diff --git a/src/main/flight/pid.h b/src/main/flight/pid.h
index 30ce2d5729..37a9c41110 100644
--- a/src/main/flight/pid.h
+++ b/src/main/flight/pid.h
@@ -214,8 +214,7 @@ bool pidAntiGravityEnabled(void);
 extern float axisError[XYZ_AXIS_COUNT];
 void applyItermRelax(const int axis, const float iterm,
     const float gyroRate, float *itermErrorRate, float *currentPidSetpoint);
-void applyAbsoluteControl(const int axis, const float gyroRate, const bool itermRelaxIsEnabled,
-    const float setpointLpf, const float setpointHpf, float *currentPidSetpoint, float *itermErrorRate);
+void applyAbsoluteControl(const int axis, const float gyroRate, float *currentPidSetpoint, float *itermErrorRate);
 void rotateItermAndAxisError();
 float pidLevel(int axis, const pidProfile_t *pidProfile,
     const rollAndPitchTrims_t *angleTrim, float currentPidSetpoint);
diff --git a/src/test/unit/pid_unittest.cc b/src/test/unit/pid_unittest.cc
index 0520a6798e..6c0dfccf78 100644
--- a/src/test/unit/pid_unittest.cc
+++ b/src/test/unit/pid_unittest.cc
@@ -589,8 +589,6 @@ TEST(pidControllerTest, testAbsoluteControl) {
     pidStabilisationState(PID_STABILISATION_ON);
 
     float gyroRate = 0;
-    float setpointLpf = 6;
-    float setpointHpf = 30;
 
     float itermErrorRate = 10;
     float currentPidSetpoint = 10;
@@ -600,16 +598,13 @@ TEST(pidControllerTest, testAbsoluteControl) {
     ASSERT_NEAR(10.8, itermErrorRate, calculateTolerance(10.8));
     ASSERT_NEAR(10.8, currentPidSetpoint, calculateTolerance(10.8));
 
-    itermRelaxIsEnabled = true;
-    applyAbsoluteControl(FD_PITCH, gyroRate, itermRelaxIsEnabled, setpointLpf, setpointHpf,
-        &currentPidSetpoint, &itermErrorRate);
+    applyAbsoluteControl(FD_PITCH, gyroRate, &currentPidSetpoint, &itermErrorRate);
     ASSERT_NEAR(10.8, itermErrorRate, calculateTolerance(10.8));
     ASSERT_NEAR(10.8, currentPidSetpoint, calculateTolerance(10.8));
 
     gyroRate = -53;
     axisError[FD_PITCH] = -60;
-    applyAbsoluteControl(FD_PITCH, gyroRate, itermRelaxIsEnabled, setpointLpf, setpointHpf,
-        &currentPidSetpoint, &itermErrorRate);
+    applyAbsoluteControl(FD_PITCH, gyroRate, &currentPidSetpoint, &itermErrorRate);
     ASSERT_NEAR(-79.2, itermErrorRate, calculateTolerance(-79.2));
     ASSERT_NEAR(-79.2, currentPidSetpoint, calculateTolerance(-79.2));
 }