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authorJohan Jansen <jnsn.johan@gmail.com>2015-02-12 14:43:23 +0100
committerJohan Jansen <jnsn.johan@gmail.com>2015-02-12 14:43:23 +0100
commit6af2a38f3621afb57ec33e4298e4399fb567e25a (patch)
tree287918edecf6e2239fd9bbe4c8b1704642c8858f
parenta8c298c77260b496b2b04ba9348ce351086c68c1 (diff)
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AttPosEKF: Moved class declaration to header file
-rw-r--r--src/modules/ekf_att_pos_estimator/AttitudePositionEstimatorEKF.h338
-rw-r--r--src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp294
-rw-r--r--src/modules/ekf_att_pos_estimator/estimator_22states.cpp4
3 files changed, 343 insertions, 293 deletions
diff --git a/src/modules/ekf_att_pos_estimator/AttitudePositionEstimatorEKF.h b/src/modules/ekf_att_pos_estimator/AttitudePositionEstimatorEKF.h
new file mode 100644
index 000000000..07db924b2
--- /dev/null
+++ b/src/modules/ekf_att_pos_estimator/AttitudePositionEstimatorEKF.h
@@ -0,0 +1,338 @@
+/****************************************************************************
+ *
+ * Copyright (c) 2013-2015 PX4 Development Team. All rights reserved.
+ *
+ * Redistribution and use in source and binary forms, with or without
+ * modification, are permitted provided that the following conditions
+ * are met:
+ *
+ * 1. Redistributions of source code must retain the above copyright
+ * notice, this list of conditions and the following disclaimer.
+ * 2. Redistributions in binary form must reproduce the above copyright
+ * notice, this list of conditions and the following disclaimer in
+ * the documentation and/or other materials provided with the
+ * distribution.
+ * 3. Neither the name PX4 nor the names of its contributors may be
+ * used to endorse or promote products derived from this software
+ * without specific prior written permission.
+ *
+ * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
+ * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
+ * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
+ * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
+ * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
+ * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
+ * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
+ * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
+ * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
+ * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
+ * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
+ * POSSIBILITY OF SUCH DAMAGE.
+ *
+ ****************************************************************************/
+
+/**
+ * @file AttitudePositionEstimatorEKF.h
+ * Implementation of the attitude and position estimator. This is a PX4 wrapper around
+ * the EKF IntertialNav filter of Paul Riseborough (@see estimator_22states.cpp)
+ *
+ * @author Paul Riseborough <p_riseborough@live.com.au>
+ * @author Lorenz Meier <lm@inf.ethz.ch>
+ * @author Johan Jansen <jnsn.johan@gmail.com>
+ */
+
+#pragma once
+
+#include <uORB/uORB.h>
+#include <uORB/topics/airspeed.h>
+#include <uORB/topics/vehicle_global_position.h>
+#include <uORB/topics/vehicle_local_position.h>
+#include <uORB/topics/vehicle_gps_position.h>
+#include <uORB/topics/vehicle_attitude.h>
+#include <uORB/topics/actuator_controls.h>
+#include <uORB/topics/vehicle_status.h>
+#include <uORB/topics/parameter_update.h>
+#include <uORB/topics/estimator_status.h>
+#include <uORB/topics/actuator_armed.h>
+#include <uORB/topics/home_position.h>
+#include <uORB/topics/wind_estimate.h>
+#include <uORB/topics/sensor_combined.h>
+
+#include <drivers/drv_hrt.h>
+#include <drivers/drv_gyro.h>
+#include <drivers/drv_accel.h>
+#include <drivers/drv_mag.h>
+#include <drivers/drv_baro.h>
+#include <drivers/drv_range_finder.h>
+
+#include <geo/geo.h>
+#include <systemlib/perf_counter.h>
+
+//Forward declaration
+class AttPosEKF;
+
+class AttitudePositionEstimatorEKF
+{
+public:
+ /**
+ * Constructor
+ */
+ AttitudePositionEstimatorEKF();
+
+ /* we do not want people ever copying this class */
+ AttitudePositionEstimatorEKF(const AttitudePositionEstimatorEKF& that) = delete;
+ AttitudePositionEstimatorEKF operator=(const AttitudePositionEstimatorEKF&) = delete;
+
+ /**
+ * Destructor, also kills the sensors task.
+ */
+ ~AttitudePositionEstimatorEKF();
+
+ /**
+ * Start the sensors task.
+ *
+ * @return OK on success.
+ */
+ int start();
+
+ /**
+ * Task status
+ *
+ * @return true if the mainloop is running
+ */
+ bool task_running() { return _task_running; }
+
+ /**
+ * Print the current status.
+ */
+ void print_status();
+
+ /**
+ * Trip the filter by feeding it NaN values.
+ */
+ int trip_nan();
+
+ /**
+ * Enable logging.
+ *
+ * @param enable Set to true to enable logging, false to disable
+ */
+ int enable_logging(bool enable);
+
+ /**
+ * Set debug level.
+ *
+ * @param debug Desired debug level - 0 to disable.
+ */
+ int set_debuglevel(unsigned debug) { _debug = debug; return 0; }
+
+private:
+ bool _task_should_exit; /**< if true, sensor task should exit */
+ bool _task_running; /**< if true, task is running in its mainloop */
+ int _estimator_task; /**< task handle for sensor task */
+
+ int _sensor_combined_sub;
+ int _distance_sub; /**< distance measurement */
+ int _airspeed_sub; /**< airspeed subscription */
+ int _baro_sub; /**< barometer subscription */
+ int _gps_sub; /**< GPS subscription */
+ int _vstatus_sub; /**< vehicle status subscription */
+ int _params_sub; /**< notification of parameter updates */
+ int _manual_control_sub; /**< notification of manual control updates */
+ int _mission_sub;
+ int _home_sub; /**< home position as defined by commander / user */
+
+ orb_advert_t _att_pub; /**< vehicle attitude */
+ orb_advert_t _global_pos_pub; /**< global position */
+ orb_advert_t _local_pos_pub; /**< position in local frame */
+ orb_advert_t _estimator_status_pub; /**< status of the estimator */
+ orb_advert_t _wind_pub; /**< wind estimate */
+
+ struct vehicle_attitude_s _att; /**< vehicle attitude */
+ struct gyro_report _gyro;
+ struct accel_report _accel;
+ struct mag_report _mag;
+ struct airspeed_s _airspeed; /**< airspeed */
+ struct baro_report _baro; /**< baro readings */
+ struct vehicle_status_s _vstatus; /**< vehicle status */
+ struct vehicle_global_position_s _global_pos; /**< global vehicle position */
+ struct vehicle_local_position_s _local_pos; /**< local vehicle position */
+ struct vehicle_gps_position_s _gps; /**< GPS position */
+ struct wind_estimate_s _wind; /**< wind estimate */
+ struct range_finder_report _distance; /**< distance estimate */
+
+ struct gyro_scale _gyro_offsets[3];
+ struct accel_scale _accel_offsets[3];
+ struct mag_scale _mag_offsets[3];
+
+ struct sensor_combined_s _sensor_combined;
+
+ struct map_projection_reference_s _pos_ref;
+
+ float _baro_ref; /**< barometer reference altitude */
+ float _baro_ref_offset; /**< offset between initial baro reference and GPS init baro altitude */
+ float _baro_gps_offset; /**< offset between baro altitude (at GPS init time) and GPS altitude */
+ hrt_abstime _last_debug_print = 0;
+
+ perf_counter_t _loop_perf; ///< loop performance counter
+ perf_counter_t _loop_intvl; ///< loop rate counter
+ perf_counter_t _perf_gyro; ///<local performance counter for gyro updates
+ perf_counter_t _perf_mag; ///<local performance counter for mag updates
+ perf_counter_t _perf_gps; ///<local performance counter for gps updates
+ perf_counter_t _perf_baro; ///<local performance counter for baro updates
+ perf_counter_t _perf_airspeed; ///<local performance counter for airspeed updates
+ perf_counter_t _perf_reset; ///<local performance counter for filter resets
+
+ float _gps_alt_filt;
+ float _baro_alt_filt;
+ float _covariancePredictionDt; ///< time lapsed since last covariance prediction
+ bool _gpsIsGood; ///< True if the current GPS fix is good enough for us to use
+ uint64_t _previousGPSTimestamp; ///< Timestamp of last good GPS fix we have received
+ bool _baro_init;
+ bool _gps_initialized;
+ hrt_abstime _filter_start_time;
+ hrt_abstime _last_sensor_timestamp;
+ hrt_abstime _last_run;
+ hrt_abstime _distance_last_valid;
+ bool _gyro_valid;
+ bool _accel_valid;
+ bool _mag_valid;
+ int _gyro_main; ///< index of the main gyroscope
+ int _accel_main; ///< index of the main accelerometer
+ int _mag_main; ///< index of the main magnetometer
+ bool _ekf_logging; ///< log EKF state
+ unsigned _debug; ///< debug level - default 0
+
+ bool _newDataGps;
+ bool _newHgtData;
+ bool _newAdsData;
+ bool _newDataMag;
+ bool _newRangeData;
+
+ int _mavlink_fd;
+
+ struct {
+ int32_t vel_delay_ms;
+ int32_t pos_delay_ms;
+ int32_t height_delay_ms;
+ int32_t mag_delay_ms;
+ int32_t tas_delay_ms;
+ float velne_noise;
+ float veld_noise;
+ float posne_noise;
+ float posd_noise;
+ float mag_noise;
+ float gyro_pnoise;
+ float acc_pnoise;
+ float gbias_pnoise;
+ float abias_pnoise;
+ float mage_pnoise;
+ float magb_pnoise;
+ float eas_noise;
+ float pos_stddev_threshold;
+ } _parameters; /**< local copies of interesting parameters */
+
+ struct {
+ param_t vel_delay_ms;
+ param_t pos_delay_ms;
+ param_t height_delay_ms;
+ param_t mag_delay_ms;
+ param_t tas_delay_ms;
+ param_t velne_noise;
+ param_t veld_noise;
+ param_t posne_noise;
+ param_t posd_noise;
+ param_t mag_noise;
+ param_t gyro_pnoise;
+ param_t acc_pnoise;
+ param_t gbias_pnoise;
+ param_t abias_pnoise;
+ param_t mage_pnoise;
+ param_t magb_pnoise;
+ param_t eas_noise;
+ param_t pos_stddev_threshold;
+ } _parameter_handles; /**< handles for interesting parameters */
+
+ AttPosEKF *_ekf;
+
+private:
+ /**
+ * Update our local parameter cache.
+ */
+ int parameters_update();
+
+ /**
+ * Update control outputs
+ *
+ */
+ void control_update();
+
+ /**
+ * Check for changes in vehicle status.
+ */
+ void vehicle_status_poll();
+
+ /**
+ * Shim for calling task_main from task_create.
+ */
+ static void task_main_trampoline(int argc, char *argv[]);
+
+ /**
+ * Main filter task.
+ */
+ void task_main();
+
+ /**
+ * Check filter sanity state
+ *
+ * @return zero if ok, non-zero for a filter error condition.
+ */
+ int check_filter_state();
+
+ /**
+ * @brief
+ * Publish the euler and quaternions for attitude estimation
+ **/
+ void publishAttitude();
+
+ /**
+ * @brief
+ * Publish local position relative to reference point where filter was initialized
+ **/
+ void publishLocalPosition();
+
+ /**
+ * @brief
+ * Publish global position estimation (WSG84 and AMSL).
+ * A global position estimate is only valid if we have a good GPS fix
+ **/
+ void publishGlobalPosition();
+
+ /**
+ * @brief
+ * Publish wind estimates for north and east in m/s
+ **/
+ void publishWindEstimate();
+
+ /**
+ * @brief
+ * Runs the sensor fusion step of the filter. The parameters determine which of the sensors
+ * are fused with each other
+ **/
+ void updateSensorFusion(const bool fuseGPS, const bool fuseMag, const bool fuseRangeSensor,
+ const bool fuseBaro, const bool fuseAirSpeed);
+
+ /**
+ * @brief
+ * Initialize first time good GPS fix so we can get a reference point to calculate local position from
+ * Should only be required to call once
+ **/
+ void initializeGPS();
+
+ /**
+ * @brief
+ * Polls all uORB subscriptions if any new sensor data has been publish and sets the appropriate
+ * flags to true (e.g newDataGps)
+ **/
+ void pollData();
+};
diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
index 8ec7c43a1..511492b5a 100644
--- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
+++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
@@ -40,6 +40,9 @@
* @author Johan Jansen <jnsn.johan@gmail.com>
*/
+#include "AttitudePositionEstimatorEKF.h"
+#include "estimator_22states.h"
+
#include <nuttx/config.h>
#include <stdio.h>
#include <stdlib.h>
@@ -52,39 +55,15 @@
#include <time.h>
#include <float.h>
-#include <drivers/drv_hrt.h>
-#include <drivers/drv_gyro.h>
-#include <drivers/drv_accel.h>
-#include <drivers/drv_mag.h>
-#include <drivers/drv_baro.h>
-#include <drivers/drv_range_finder.h>
-#include <uORB/topics/sensor_combined.h>
#include <arch/board/board.h>
-#include <uORB/uORB.h>
-#include <uORB/topics/airspeed.h>
-#include <uORB/topics/vehicle_global_position.h>
-#include <uORB/topics/vehicle_local_position.h>
-#include <uORB/topics/vehicle_gps_position.h>
-#include <uORB/topics/vehicle_attitude.h>
-#include <uORB/topics/actuator_controls.h>
-#include <uORB/topics/vehicle_status.h>
-#include <uORB/topics/parameter_update.h>
-#include <uORB/topics/estimator_status.h>
-#include <uORB/topics/actuator_armed.h>
-#include <uORB/topics/home_position.h>
-#include <uORB/topics/wind_estimate.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>
-#include <geo/geo.h>
-#include <systemlib/perf_counter.h>
#include <systemlib/systemlib.h>
#include <mathlib/mathlib.h>
#include <mathlib/math/filter/LowPassFilter2p.hpp>
#include <mavlink/mavlink_log.h>
#include <platforms/px4_defines.h>
-#include "estimator_22states.h"
-
static uint64_t IMUmsec = 0;
static uint64_t IMUusec = 0;
@@ -114,273 +93,6 @@ uint64_t getMicros()
return IMUusec;
}
-class AttitudePositionEstimatorEKF
-{
-public:
- /**
- * Constructor
- */
- AttitudePositionEstimatorEKF();
-
- /* we do not want people ever copying this class */
- AttitudePositionEstimatorEKF(const AttitudePositionEstimatorEKF& that) = delete;
- AttitudePositionEstimatorEKF operator=(const AttitudePositionEstimatorEKF&) = delete;
-
- /**
- * Destructor, also kills the sensors task.
- */
- ~AttitudePositionEstimatorEKF();
-
- /**
- * Start the sensors task.
- *
- * @return OK on success.
- */
- int start();
-
- /**
- * Task status
- *
- * @return true if the mainloop is running
- */
- bool task_running() { return _task_running; }
-
- /**
- * Print the current status.
- */
- void print_status();
-
- /**
- * Trip the filter by feeding it NaN values.
- */
- int trip_nan();
-
- /**
- * Enable logging.
- *
- * @param enable Set to true to enable logging, false to disable
- */
- int enable_logging(bool enable);
-
- /**
- * Set debug level.
- *
- * @param debug Desired debug level - 0 to disable.
- */
- int set_debuglevel(unsigned debug) { _debug = debug; return 0; }
-
-private:
- bool _task_should_exit; /**< if true, sensor task should exit */
- bool _task_running; /**< if true, task is running in its mainloop */
- int _estimator_task; /**< task handle for sensor task */
-
- int _sensor_combined_sub;
- int _distance_sub; /**< distance measurement */
- int _airspeed_sub; /**< airspeed subscription */
- int _baro_sub; /**< barometer subscription */
- int _gps_sub; /**< GPS subscription */
- int _vstatus_sub; /**< vehicle status subscription */
- int _params_sub; /**< notification of parameter updates */
- int _manual_control_sub; /**< notification of manual control updates */
- int _mission_sub;
- int _home_sub; /**< home position as defined by commander / user */
-
- orb_advert_t _att_pub; /**< vehicle attitude */
- orb_advert_t _global_pos_pub; /**< global position */
- orb_advert_t _local_pos_pub; /**< position in local frame */
- orb_advert_t _estimator_status_pub; /**< status of the estimator */
- orb_advert_t _wind_pub; /**< wind estimate */
-
- struct vehicle_attitude_s _att; /**< vehicle attitude */
- struct gyro_report _gyro;
- struct accel_report _accel;
- struct mag_report _mag;
- struct airspeed_s _airspeed; /**< airspeed */
- struct baro_report _baro; /**< baro readings */
- struct vehicle_status_s _vstatus; /**< vehicle status */
- struct vehicle_global_position_s _global_pos; /**< global vehicle position */
- struct vehicle_local_position_s _local_pos; /**< local vehicle position */
- struct vehicle_gps_position_s _gps; /**< GPS position */
- struct wind_estimate_s _wind; /**< wind estimate */
- struct range_finder_report _distance; /**< distance estimate */
-
- struct gyro_scale _gyro_offsets[3];
- struct accel_scale _accel_offsets[3];
- struct mag_scale _mag_offsets[3];
-
- struct sensor_combined_s _sensor_combined;
-
- struct map_projection_reference_s _pos_ref;
-
- float _baro_ref; /**< barometer reference altitude */
- float _baro_ref_offset; /**< offset between initial baro reference and GPS init baro altitude */
- float _baro_gps_offset; /**< offset between baro altitude (at GPS init time) and GPS altitude */
- hrt_abstime _last_debug_print = 0;
-
- perf_counter_t _loop_perf; ///< loop performance counter
- perf_counter_t _loop_intvl; ///< loop rate counter
- perf_counter_t _perf_gyro; ///<local performance counter for gyro updates
- perf_counter_t _perf_mag; ///<local performance counter for mag updates
- perf_counter_t _perf_gps; ///<local performance counter for gps updates
- perf_counter_t _perf_baro; ///<local performance counter for baro updates
- perf_counter_t _perf_airspeed; ///<local performance counter for airspeed updates
- perf_counter_t _perf_reset; ///<local performance counter for filter resets
-
- float _gps_alt_filt;
- float _baro_alt_filt;
- float _covariancePredictionDt; ///< time lapsed since last covariance prediction
- bool _gpsIsGood; ///< True if the current GPS fix is good enough for us to use
- uint64_t _previousGPSTimestamp; ///< Timestamp of last good GPS fix we have received
- bool _baro_init;
- bool _gps_initialized;
- hrt_abstime _filter_start_time;
- hrt_abstime _last_sensor_timestamp;
- hrt_abstime _last_run;
- hrt_abstime _distance_last_valid;
- bool _gyro_valid;
- bool _accel_valid;
- bool _mag_valid;
- int _gyro_main; ///< index of the main gyroscope
- int _accel_main; ///< index of the main accelerometer
- int _mag_main; ///< index of the main magnetometer
- bool _ekf_logging; ///< log EKF state
- unsigned _debug; ///< debug level - default 0
-
- bool _newDataGps;
- bool _newHgtData;
- bool _newAdsData;
- bool _newDataMag;
- bool _newRangeData;
-
- int _mavlink_fd;
-
- struct {
- int32_t vel_delay_ms;
- int32_t pos_delay_ms;
- int32_t height_delay_ms;
- int32_t mag_delay_ms;
- int32_t tas_delay_ms;
- float velne_noise;
- float veld_noise;
- float posne_noise;
- float posd_noise;
- float mag_noise;
- float gyro_pnoise;
- float acc_pnoise;
- float gbias_pnoise;
- float abias_pnoise;
- float mage_pnoise;
- float magb_pnoise;
- float eas_noise;
- float pos_stddev_threshold;
- } _parameters; /**< local copies of interesting parameters */
-
- struct {
- param_t vel_delay_ms;
- param_t pos_delay_ms;
- param_t height_delay_ms;
- param_t mag_delay_ms;
- param_t tas_delay_ms;
- param_t velne_noise;
- param_t veld_noise;
- param_t posne_noise;
- param_t posd_noise;
- param_t mag_noise;
- param_t gyro_pnoise;
- param_t acc_pnoise;
- param_t gbias_pnoise;
- param_t abias_pnoise;
- param_t mage_pnoise;
- param_t magb_pnoise;
- param_t eas_noise;
- param_t pos_stddev_threshold;
- } _parameter_handles; /**< handles for interesting parameters */
-
- AttPosEKF *_ekf;
-
-private:
- /**
- * Update our local parameter cache.
- */
- int parameters_update();
-
- /**
- * Update control outputs
- *
- */
- void control_update();
-
- /**
- * Check for changes in vehicle status.
- */
- void vehicle_status_poll();
-
- /**
- * Shim for calling task_main from task_create.
- */
- static void task_main_trampoline(int argc, char *argv[]);
-
- /**
- * Main filter task.
- */
- void task_main();
-
- /**
- * Check filter sanity state
- *
- * @return zero if ok, non-zero for a filter error condition.
- */
- int check_filter_state();
-
- /**
- * @brief
- * Publish the euler and quaternions for attitude estimation
- **/
- void publishAttitude();
-
- /**
- * @brief
- * Publish local position relative to reference point where filter was initialized
- **/
- void publishLocalPosition();
-
- /**
- * @brief
- * Publish global position estimation (WSG84 and AMSL).
- * A global position estimate is only valid if we have a good GPS fix
- **/
- void publishGlobalPosition();
-
- /**
- * @brief
- * Publish wind estimates for north and east in m/s
- **/
- void publishWindEstimate();
-
- /**
- * @brief
- * Runs the sensor fusion step of the filter. The parameters determine which of the sensors
- * are fused with each other
- **/
- void updateSensorFusion(const bool fuseGPS, const bool fuseMag, const bool fuseRangeSensor,
- const bool fuseBaro, const bool fuseAirSpeed);
-
- /**
- * @brief
- * Initialize first time good GPS fix so we can get a reference point to calculate local position from
- * Should only be required to call once
- **/
- void initializeGPS();
-
- /**
- * @brief
- * Polls all uORB subscriptions if any new sensor data has been publish and sets the appropriate
- * flags to true (e.g newDataGps)
- **/
- void pollData();
-
-};
-
namespace estimator
{
diff --git a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp
index e912e699e..f8c6510a2 100644
--- a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp
+++ b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp
@@ -1087,8 +1087,8 @@ void AttPosEKF::FuseVelposNED()
else horizRetryTime = gpsRetryTimeNoTAS;
// Form the observation vector
- for (uint8_t i=0; i<=2; i++) observation[i] = velNED[i];
- for (uint8_t i=3; i<=4; i++) observation[i] = posNE[i-3];
+ for (uint8_t i=0; i <=2; i++) observation[i] = velNED[i];
+ for (uint8_t i=3; i <=4; i++) observation[i] = posNE[i-3];
observation[5] = -(hgtMea);
// Estimate the GPS Velocity, GPS horiz position and height measurement variances.