Plane: use AP_AHRS_NavEKF when available

ArduPlane/ArduPlane.pde

@@ -273,7 +273,12 @@ AP_InertialSensor_L3G4200D ins;
   #error Unrecognised CONFIG_INS_TYPE setting.
 #endif // CONFIG_INS_TYPE
 
+// Inertial Navigation EKF
+#if AP_AHRS_NAVEKF_AVAILABLE
+AP_AHRS_NavEKF ahrs(ins, g_gps, barometer);
+#else
 AP_AHRS_DCM ahrs(ins, g_gps);
+#endif
 
 static AP_L1_Control L1_controller(ahrs);
 static AP_TECS TECS_controller(ahrs, aparm);
@@ -284,11 +289,6 @@ static AP_PitchController pitchController(ahrs, aparm);
 static AP_YawController   yawController(ahrs, aparm);
 static AP_SteerController steerController(ahrs);
 
-// Inertial Navigation EKF
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
-static NavEKF NavEKF(ahrs, barometer);
-#endif
-
 #if CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
 SITL sitl;
 #endif
@@ -807,14 +807,10 @@ static void ahrs_update()
 #endif
 
     ahrs.update();
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
-    NavEKF.UpdateFilter();
-#endif
 
     if (should_log(MASK_LOG_ATTITUDE_FAST)) {
         Log_Write_Attitude();
-        Log_Write_EKF1();
+        Log_Write_EKF();
-        Log_Write_EKF2();
     }
 
     if (should_log(MASK_LOG_IMU))
@@ -898,8 +894,7 @@ static void update_logging1(void)
 {
     if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_ATTITUDE_FAST)) {
         Log_Write_Attitude();
-        Log_Write_EKF1();
+        Log_Write_EKF();
-        Log_Write_EKF2();
     }
 
     if (should_log(MASK_LOG_ATTITUDE_MED) && !should_log(MASK_LOG_IMU))

ArduPlane/GCS_Mavlink.pde

@@ -530,11 +530,11 @@ static void NOINLINE send_simstate(mavlink_channel_t chan)
 // report NavEKF state
 static void NOINLINE send_ekf(mavlink_channel_t chan)
 {
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
+#if AP_AHRS_NAVEKF_AVAILABLE
     Vector3f euler;
     struct Location loc;
-    NavEKF.getEulerAngles(euler);
+    ahrs.get_NavEKF().getEulerAngles(euler);
-    NavEKF.getLLH(loc);
+    ahrs.get_NavEKF().getLLH(loc);
     mavlink_msg_ekf_send(chan,
                          euler.x,
                          euler.y,

ArduPlane/Log.pde

@@ -206,20 +206,37 @@ struct PACKED log_EKF1 {
     int8_t gyrZ;
 };
 
+struct PACKED log_EKF2 {
+    LOG_PACKET_HEADER;
+    uint32_t time_ms;
+    int8_t accX;
+    int8_t accY;
+    int8_t accZ;
+    int16_t windN;
+    int16_t windE;
+    int16_t magN;
+    int16_t magE;
+    int16_t magD;
+    int16_t magX;
+    int16_t magY;
+    int16_t magZ;
+};
+
+
 // Write first EKF packet
-static void Log_Write_EKF1(void)
+static void Log_Write_EKF(void)
 {
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
+#if AP_AHRS_NAVEKF_AVAILABLE
     Vector3f euler;
     Vector3f posNED;
     Vector3f velNED;
     Vector3f dAngBias;
     Vector3f dVelBias;
     Vector3f gyroBias;
-    NavEKF.getEulerAngles(euler);
+    ahrs.get_NavEKF().getEulerAngles(euler);
-    NavEKF.getVelNED(velNED);
+    ahrs.get_NavEKF().getVelNED(velNED);
-    NavEKF.getPosNED(posNED);
+    ahrs.get_NavEKF().getPosNED(posNED);
-    NavEKF.getGyroBias(gyroBias);
+    ahrs.get_NavEKF().getGyroBias(gyroBias);
     struct log_EKF1 pkt = {
         LOG_PACKET_HEADER_INIT(LOG_EKF1_MSG),
         time_ms : hal.scheduler->millis(),
@@ -237,39 +254,16 @@ static void Log_Write_EKF1(void)
         gyrZ    : (int8_t)(gyroBias.z)  // deg/min
     };
     DataFlash.WriteBlock(&pkt, sizeof(pkt));
-#endif
-}
 
-struct PACKED log_EKF2 {
-    LOG_PACKET_HEADER;
-    uint32_t time_ms;
-    int8_t accX;
-    int8_t accY;
-    int8_t accZ;
-    int16_t windN;
-    int16_t windE;
-    int16_t magN;
-    int16_t magE;
-    int16_t magD;
-    int16_t magX;
-    int16_t magY;
-    int16_t magZ;
-};
-
-// Write second EKF packet
-static void Log_Write_EKF2(void)
-{
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
-    Vector3f euler;
     Vector3f accelBias;
     Vector3f wind;
     Vector3f magNED;
     Vector3f magXYZ;
-    NavEKF.getAccelBias(accelBias);
+    ahrs.get_NavEKF().getAccelBias(accelBias);
-    NavEKF.getWind(wind);
+    ahrs.get_NavEKF().getWind(wind);
-    NavEKF.getMagNED(magNED);
+    ahrs.get_NavEKF().getMagNED(magNED);
-    NavEKF.getMagXYZ(magXYZ);
+    ahrs.get_NavEKF().getMagXYZ(magXYZ);
-    struct log_EKF2 pkt = {
+    struct log_EKF2 pkt2 = {
         LOG_PACKET_HEADER_INIT(LOG_EKF2_MSG),
         time_ms : hal.scheduler->millis(),
         accX    : (int8_t)(100*accelBias.x),
@@ -284,10 +278,11 @@ static void Log_Write_EKF2(void)
         magY    : (int16_t)(magXYZ.y),
         magZ    : (int16_t)(magXYZ.z)
     };
-    DataFlash.WriteBlock(&pkt, sizeof(pkt));
+    DataFlash.WriteBlock(&pkt2, sizeof(pkt2));
 #endif
 }
 
+
 struct PACKED log_Performance {
     LOG_PACKET_HEADER;
     uint32_t loop_time;
@@ -726,8 +721,7 @@ static void Log_Write_Nav_Tuning() {}
 static void Log_Write_TECS_Tuning() {}
 static void Log_Write_Performance() {}
 static void Log_Write_Attitude() {}
-static void Log_Write_EKF1() {}
+static void Log_Write_EKF() {}
-static void Log_Write_EKF2() {}
 static void Log_Write_Control_Tuning() {}
 static void Log_Write_Camera() {}
 static void Log_Write_Mode(uint8_t mode) {}

ArduPlane/commands.pde

@@ -239,11 +239,6 @@ static void init_home()
     // -------------
     guided_WP = home;
     guided_WP.alt += g.RTL_altitude_cm;
-
-    // startup EKF now we have home
-#if HAL_CPU_CLASS >= HAL_CPU_CLASS_150
-    NavEKF.InitialiseFilter();
-#endif
 }
 
 /*