diff --git a/ArduPlane/Parameters.h b/ArduPlane/Parameters.h
index b8546e48b9..3bac4730bf 100644
--- a/ArduPlane/Parameters.h
+++ b/ArduPlane/Parameters.h
@@ -70,6 +70,7 @@ public:
         k_param_reset_switch_chan,
         k_param_manual_level,
 		k_param_land_pitch_cd,
+		k_param_ins,
 
 		// 110: Telemetry control
 		//
@@ -292,7 +293,6 @@ public:
     //
     AP_Int8     flybywire_airspeed_min;
     AP_Int8     flybywire_airspeed_max;
-    AP_Int16    FBWB_min_altitude;
 
     // Throttle
     //
@@ -338,23 +338,25 @@ public:
     AP_Int8		reset_switch_chan;
     AP_Int8		manual_level;
     AP_Int16    airspeed_cruise_cm;
+    AP_Int16    RTL_altitude;
 	AP_Int16	land_pitch_cd;
     AP_Int16    min_gndspeed;
     AP_Int16    pitch_trim;
-    AP_Int16    RTL_altitude;
+    AP_Int16    FBWB_min_altitude;
+
     AP_Int8		compass_enabled;
     AP_Int16    angle_of_attack;
     AP_Int8		battery_monitoring;	// 0=disabled, 3=voltage only, 4=voltage and current
+    AP_Int8		flap_1_percent;
+    AP_Int8		flap_1_speed;
+    AP_Int8		flap_2_percent;
+    AP_Int8		flap_2_speed;
     AP_Float	volt_div_ratio;
     AP_Float	curr_amp_per_volt;
     AP_Float	input_voltage;
 	AP_Int16	pack_capacity;		// Battery pack capacity less reserve
     AP_Int8		inverted_flight_ch; // 0=disabled, 1-8 is channel for inverted flight trigger
     AP_Int8		sonar_enabled;
-    AP_Int8		flap_1_percent;
-    AP_Int8		flap_1_speed;
-    AP_Int8		flap_2_percent;
-    AP_Int8		flap_2_speed;
 
 	// Camera
 #if CAMERA == ENABLED
@@ -458,19 +460,19 @@ public:
         reset_switch_chan		(0),
         manual_level			(MANUAL_LEVEL),
         airspeed_cruise_cm      (AIRSPEED_CRUISE_CM),
+        RTL_altitude            (ALT_HOLD_HOME_CM),
 		land_pitch_cd			(0),
         min_gndspeed            (MIN_GNDSPEED_CM),
         pitch_trim              (0),
-        RTL_altitude            (ALT_HOLD_HOME_CM),
         FBWB_min_altitude       (ALT_HOLD_FBW_CM),
         compass_enabled			(MAGNETOMETER),
+        battery_monitoring 		(DISABLED),
         flap_1_percent			(FLAP_1_PERCENT),
         flap_1_speed			(FLAP_1_SPEED),
         flap_2_percent			(FLAP_2_PERCENT),
         flap_2_speed			(FLAP_2_SPEED),
 
 
-        battery_monitoring 		(DISABLED),
         volt_div_ratio			(VOLT_DIV_RATIO),
         curr_amp_per_volt		(CURR_AMP_PER_VOLT),
         input_voltage			(INPUT_VOLTAGE),
diff --git a/ArduPlane/Parameters.pde b/ArduPlane/Parameters.pde
index cb41105475..7215df53a2 100644
--- a/ArduPlane/Parameters.pde
+++ b/ArduPlane/Parameters.pde
@@ -513,6 +513,10 @@ static const AP_Param::Info var_info[] PROGMEM = {
 	GOBJECT(gcs0,					"SR0_",     GCS_MAVLINK),
 	GOBJECT(gcs3,					"SR3_",     GCS_MAVLINK),
 
+	// @Group: INS_
+	// @Path: ../libraries/AP_InertialSensor/AP_InertialSensor_Oilpan.cpp
+	GOBJECT(ins,        			"INS_", AP_InertialSensor_Oilpan),
+
 	// @Group: IMU_
 	// @Path: ../libraries/AP_IMU/IMU.cpp
 	GOBJECT(imu,					"IMU_",     IMU),