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update msgs fields from camelCase to snake_case so rosidl_generate_interfaces() is able to generate code for ROS IDL files
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@@ -1956,21 +1956,21 @@ FixedwingPositionControl::tecs_update_pitch_throttle(float alt_sp, float airspee
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break;
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}
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t.altitudeSp = _tecs.hgt_setpoint_adj();
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t.altitude_sp = _tecs.hgt_setpoint_adj();
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t.altitude_filtered = _tecs.vert_pos_state();
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t.airspeedSp = _tecs.TAS_setpoint_adj();
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t.airspeed_filtered = _tecs.tas_state();
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t.airspeed_sp = _tecs.TAS_setpoint_adj();
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t.airspeed_filtered = _tecs.tas_state();
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t.flightPathAngleSp = _tecs.hgt_rate_setpoint();
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t.flightPathAngle = _tecs.vert_vel_state();
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t.flight_path_angle_sp = _tecs.hgt_rate_setpoint();
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t.flight_path_angle = _tecs.vert_vel_state();
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t.airspeedDerivativeSp = _tecs.TAS_rate_setpoint();
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t.airspeedDerivative = _tecs.speed_derivative();
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t.airspeed_derivative_sp = _tecs.TAS_rate_setpoint();
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t.airspeed_derivative = _tecs.speed_derivative();
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t.totalEnergyError = _tecs.STE_error();
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t.totalEnergyRateError = _tecs.STE_rate_error();
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t.energyDistributionError = _tecs.SEB_error();
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t.energyDistributionRateError = _tecs.SEB_rate_error();
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t.total_energy_error = _tecs.STE_error();
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t.total_energy_rate_error = _tecs.STE_rate_error();
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t.energy_distribution_error = _tecs.SEB_error();
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t.energy_distribution_rate_error = _tecs.SEB_rate_error();
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t.throttle_integ = _tecs.throttle_integ_state();
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t.pitch_integ = _tecs.pitch_integ_state();
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