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TECS: add EAS_sp to tecs_status.msg and rename other airspeeds to TAS

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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer
2021-01-19 10:18:29 +01:00
committed by Daniel Agar
parent 5e32e9be5a
commit 92f2043d8b
5 changed files with 13 additions and 10 deletions
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src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
+5 -4
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@@ -341,14 +341,15 @@ FixedwingPositionControl::tecs_status_publish()
t.altitude_sp = _tecs.hgt_setpoint_adj();
t.altitude_filtered = _tecs.vert_pos_state();
t.airspeed_sp = _tecs.TAS_setpoint_adj();
t.airspeed_filtered = _tecs.tas_state();
t.true_airspeed_sp = _tecs.TAS_setpoint_adj();
t.true_airspeed_filtered = _tecs.tas_state();
t.height_rate_setpoint = _tecs.hgt_rate_setpoint();
t.height_rate = _tecs.vert_vel_state();
t.airspeed_derivative_sp = _tecs.TAS_rate_setpoint();
t.airspeed_derivative = _tecs.speed_derivative();
t.equivalent_airspeed_sp = _tecs.get_EAS_setpoint();
t.true_airspeed_derivative_sp = _tecs.TAS_rate_setpoint();
t.true_airspeed_derivative = _tecs.speed_derivative();
t.total_energy_error = _tecs.STE_error();
t.total_energy_rate_error = _tecs.STE_rate_error();