: Thomas Gubler Date: Sun, 20 Oct 2013 17:36:49 +0200 Subject: fix small bug where roll instead of pitch was used --- src/modules/fw_att_control/fw_att_control_main.cpp | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) (limited to 'src/modules/fw_att_control/fw_att_control_main.cpp') diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index 277259330..c29cf4cc3 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -442,7 +442,7 @@ FixedwingAttitudeControl::vehicle_airspeed_poll() if (airspeed_updated) { orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed); - warnx("airspeed poll: ind: %.4f, true: %.4f", _airspeed.indicated_airspeed_m_s, _airspeed.true_airspeed_m_s); +// warnx("airspeed poll: ind: %.4f, true: %.4f", _airspeed.indicated_airspeed_m_s, _airspeed.true_airspeed_m_s); return true; } @@ -698,7 +698,7 @@ FixedwingAttitudeControl::task_main() _att.pitchspeed, _att.yawspeed, _yaw_ctrl.get_desired_rate(), _parameters.airspeed_min, _parameters.airspeed_max, airspeed, airspeed_scaling, lock_integrator); - _actuators.control[1] = (isfinite(roll_u)) ? roll_u : 0.0f; + _actuators.control[1] = (isfinite(pitch_u)) ? pitch_u : 0.0f; float yaw_u = _yaw_ctrl.control_bodyrate( _att.roll, _att.pitch, _att.pitchspeed, _att.yawspeed, -- cgit v1.2.3