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log tecs trim throttle
Signed-off-by: RomanBapst <bapstroman@gmail.com>
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@ -40,5 +40,6 @@ float32 pitch_integ
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float32 throttle_sp
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float32 pitch_sp_rad
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float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
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uint8 mode
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@ -537,6 +537,7 @@ FixedwingPositionControl::tecs_status_publish()
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t.throttle_sp = _tecs.get_throttle_setpoint();
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t.pitch_sp_rad = _tecs.get_pitch_setpoint();
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t.throttle_trim = _tecs.get_throttle_trim();
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t.timestamp = hrt_absolute_time();
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