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Diffstat (limited to 'src/modules/fw_pos_control_l1/mtecs/mTecs.h')
-rw-r--r--src/modules/fw_pos_control_l1/mtecs/mTecs.h6
1 files changed, 3 insertions, 3 deletions
diff --git a/src/modules/fw_pos_control_l1/mtecs/mTecs.h b/src/modules/fw_pos_control_l1/mtecs/mTecs.h
index 9ed233ba0..147c108f3 100644
--- a/src/modules/fw_pos_control_l1/mtecs/mTecs.h
+++ b/src/modules/fw_pos_control_l1/mtecs/mTecs.h
@@ -69,17 +69,17 @@ public:
/*
* Control in altitude setpoint and speed mode
*/
- void updateAltitudeSpeed(float flightPathAngle, float altitude, float altitudeSp, float airspeed, float airspeedSp, tecs_mode mode);
+ int updateAltitudeSpeed(float flightPathAngle, float altitude, float altitudeSp, float airspeed, float airspeedSp, tecs_mode mode);
/*
* Control in flightPathAngle setpoint (flollow a slope etc.) and speed mode
*/
- void updateFlightPathAngleSpeed(float flightPathAngle, float flightPathAngleSp, float airspeed, float airspeedSp, tecs_mode mode);
+ int updateFlightPathAngleSpeed(float flightPathAngle, float flightPathAngleSp, float airspeed, float airspeedSp, tecs_mode mode);
/*
* Control in flightPathAngle setpoint (flollow a slope etc.) and acceleration mode (base case)
*/
- void updateFlightPathAngleAcceleration(float flightPathAngle, float flightPathAngleSp, float airspeed, float accelerationLongitudinalSp, tecs_mode mode);
+ int updateFlightPathAngleAcceleration(float flightPathAngle, float flightPathAngleSp, float airspeed, float accelerationLongitudinalSp, tecs_mode mode);
/*
* Reset all integrators