Fix comments

src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp

@@ -1689,8 +1689,6 @@ FixedwingPositionControl::control_altitude(const hrt_abstime &now, const Vector2
 		_att_sp.thrust_body[0] = min(get_tecs_thrust(), throttle_max);
 	}
 
-	// decide when to use pitch setpoint from TECS because in some cases pitch
-	// setpoint is generated by other means
 	_att_sp.pitch_body = get_tecs_pitch();
 
 	_last_manual = !_control_mode.flag_control_position_enabled;
@@ -1811,8 +1809,6 @@ FixedwingPositionControl::control_position(const hrt_abstime &now, const Vector2
 		_att_sp.thrust_body[0] = min(get_tecs_thrust(), throttle_max);
 	}
 
-	// decide when to use pitch setpoint from TECS because in some cases pitch
-	// setpoint is generated by other means
 	_att_sp.pitch_body = get_tecs_pitch();
 
 	_last_manual = !_control_mode.flag_control_position_enabled;
@@ -1961,7 +1957,6 @@ FixedwingPositionControl::Run()
 		Vector2f ground_speed(_local_pos.vx, _local_pos.vy);
 
 		set_control_mode_current(_pos_sp_triplet.current.valid);
-		bool setpoint = true;
 
 		switch (_control_mode_current) {
 		case FW_POSCTRL_MODE_AUTO: {
@@ -1981,7 +1976,6 @@ FixedwingPositionControl::Run()
 			}
 
 		case FW_POSCTRL_MODE_OTHER: {
-				setpoint = false;
 				/* do not publish the setpoint */
 				// reset hold altitude
 				_hold_alt = _current_altitude;
@@ -1999,7 +1993,8 @@ FixedwingPositionControl::Run()
 
 		}
 
-		if (setpoint) {
+		if (_control_mode_current != FW_POSCTRL_MODE_OTHER) {
+
 			if (_control_mode.flag_control_manual_enabled) {
 				_att_sp.roll_body = constrain(_att_sp.roll_body, -radians(_param_fw_man_r_max.get()),
 							      radians(_param_fw_man_r_max.get()));