Merge branch 'master' into seatbelt_multirotor

src/drivers/ets_airspeed/ets_airspeed.cpp

@@ -77,10 +77,10 @@
 #define PX4_I2C_BUS_DEFAULT		PX4_I2C_BUS_EXPANSION
 
 /* I2C bus address */
-#define I2C_ADDRESS		0x75	/* 7-bit address. 8-bit address is 0xEA */
+#define I2C_ADDRESS	0x75	/* 7-bit address. 8-bit address is 0xEA */
 
 /* Register address */
-#define READ_CMD		0x07		/* Read the data */
+#define READ_CMD	0x07	/* Read the data */
 
 /**
  * The Eagle Tree Airspeed V3 cannot provide accurate reading below speeds of 15km/h.
@@ -106,35 +106,35 @@ public:
 	ETSAirspeed(int bus, int address = I2C_ADDRESS);
 	virtual ~ETSAirspeed();
 
-	virtual int 		init();
+	virtual int	init();
 
-	virtual ssize_t		read(struct file *filp, char *buffer, size_t buflen);
+	virtual ssize_t	read(struct file *filp, char *buffer, size_t buflen);
-	virtual int			ioctl(struct file *filp, int cmd, unsigned long arg);
+	virtual int	ioctl(struct file *filp, int cmd, unsigned long arg);
 
 	/**
 	 * Diagnostics - print some basic information about the driver.
 	 */
-	void				print_info();
+	void		print_info();
 
 protected:
-	virtual int			probe();
+	virtual int	probe();
 
 private:
-	work_s						_work;
+	work_s			_work;
-	unsigned					_num_reports;
+	unsigned		_num_reports;
-	volatile unsigned			_next_report;
+	volatile unsigned	_next_report;
-	volatile unsigned			_oldest_report;
+	volatile unsigned	_oldest_report;
-	differential_pressure_s		*_reports;
+	differential_pressure_s	*_reports;
-	bool						_sensor_ok;
+	bool			_sensor_ok;
-	int							_measure_ticks;
+	int			_measure_ticks;
-	bool						_collect_phase;
+	bool			_collect_phase;
-	int 						_diff_pres_offset;
+	int			_diff_pres_offset;
 
-	orb_advert_t				_airspeed_pub;
+	orb_advert_t		_airspeed_pub;
 
-	perf_counter_t				_sample_perf;
+	perf_counter_t		_sample_perf;
-	perf_counter_t				_comms_errors;
+	perf_counter_t		_comms_errors;
-	perf_counter_t				_buffer_overflows;
+	perf_counter_t		_buffer_overflows;
 
 
 	/**
@@ -144,7 +144,7 @@ private:
 	* @param address	The I2C bus address to probe.
 	* @return		True if the device is present.
 	*/
-	int					probe_address(uint8_t address);
+	int	probe_address(uint8_t address);
 
 	/**
 	* Initialise the automatic measurement state machine and start it.
@@ -152,20 +152,20 @@ private:
 	* @note This function is called at open and error time.  It might make sense
 	*       to make it more aggressive about resetting the bus in case of errors.
 	*/
-	void				start();
+	void	start();
 
 	/**
 	* Stop the automatic measurement state machine.
 	*/
-	void				stop();
+	void	stop();
 
 	/**
 	* Perform a poll cycle; collect from the previous measurement
 	* and start a new one.
 	*/
-	void				cycle();
+	void	cycle();
-	int					measure();
+	int	measure();
-	int					collect();
+	int	collect();
 
 	/**
 	* Static trampoline from the workq context; because we don't have a
@@ -173,7 +173,7 @@ private:
 	*
 	* @param arg		Instance pointer for the driver that is polling.
 	*/
-	static void		cycle_trampoline(void *arg);
+	static void	cycle_trampoline(void *arg);
 
 
 };
@@ -230,6 +230,7 @@ ETSAirspeed::init()
 	/* allocate basic report buffers */
 	_num_reports = 2;
 	_reports = new struct differential_pressure_s[_num_reports];
+
 	for (unsigned i = 0; i < _num_reports; i++)
 		_reports[i].max_differential_pressure_pa = 0;
 
@@ -432,12 +433,12 @@ ETSAirspeed::measure()
 	uint8_t cmd = READ_CMD;
 	ret = transfer(&cmd, 1, nullptr, 0);
 
-	if (OK != ret)
+	if (OK != ret) {
-	{
 		perf_count(_comms_errors);
 		log("i2c::transfer returned %d", ret);
 		return ret;
 	}
+
 	ret = OK;
 
 	return ret;
@@ -466,11 +467,12 @@ ETSAirspeed::collect()
 
 	if (diff_pres_pa < _diff_pres_offset + MIN_ACCURATE_DIFF_PRES_PA) {
 		diff_pres_pa = 0;
+
 	} else {
 		diff_pres_pa -= _diff_pres_offset;
 	}
 
-    // XXX we may want to smooth out the readings to remove noise.
+	// XXX we may want to smooth out the readings to remove noise.
 
 	_reports[_next_report].timestamp = hrt_absolute_time();
 	_reports[_next_report].differential_pressure_pa = diff_pres_pa;
@@ -517,11 +519,13 @@ ETSAirspeed::start()
 		true,
 		true,
 		true,
-		SUBSYSTEM_TYPE_DIFFPRESSURE};
+		SUBSYSTEM_TYPE_DIFFPRESSURE
+	};
 	static orb_advert_t pub = -1;
 
 	if (pub > 0) {
 		orb_publish(ORB_ID(subsystem_info), pub, &info);
+
 	} else {
 		pub = orb_advertise(ORB_ID(subsystem_info), &info);
 	}
@@ -653,8 +657,7 @@ start(int i2c_bus)
 
 fail:
 
-	if (g_dev != nullptr) 
+	if (g_dev != nullptr) {
-	{
 		delete g_dev;
 		g_dev = nullptr;
 	}
@@ -668,15 +671,14 @@ fail:
 void
 stop()
 {
-	if (g_dev != nullptr)
+	if (g_dev != nullptr) {
-	{
 		delete g_dev;
 		g_dev = nullptr;
-	}
+
-	else
+	} else {
-	{
 		errx(1, "driver not running");
 	}
+
 	exit(0);
 }
 
@@ -776,7 +778,7 @@ info()
 static void
 ets_airspeed_usage()
 {
-	fprintf(stderr, "usage: ets_airspeed [options] command\n");
+	fprintf(stderr, "usage: ets_airspeed command [options]\n");
 	fprintf(stderr, "options:\n");
 	fprintf(stderr, "\t-b --bus i2cbus (%d)\n", PX4_I2C_BUS_DEFAULT);
 	fprintf(stderr, "command:\n");
@@ -789,6 +791,7 @@ ets_airspeed_main(int argc, char *argv[])
 	int i2c_bus = PX4_I2C_BUS_DEFAULT;
 
 	int i;
+
 	for (i = 1; i < argc; i++) {
 		if (strcmp(argv[i], "-b") == 0 || strcmp(argv[i], "--bus") == 0) {
 			if (argc > i + 1) {
@@ -803,11 +806,11 @@ ets_airspeed_main(int argc, char *argv[])
 	if (!strcmp(argv[1], "start"))
 		ets_airspeed::start(i2c_bus);
 
-	 /*
+	/*
-	  * Stop the driver
+	 * Stop the driver
-	  */
+	 */
-	 if (!strcmp(argv[1], "stop"))
+	if (!strcmp(argv[1], "stop"))
-		 ets_airspeed::stop();
+		ets_airspeed::stop();
 
 	/*
 	 * Test the driver/device.

src/drivers/hott_telemetry/messages.c

@@ -44,6 +44,7 @@
 #include <string.h>
 #include <systemlib/geo/geo.h>
 #include <unistd.h>
+#include <uORB/topics/airspeed.h>
 #include <uORB/topics/battery_status.h>
 #include <uORB/topics/home_position.h>
 #include <uORB/topics/sensor_combined.h>
@@ -56,6 +57,7 @@ static int battery_sub = -1;
 static int gps_sub = -1;
 static int home_sub = -1;
 static int sensor_sub = -1;
+static int airspeed_sub = -1;
 
 static bool home_position_set = false;
 static double home_lat = 0.0d;
@@ -68,6 +70,7 @@ messages_init(void)
 	gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
 	home_sub = orb_subscribe(ORB_ID(home_position));
 	sensor_sub = orb_subscribe(ORB_ID(sensor_combined));
+	airspeed_sub = orb_subscribe(ORB_ID(airspeed));
 }
 
 void 
@@ -100,6 +103,16 @@ build_eam_response(uint8_t *buffer, size_t *size)
 	msg.altitude_L = (uint8_t)alt & 0xff;
 	msg.altitude_H = (uint8_t)(alt >> 8) & 0xff;
 
+	/* get a local copy of the airspeed data */
+	struct airspeed_s airspeed;
+	memset(&airspeed, 0, sizeof(airspeed));
+	orb_copy(ORB_ID(airspeed), airspeed_sub, &airspeed);
+
+	uint16_t speed = (uint16_t)(airspeed.indicated_airspeed_m_s);
+	msg.speed_L = (uint8_t)speed & 0xff;
+	msg.speed_H = (uint8_t)(speed >> 8) & 0xff;
+    
+
 	msg.stop = STOP_BYTE;
 	memcpy(buffer, &msg, *size);
 }

src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp

@@ -126,7 +126,7 @@ int attitude_estimator_ekf_main(int argc, char *argv[])
 		attitude_estimator_ekf_task = task_spawn("attitude_estimator_ekf",
 					      SCHED_DEFAULT,
 					      SCHED_PRIORITY_MAX - 5,
-					      12400,
+					      14000,
 					      attitude_estimator_ekf_thread_main,
 					      (argv) ? (const char **)&argv[2] : (const char **)NULL);
 		exit(0);

src/modules/sdlog2/sdlog2.c

@@ -241,7 +241,7 @@ int sdlog2_main(int argc, char *argv[])
 		deamon_task = task_spawn("sdlog2",
 					 SCHED_DEFAULT,
 					 SCHED_PRIORITY_DEFAULT - 30,
-					 2048,
+					 3000,
 					 sdlog2_thread_main,
 					 (const char **)argv);
 		exit(0);
@@ -661,6 +661,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 		int vicon_pos_sub;
 		int flow_sub;
 		int rc_sub;
+		int airspeed_sub;
 	} subs;
 
 	/* log message buffer: header + body */
@@ -681,6 +682,7 @@ int sdlog2_thread_main(int argc, char *argv[])
 			struct log_RC_s log_RC;
 			struct log_OUT0_s log_OUT0;
 			struct log_ARSP_s log_ARSP;
+			struct log_AIRS_s log_AIRS;
 		} body;
 	} log_msg = {
 		LOG_PACKET_HEADER_INIT(0)
@@ -784,6 +786,12 @@ int sdlog2_thread_main(int argc, char *argv[])
 	fds[fdsc_count].events = POLLIN;
 	fdsc_count++;
 
+	/* --- AIRSPEED --- */
+	subs.airspeed_sub = orb_subscribe(ORB_ID(airspeed));
+	fds[fdsc_count].fd = subs.airspeed_sub;
+	fds[fdsc_count].events = POLLIN;
+	fdsc_count++;	
+
 	/* WARNING: If you get the error message below,
 	 * then the number of registered messages (fdsc)
 	 * differs from the number of messages in the above list.
@@ -1069,6 +1077,15 @@ int sdlog2_thread_main(int argc, char *argv[])
 				LOGBUFFER_WRITE_AND_COUNT(RC);
 			}
 
+			/* --- AIRSPEED --- */
+			if (fds[ifds++].revents & POLLIN) {
+				orb_copy(ORB_ID(airspeed), subs.airspeed_sub, &buf.airspeed);
+				log_msg.msg_type = LOG_AIRS_MSG;
+				log_msg.body.log_AIRS.indicated_airspeed = buf.airspeed.indicated_airspeed_m_s;
+				log_msg.body.log_AIRS.true_airspeed = buf.airspeed.true_airspeed_m_s;
+				LOGBUFFER_WRITE_AND_COUNT(AIRS);
+			}
+
 			/* signal the other thread new data, but not yet unlock */
 			if (logbuffer_count(&lb) > MIN_BYTES_TO_WRITE) {
 #ifdef SDLOG2_DEBUG

src/modules/sdlog2/sdlog2_messages.h

@@ -178,6 +178,13 @@ struct log_ARSP_s {
 	float pitch_rate_sp;
 	float yaw_rate_sp;
 };
+
+/* --- AIRS - AIRSPEED --- */
+#define LOG_AIRS_MSG 13
+struct log_AIRS_s {
+	float indicated_airspeed;
+	float true_airspeed;
+};
 #pragma pack(pop)
 
 /* construct list of all message formats */
@@ -195,7 +202,7 @@ static const struct log_format_s log_formats[] = {
 	LOG_FORMAT(STAT, "BBBBBfffB", "State,FlightMode,CtlMode,SASMode,Armed,BatV,BatC,BatRem,BatWarn"),
 	LOG_FORMAT(RC, "ffffffff", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7"),
 	LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"),
-	LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"),
+	LOG_FORMAT(AIRS, "ff", "IndSpeed,TrueSpeed"),
 };
 
 static const int log_formats_num = sizeof(log_formats) / sizeof(struct log_format_s);