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authorLorenz Meier <lm@inf.ethz.ch>2014-04-22 11:02:53 +0200
committerLorenz Meier <lm@inf.ethz.ch>2014-04-22 11:02:53 +0200
commita30411e9f2438018a08c0965261067940f88be10 (patch)
treefdf108c2d24e67c31ec9f323d15ccb59b6861722 /src/modules/fw_att_control
parent4585df1182083c39f2439bb7b88953dcc3575240 (diff)
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Fixed printing in attitude control
Diffstat (limited to 'src/modules/fw_att_control')
-rw-r--r--src/modules/fw_att_control/fw_att_control_main.cpp8
1 files changed, 4 insertions, 4 deletions
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 2f84dc963..5ded7aa76 100644
--- a/src/modules/fw_att_control/fw_att_control_main.cpp
+++ b/src/modules/fw_att_control/fw_att_control_main.cpp
@@ -771,7 +771,7 @@ FixedwingAttitudeControl::task_main()
_actuators.control[1] = (isfinite(pitch_u)) ? pitch_u + _parameters.trim_pitch : _parameters.trim_pitch;
if (!isfinite(pitch_u)) {
warnx("pitch_u %.4f, _yaw_ctrl.get_desired_rate() %.4f, airspeed %.4f, airspeed_scaling %.4f, roll_sp %.4f, pitch_sp %.4f, _roll_ctrl.get_desired_rate() %.4f, _pitch_ctrl.get_desired_rate() %.4f att_sp.roll_body %.4f",
- pitch_u, _yaw_ctrl.get_desired_rate(), airspeed, airspeed_scaling, roll_sp, pitch_sp, _roll_ctrl.get_desired_rate(), _pitch_ctrl.get_desired_rate(), _att_sp.roll_body);
+ (double)pitch_u, (double)_yaw_ctrl.get_desired_rate(), (double)airspeed, (double)airspeed_scaling, (double)roll_sp, (double)pitch_sp, (double)_roll_ctrl.get_desired_rate(), (double)_pitch_ctrl.get_desired_rate(), (double)_att_sp.roll_body);
}
float yaw_u = _yaw_ctrl.control_bodyrate(_att.roll, _att.pitch,
@@ -780,16 +780,16 @@ FixedwingAttitudeControl::task_main()
_parameters.airspeed_min, _parameters.airspeed_max, airspeed, airspeed_scaling, lock_integrator);
_actuators.control[2] = (isfinite(yaw_u)) ? yaw_u + _parameters.trim_yaw : _parameters.trim_yaw;
if (!isfinite(yaw_u)) {
- warnx("yaw_u %.4f", yaw_u);
+ warnx("yaw_u %.4f", (double)yaw_u);
}
/* throttle passed through */
_actuators.control[3] = (isfinite(throttle_sp)) ? throttle_sp : 0.0f;
if (!isfinite(throttle_sp)) {
- warnx("throttle_sp %.4f", throttle_sp);
+ warnx("throttle_sp %.4f", (double)throttle_sp);
}
} else {
- warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", roll_sp, pitch_sp);
+ warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", (double)roll_sp, (double)pitch_sp);
}
/*