Merge branch 'master' into vfr_fix

This commit is contained in:
Anton Babushkin
2014-11-08 15:49:23 +01:00
44 changed files with 1039 additions and 323 deletions
+1 -1
Submodule NuttX updated: 41fffa0df1...5ee4b2b2c2
@@ -27,3 +27,4 @@ fi
set MIXER FMU_quad_w
set PWM_OUTPUTS 1234
set PWM_MIN 1200
+7 -3
View File
@@ -178,9 +178,9 @@ class uploader(object):
MAVLINK_REBOOT_ID1 = bytearray(b'\xfe\x21\x72\xff\x00\x4c\x00\x00\x80\x3f\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\xf6\x00\x01\x00\x00\x48\xf0')
MAVLINK_REBOOT_ID0 = bytearray(b'\xfe\x21\x45\xff\x00\x4c\x00\x00\x80\x3f\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\xf6\x00\x00\x00\x00\xd7\xac')
def __init__(self, portname, baudrate, interCharTimeout=0.001, timeout=0.5):
def __init__(self, portname, baudrate):
# open the port, keep the default timeout short so we can poll quickly
self.port = serial.Serial(portname, baudrate)
self.port = serial.Serial(portname, baudrate, timeout=0.5)
self.otp = b''
self.sn = b''
@@ -195,7 +195,7 @@ class uploader(object):
def __recv(self, count=1):
c = self.port.read(count)
if len(c) < 1:
raise RuntimeError("timeout waiting for data (%u bytes)", count)
raise RuntimeError("timeout waiting for data (%u bytes)" % count)
# print("recv " + binascii.hexlify(c))
return c
@@ -459,6 +459,7 @@ if os.path.exists("/usr/sbin/ModemManager"):
# Load the firmware file
fw = firmware(args.firmware)
print("Loaded firmware for %x,%x, waiting for the bootloader..." % (fw.property('board_id'), fw.property('board_revision')))
print("If the board does not respond within 1-2 seconds, unplug and re-plug the USB connector.")
# Spin waiting for a device to show up
while True:
@@ -508,9 +509,12 @@ while True:
except Exception:
# most probably a timeout talking to the port, no bootloader, try to reboot the board
print("attempting reboot on %s..." % port)
print("if the board does not respond, unplug and re-plug the USB connector.")
up.send_reboot()
# wait for the reboot, without we might run into Serial I/O Error 5
time.sleep(0.5)
# always close the port
up.close()
continue
try:
Regular → Executable
+2 -2
View File
@@ -154,8 +154,8 @@ class SDLog2Parser:
first_data_msg = False
self.__parseMsg(msg_descr)
bytes_read += self.__ptr
if not self.__debug_out and self.__time_msg != None and self.__csv_updated:
self.__printCSVRow()
if not self.__debug_out and self.__time_msg != None and self.__csv_updated:
self.__printCSVRow()
f.close()
def __bytesLeft(self):
+55
View File
@@ -0,0 +1,55 @@
import serial, time
port = serial.Serial('/dev/ttyACM0', baudrate=57600, timeout=2)
data = '01234567890123456789012345678901234567890123456789'
#data = 'hellohello'
outLine = 'echo %s\n' % data
port.write('\n\n\n')
port.write('free\n')
line = port.readline(80)
while line != '':
print(line)
line = port.readline(80)
i = 0
bytesOut = 0
bytesIn = 0
startTime = time.time()
lastPrint = startTime
while True:
bytesOut += port.write(outLine)
line = port.readline(80)
bytesIn += len(line)
# check command line echo
if (data not in line):
print('command error %d: %s' % (i,line))
#break
# read echo output
line = port.readline(80)
if (data not in line):
print('echo output error %d: %s' % (i,line))
#break
bytesIn += len(line)
#print('%d: %s' % (i,line))
#print('%d: bytesOut: %d, bytesIn: %d' % (i, bytesOut, bytesIn))
elapsedT = time.time() - lastPrint
if (time.time() - lastPrint >= 5):
outRate = bytesOut / elapsedT
inRate = bytesIn / elapsedT
usbRate = (bytesOut + bytesIn) / elapsedT
lastPrint = time.time()
print('elapsed time: %f' % (time.time() - startTime))
print('data rates (bytes/sec): out: %f, in: %f, total: %f' % (outRate, inRate, usbRate))
bytesOut = 0
bytesIn = 0
i += 1
#if (i > 2): break
@@ -77,6 +77,7 @@
#define GPIO_LED1 (GPIO_OUTPUT|GPIO_CNF_OUTOD|GPIO_MODE_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN14)
#define GPIO_LED2 (GPIO_OUTPUT|GPIO_CNF_OUTOD|GPIO_MODE_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN15)
#define GPIO_LED3 (GPIO_OUTPUT|GPIO_CNF_OUTOD|GPIO_MODE_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN13)
#define GPIO_LED4 (GPIO_OUTPUT|GPIO_CNF_OUTOD|GPIO_MODE_50MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN11)
/* Safety switch button *******************************************************/
@@ -108,6 +108,7 @@ __EXPORT void stm32_boardinitialize(void)
stm32_configgpio(GPIO_LED1);
stm32_configgpio(GPIO_LED2);
stm32_configgpio(GPIO_LED3);
stm32_configgpio(GPIO_LED4);
stm32_configgpio(GPIO_BTN_SAFETY);
+3
View File
@@ -213,6 +213,9 @@ ORB_DECLARE(output_pwm);
/** make failsafe non-recoverable (termination) if it occurs */
#define PWM_SERVO_SET_TERMINATION_FAILSAFE _IOC(_PWM_SERVO_BASE, 25)
/** force safety switch on (to enable use of safety switch) */
#define PWM_SERVO_SET_FORCE_SAFETY_ON _IOC(_PWM_SERVO_BASE, 26)
/*
*
*
+8 -1
View File
@@ -176,6 +176,7 @@ static const int ERROR = -1;
#define L3G4200D_DEFAULT_RATE 800
#define L3GD20_DEFAULT_RANGE_DPS 2000
#define L3GD20_DEFAULT_FILTER_FREQ 30
#define L3GD20_TEMP_OFFSET_CELSIUS 40
#ifndef SENSOR_BOARD_ROTATION_DEFAULT
#define SENSOR_BOARD_ROTATION_DEFAULT SENSOR_BOARD_ROTATION_270_DEG
@@ -856,7 +857,7 @@ L3GD20::measure()
#pragma pack(push, 1)
struct {
uint8_t cmd;
uint8_t temp;
int8_t temp;
uint8_t status;
int16_t x;
int16_t y;
@@ -930,6 +931,8 @@ L3GD20::measure()
report.z_raw = raw_report.z;
report.temperature_raw = raw_report.temp;
report.x = ((report.x_raw * _gyro_range_scale) - _gyro_scale.x_offset) * _gyro_scale.x_scale;
report.y = ((report.y_raw * _gyro_range_scale) - _gyro_scale.y_offset) * _gyro_scale.y_scale;
report.z = ((report.z_raw * _gyro_range_scale) - _gyro_scale.z_offset) * _gyro_scale.z_scale;
@@ -938,6 +941,8 @@ L3GD20::measure()
report.y = _gyro_filter_y.apply(report.y);
report.z = _gyro_filter_z.apply(report.z);
report.temperature = L3GD20_TEMP_OFFSET_CELSIUS - raw_report.temp;
// apply user specified rotation
rotate_3f(_rotation, report.x, report.y, report.z);
@@ -1091,9 +1096,11 @@ test()
warnx("gyro x: \t% 9.5f\trad/s", (double)g_report.x);
warnx("gyro y: \t% 9.5f\trad/s", (double)g_report.y);
warnx("gyro z: \t% 9.5f\trad/s", (double)g_report.z);
warnx("temp: \t%d\tC", (int)g_report.temperature);
warnx("gyro x: \t%d\traw", (int)g_report.x_raw);
warnx("gyro y: \t%d\traw", (int)g_report.y_raw);
warnx("gyro z: \t%d\traw", (int)g_report.z_raw);
warnx("temp: \t%d\traw", (int)g_report.temperature_raw);
warnx("gyro range: %8.4f rad/s (%d deg/s)", (double)g_report.range_rad_s,
(int)((g_report.range_rad_s / M_PI_F) * 180.0f + 0.5f));
+187 -59
View File
@@ -73,14 +73,19 @@
/* Configuration Constants */
#define LL40LS_BUS PX4_I2C_BUS_EXPANSION
#define LL40LS_BASEADDR 0x42 /* 7-bit address */
#define LL40LS_DEVICE_PATH "/dev/ll40ls"
#define LL40LS_BASEADDR 0x62 /* 7-bit address */
#define LL40LS_BASEADDR_OLD 0x42 /* previous 7-bit address */
#define LL40LS_DEVICE_PATH_INT "/dev/ll40ls_int"
#define LL40LS_DEVICE_PATH_EXT "/dev/ll40ls_ext"
/* LL40LS Registers addresses */
#define LL40LS_MEASURE_REG 0x00 /* Measure range register */
#define LL40LS_MSRREG_ACQUIRE 0x04 /* Value to initiate a measurement, varies based on sensor revision */
#define LL40LS_MSRREG_ACQUIRE 0x04 /* Value to initiate a measurement, varies based on sensor revision */
#define LL40LS_DISTHIGH_REG 0x8F /* High byte of distance register, auto increment */
#define LL40LS_WHO_AM_I_REG 0x11
#define LL40LS_WHO_AM_I_REG_VAL 0xCA
#define LL40LS_SIGNAL_STRENGTH_REG 0x5b
/* Device limits */
#define LL40LS_MIN_DISTANCE (0.00f)
@@ -101,7 +106,7 @@ static const int ERROR = -1;
class LL40LS : public device::I2C
{
public:
LL40LS(int bus = LL40LS_BUS, int address = LL40LS_BASEADDR);
LL40LS(int bus, const char *path, int address = LL40LS_BASEADDR);
virtual ~LL40LS();
virtual int init();
@@ -116,6 +121,7 @@ public:
protected:
virtual int probe();
virtual int read_reg(uint8_t reg, uint8_t &val);
private:
float _min_distance;
@@ -132,6 +138,10 @@ private:
perf_counter_t _sample_perf;
perf_counter_t _comms_errors;
perf_counter_t _buffer_overflows;
uint16_t _last_distance;
/**< the bus the device is connected to */
int _bus;
/**
* Test whether the device supported by the driver is present at a
@@ -188,8 +198,8 @@ private:
*/
extern "C" __EXPORT int ll40ls_main(int argc, char *argv[]);
LL40LS::LL40LS(int bus, int address) :
I2C("LL40LS", LL40LS_DEVICE_PATH, bus, address, 100000),
LL40LS::LL40LS(int bus, const char *path, int address) :
I2C("LL40LS", path, bus, address, 100000),
_min_distance(LL40LS_MIN_DISTANCE),
_max_distance(LL40LS_MAX_DISTANCE),
_reports(nullptr),
@@ -200,10 +210,12 @@ LL40LS::LL40LS(int bus, int address) :
_range_finder_topic(-1),
_sample_perf(perf_alloc(PC_ELAPSED, "ll40ls_read")),
_comms_errors(perf_alloc(PC_COUNT, "ll40ls_comms_errors")),
_buffer_overflows(perf_alloc(PC_COUNT, "ll40ls_buffer_overflows"))
_buffer_overflows(perf_alloc(PC_COUNT, "ll40ls_buffer_overflows")),
_last_distance(0),
_bus(bus)
{
// up the retries since the device misses the first measure attempts
I2C::_retries = 3;
_retries = 3;
// enable debug() calls
_debug_enabled = false;
@@ -270,9 +282,51 @@ out:
return ret;
}
int
LL40LS::read_reg(uint8_t reg, uint8_t &val)
{
return transfer(&reg, 1, &val, 1);
}
int
LL40LS::probe()
{
// cope with both old and new I2C bus address
const uint8_t addresses[2] = {LL40LS_BASEADDR, LL40LS_BASEADDR_OLD};
// more retries for detection
_retries = 10;
for (uint8_t i=0; i<sizeof(addresses); i++) {
uint8_t val=0, who_am_i=0;
// set the I2C bus address
set_address(addresses[i]);
if (read_reg(LL40LS_WHO_AM_I_REG, who_am_i) == OK && who_am_i == LL40LS_WHO_AM_I_REG_VAL) {
// it is responding correctly to a WHO_AM_I
goto ok;
}
if (read_reg(LL40LS_SIGNAL_STRENGTH_REG, val) == OK && val != 0) {
// very likely to be a ll40ls. px4flow does not
// respond to this
goto ok;
}
debug("WHO_AM_I byte mismatch 0x%02x should be 0x%02x val=0x%02x\n",
(unsigned)who_am_i,
LL40LS_WHO_AM_I_REG_VAL,
(unsigned)val);
}
// not found on any address
return -EIO;
ok:
_retries = 3;
// start a measurement
return measure();
}
@@ -521,6 +575,8 @@ LL40LS::collect()
float si_units = distance * 0.01f; /* cm to m */
struct range_finder_report report;
_last_distance = distance;
/* this should be fairly close to the end of the measurement, so the best approximation of the time */
report.timestamp = hrt_absolute_time();
report.error_count = perf_event_count(_comms_errors);
@@ -648,6 +704,8 @@ LL40LS::print_info()
perf_print_counter(_buffer_overflows);
printf("poll interval: %u ticks\n", _measure_ticks);
_reports->print_info("report queue");
printf("distance: %ucm (0x%04x)\n",
(unsigned)_last_distance, (unsigned)_last_distance);
}
/**
@@ -662,55 +720,89 @@ namespace ll40ls
#endif
const int ERROR = -1;
LL40LS *g_dev;
LL40LS *g_dev_int;
LL40LS *g_dev_ext;
void start();
void stop();
void test();
void reset();
void info();
void start(int bus);
void stop(int bus);
void test(int bus);
void reset(int bus);
void info(int bus);
void usage();
/**
* Start the driver.
*/
void
start()
start(int bus)
{
int fd;
if (g_dev != nullptr) {
errx(1, "already started");
/* create the driver, attempt expansion bus first */
if (bus == -1 || bus == PX4_I2C_BUS_EXPANSION) {
if (g_dev_ext != nullptr)
errx(0, "already started external");
g_dev_ext = new LL40LS(PX4_I2C_BUS_EXPANSION, LL40LS_DEVICE_PATH_EXT);
if (g_dev_ext != nullptr && OK != g_dev_ext->init()) {
delete g_dev_ext;
g_dev_ext = nullptr;
}
}
/* create the driver */
g_dev = new LL40LS(LL40LS_BUS);
#ifdef PX4_I2C_BUS_ONBOARD
/* if this failed, attempt onboard sensor */
if (bus == -1 || bus == PX4_I2C_BUS_ONBOARD) {
if (g_dev_int != nullptr)
errx(0, "already started internal");
g_dev_int = new LL40LS(PX4_I2C_BUS_ONBOARD, LL40LS_DEVICE_PATH_INT);
if (g_dev_int != nullptr && OK != g_dev_int->init()) {
/* tear down the failing onboard instance */
delete g_dev_int;
g_dev_int = nullptr;
if (g_dev == nullptr) {
goto fail;
}
if (OK != g_dev->init()) {
goto fail;
if (bus == PX4_I2C_BUS_ONBOARD) {
goto fail;
}
}
if (g_dev_int == nullptr && bus == PX4_I2C_BUS_ONBOARD) {
goto fail;
}
}
#endif
/* set the poll rate to default, starts automatic data collection */
fd = open(LL40LS_DEVICE_PATH, O_RDONLY);
if (g_dev_int != nullptr) {
int fd = open(LL40LS_DEVICE_PATH_INT, O_RDONLY);
if (fd == -1) {
goto fail;
}
int ret = ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT);
close(fd);
if (ret < 0) {
goto fail;
}
}
if (fd < 0) {
goto fail;
}
if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0) {
goto fail;
}
if (g_dev_ext != nullptr) {
int fd = open(LL40LS_DEVICE_PATH_EXT, O_RDONLY);
if (fd == -1) {
goto fail;
}
int ret = ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT);
close(fd);
if (ret < 0) {
goto fail;
}
}
exit(0);
fail:
if (g_dev != nullptr) {
delete g_dev;
g_dev = nullptr;
if (g_dev_int != nullptr && (bus == -1 || bus == PX4_I2C_BUS_ONBOARD)) {
delete g_dev_int;
g_dev_int = nullptr;
}
if (g_dev_ext != nullptr && (bus == -1 || bus == PX4_I2C_BUS_EXPANSION)) {
delete g_dev_ext;
g_dev_ext = nullptr;
}
errx(1, "driver start failed");
@@ -719,11 +811,12 @@ fail:
/**
* Stop the driver
*/
void stop()
void stop(int bus)
{
if (g_dev != nullptr) {
delete g_dev;
g_dev = nullptr;
LL40LS **g_dev = (bus == PX4_I2C_BUS_ONBOARD?&g_dev_int:&g_dev_ext);
if (*g_dev != nullptr) {
delete *g_dev;
*g_dev = nullptr;
} else {
errx(1, "driver not running");
@@ -738,16 +831,17 @@ void stop()
* and automatic modes.
*/
void
test()
test(int bus)
{
struct range_finder_report report;
ssize_t sz;
int ret;
const char *path = (bus==PX4_I2C_BUS_ONBOARD?LL40LS_DEVICE_PATH_INT:LL40LS_DEVICE_PATH_EXT);
int fd = open(LL40LS_DEVICE_PATH, O_RDONLY);
int fd = open(path, O_RDONLY);
if (fd < 0) {
err(1, "%s open failed (try 'll40ls start' if the driver is not running", LL40LS_DEVICE_PATH);
err(1, "%s open failed (try 'll40ls start' if the driver is not running", path);
}
/* do a simple demand read */
@@ -803,9 +897,10 @@ test()
* Reset the driver.
*/
void
reset()
reset(int bus)
{
int fd = open(LL40LS_DEVICE_PATH, O_RDONLY);
const char *path = (bus==PX4_I2C_BUS_ONBOARD?LL40LS_DEVICE_PATH_INT:LL40LS_DEVICE_PATH_EXT);
int fd = open(path, O_RDONLY);
if (fd < 0) {
err(1, "failed ");
@@ -826,8 +921,9 @@ reset()
* Print a little info about the driver.
*/
void
info()
info(int bus)
{
LL40LS *g_dev = (bus == PX4_I2C_BUS_ONBOARD?g_dev_int:g_dev_ext);
if (g_dev == nullptr) {
errx(1, "driver not running");
}
@@ -838,44 +934,76 @@ info()
exit(0);
}
void
usage()
{
warnx("missing command: try 'start', 'stop', 'info', 'test', 'reset', 'info'");
warnx("options:");
warnx(" -X only external bus");
#ifdef PX4_I2C_BUS_ONBOARD
warnx(" -I only internal bus");
#endif
}
} // namespace
int
ll40ls_main(int argc, char *argv[])
{
int ch;
int bus = -1;
while ((ch = getopt(argc, argv, "XI")) != EOF) {
switch (ch) {
#ifdef PX4_I2C_BUS_ONBOARD
case 'I':
bus = PX4_I2C_BUS_ONBOARD;
break;
#endif
case 'X':
bus = PX4_I2C_BUS_EXPANSION;
break;
default:
ll40ls::usage();
exit(0);
}
}
const char *verb = argv[optind];
/*
* Start/load the driver.
*/
if (!strcmp(argv[1], "start")) {
ll40ls::start();
if (!strcmp(verb, "start")) {
ll40ls::start(bus);
}
/*
* Stop the driver
*/
if (!strcmp(argv[1], "stop")) {
ll40ls::stop();
if (!strcmp(verb, "stop")) {
ll40ls::stop(bus);
}
/*
* Test the driver/device.
*/
if (!strcmp(argv[1], "test")) {
ll40ls::test();
if (!strcmp(verb, "test")) {
ll40ls::test(bus);
}
/*
* Reset the driver.
*/
if (!strcmp(argv[1], "reset")) {
ll40ls::reset();
if (!strcmp(verb, "reset")) {
ll40ls::reset(bus);
}
/*
* Print driver information.
*/
if (!strcmp(argv[1], "info") || !strcmp(argv[1], "status")) {
ll40ls::info();
if (!strcmp(verb, "info") || !strcmp(verb, "status")) {
ll40ls::info(bus);
}
errx(1, "unrecognized command, try 'start', 'test', 'reset' or 'info'");
+11
View File
@@ -229,6 +229,7 @@ private:
perf_counter_t _gyro_reads;
perf_counter_t _sample_perf;
perf_counter_t _bad_transfers;
perf_counter_t _good_transfers;
math::LowPassFilter2p _accel_filter_x;
math::LowPassFilter2p _accel_filter_y;
@@ -404,6 +405,7 @@ MPU6000::MPU6000(int bus, const char *path_accel, const char *path_gyro, spi_dev
_gyro_reads(perf_alloc(PC_COUNT, "mpu6000_gyro_read")),
_sample_perf(perf_alloc(PC_ELAPSED, "mpu6000_read")),
_bad_transfers(perf_alloc(PC_COUNT, "mpu6000_bad_transfers")),
_good_transfers(perf_alloc(PC_COUNT, "mpu6000_good_transfers")),
_accel_filter_x(MPU6000_ACCEL_DEFAULT_RATE, MPU6000_ACCEL_DEFAULT_DRIVER_FILTER_FREQ),
_accel_filter_y(MPU6000_ACCEL_DEFAULT_RATE, MPU6000_ACCEL_DEFAULT_DRIVER_FILTER_FREQ),
_accel_filter_z(MPU6000_ACCEL_DEFAULT_RATE, MPU6000_ACCEL_DEFAULT_DRIVER_FILTER_FREQ),
@@ -456,6 +458,7 @@ MPU6000::~MPU6000()
perf_free(_accel_reads);
perf_free(_gyro_reads);
perf_free(_bad_transfers);
perf_free(_good_transfers);
}
int
@@ -1279,8 +1282,14 @@ MPU6000::measure()
// all zero data - probably a SPI bus error
perf_count(_bad_transfers);
perf_end(_sample_perf);
// note that we don't call reset() here as a reset()
// costs 20ms with interrupts disabled. That means if
// the mpu6k does go bad it would cause a FMU failure,
// regardless of whether another sensor is available,
return;
}
perf_count(_good_transfers);
/*
@@ -1399,6 +1408,8 @@ MPU6000::print_info()
perf_print_counter(_sample_perf);
perf_print_counter(_accel_reads);
perf_print_counter(_gyro_reads);
perf_print_counter(_bad_transfers);
perf_print_counter(_good_transfers);
_accel_reports->print_info("accel queue");
_gyro_reports->print_info("gyro queue");
}
+112 -69
View File
@@ -76,7 +76,7 @@
#define PX4FLOW_BUS PX4_I2C_BUS_EXPANSION
#define I2C_FLOW_ADDRESS 0x42 //* 7-bit address. 8-bit address is 0x84
//range 0x42 - 0x49
/* PX4FLOW Registers addresses */
#define PX4FLOW_REG 0x00 /* Measure Register */
@@ -212,8 +212,9 @@ PX4FLOW::~PX4FLOW()
stop();
/* free any existing reports */
if (_reports != nullptr)
if (_reports != nullptr) {
delete _reports;
}
}
int
@@ -222,22 +223,25 @@ PX4FLOW::init()
int ret = ERROR;
/* do I2C init (and probe) first */
if (I2C::init() != OK)
if (I2C::init() != OK) {
goto out;
}
/* allocate basic report buffers */
_reports = new RingBuffer(2, sizeof(struct optical_flow_s));
if (_reports == nullptr)
if (_reports == nullptr) {
goto out;
}
/* get a publish handle on the px4flow topic */
struct optical_flow_s zero_report;
memset(&zero_report, 0, sizeof(zero_report));
_px4flow_topic = orb_advertise(ORB_ID(optical_flow), &zero_report);
if (_px4flow_topic < 0)
if (_px4flow_topic < 0) {
debug("failed to create px4flow object. Did you start uOrb?");
}
ret = OK;
/* sensor is ok, but we don't really know if it is within range */
@@ -249,6 +253,17 @@ out:
int
PX4FLOW::probe()
{
uint8_t val[22];
// to be sure this is not a ll40ls Lidar (which can also be on
// 0x42) we check if a 22 byte transfer works from address
// 0. The ll40ls gives an error for that, whereas the flow
// happily returns some data
if (transfer(nullptr, 0, &val[0], 22) != OK) {
return -EIO;
}
// that worked, so start a measurement cycle
return measure();
}
@@ -260,20 +275,20 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg)
case SENSORIOCSPOLLRATE: {
switch (arg) {
/* switching to manual polling */
/* switching to manual polling */
case SENSOR_POLLRATE_MANUAL:
stop();
_measure_ticks = 0;
return OK;
/* external signalling (DRDY) not supported */
/* external signalling (DRDY) not supported */
case SENSOR_POLLRATE_EXTERNAL:
/* zero would be bad */
/* zero would be bad */
case 0:
return -EINVAL;
/* set default/max polling rate */
/* set default/max polling rate */
case SENSOR_POLLRATE_MAX:
case SENSOR_POLLRATE_DEFAULT: {
/* do we need to start internal polling? */
@@ -283,13 +298,14 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg)
_measure_ticks = USEC2TICK(PX4FLOW_CONVERSION_INTERVAL);
/* if we need to start the poll state machine, do it */
if (want_start)
if (want_start) {
start();
}
return OK;
}
/* adjust to a legal polling interval in Hz */
/* adjust to a legal polling interval in Hz */
default: {
/* do we need to start internal polling? */
bool want_start = (_measure_ticks == 0);
@@ -298,15 +314,17 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg)
unsigned ticks = USEC2TICK(1000000 / arg);
/* check against maximum rate */
if (ticks < USEC2TICK(PX4FLOW_CONVERSION_INTERVAL))
if (ticks < USEC2TICK(PX4FLOW_CONVERSION_INTERVAL)) {
return -EINVAL;
}
/* update interval for next measurement */
_measure_ticks = ticks;
/* if we need to start the poll state machine, do it */
if (want_start)
if (want_start) {
start();
}
return OK;
}
@@ -314,25 +332,29 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg)
}
case SENSORIOCGPOLLRATE:
if (_measure_ticks == 0)
if (_measure_ticks == 0) {
return SENSOR_POLLRATE_MANUAL;
}
return (1000 / _measure_ticks);
case SENSORIOCSQUEUEDEPTH: {
/* lower bound is mandatory, upper bound is a sanity check */
if ((arg < 1) || (arg > 100))
return -EINVAL;
/* lower bound is mandatory, upper bound is a sanity check */
if ((arg < 1) || (arg > 100)) {
return -EINVAL;
}
irqstate_t flags = irqsave();
if (!_reports->resize(arg)) {
irqrestore(flags);
return -ENOMEM;
}
irqstate_t flags = irqsave();
if (!_reports->resize(arg)) {
irqrestore(flags);
return -ENOMEM;
}
irqrestore(flags);
return OK;
}
return OK;
}
case SENSORIOCGQUEUEDEPTH:
return _reports->size();
@@ -355,8 +377,9 @@ PX4FLOW::read(struct file *filp, char *buffer, size_t buflen)
int ret = 0;
/* buffer must be large enough */
if (count < 1)
if (count < 1) {
return -ENOSPC;
}
/* if automatic measurement is enabled */
if (_measure_ticks > 0) {
@@ -417,13 +440,13 @@ PX4FLOW::measure()
uint8_t cmd = PX4FLOW_REG;
ret = transfer(&cmd, 1, nullptr, 0);
if (OK != ret)
{
if (OK != ret) {
perf_count(_comms_errors);
log("i2c::transfer returned %d", ret);
printf("i2c::transfer flow returned %d");
printf("i2c::transfer flow returned %d");
return ret;
}
ret = OK;
return ret;
@@ -435,14 +458,13 @@ PX4FLOW::collect()
int ret = -EIO;
/* read from the sensor */
uint8_t val[22] = {0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0};
uint8_t val[22] = {0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0};
perf_begin(_sample_perf);
ret = transfer(nullptr, 0, &val[0], 22);
if (ret < 0)
{
if (ret < 0) {
log("error reading from sensor: %d", ret);
perf_count(_comms_errors);
perf_end(_sample_perf);
@@ -467,12 +489,12 @@ PX4FLOW::collect()
int16_t gdist = val[21] << 8 | val[20];
struct optical_flow_s report;
report.flow_comp_x_m = float(flowcx)/1000.0f;
report.flow_comp_y_m = float(flowcy)/1000.0f;
report.flow_raw_x= val[3] << 8 | val[2];
report.flow_raw_y= val[5] << 8 | val[4];
report.ground_distance_m =float(gdist)/1000.0f;
report.quality= val[10];
report.flow_comp_x_m = float(flowcx) / 1000.0f;
report.flow_comp_y_m = float(flowcy) / 1000.0f;
report.flow_raw_x = val[3] << 8 | val[2];
report.flow_raw_y = val[5] << 8 | val[4];
report.ground_distance_m = float(gdist) / 1000.0f;
report.quality = val[10];
report.sensor_id = 0;
report.timestamp = hrt_absolute_time();
@@ -509,11 +531,13 @@ PX4FLOW::start()
true,
true,
true,
SUBSYSTEM_TYPE_OPTICALFLOW};
SUBSYSTEM_TYPE_OPTICALFLOW
};
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);
}
@@ -567,8 +591,9 @@ PX4FLOW::cycle()
}
/* measurement phase */
if (OK != measure())
if (OK != measure()) {
log("measure error");
}
/* next phase is collection */
_collect_phase = true;
@@ -619,33 +644,37 @@ start()
{
int fd;
if (g_dev != nullptr)
if (g_dev != nullptr) {
errx(1, "already started");
}
/* create the driver */
g_dev = new PX4FLOW(PX4FLOW_BUS);
if (g_dev == nullptr)
if (g_dev == nullptr) {
goto fail;
}
if (OK != g_dev->init())
if (OK != g_dev->init()) {
goto fail;
}
/* set the poll rate to default, starts automatic data collection */
fd = open(PX4FLOW_DEVICE_PATH, O_RDONLY);
if (fd < 0)
if (fd < 0) {
goto fail;
}
if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_MAX) < 0)
if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_MAX) < 0) {
goto fail;
}
exit(0);
fail:
if (g_dev != nullptr)
{
if (g_dev != nullptr) {
delete g_dev;
g_dev = nullptr;
}
@@ -658,15 +687,14 @@ 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);
}
@@ -684,14 +712,17 @@ test()
int fd = open(PX4FLOW_DEVICE_PATH, O_RDONLY);
if (fd < 0)
if (fd < 0) {
err(1, "%s open failed (try 'px4flow start' if the driver is not running", PX4FLOW_DEVICE_PATH);
}
/* do a simple demand read */
sz = read(fd, &report, sizeof(report));
if (sz != sizeof(report))
// err(1, "immediate read failed");
{
warnx("immediate read failed");
}
warnx("single read");
warnx("flowx: %0.2f m/s", (double)report.flow_comp_x_m);
@@ -700,8 +731,9 @@ test()
/* start the sensor polling at 2Hz */
if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2))
if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) {
errx(1, "failed to set 2Hz poll rate");
}
/* read the sensor 5x and report each value */
for (unsigned i = 0; i < 5; i++) {
@@ -712,14 +744,16 @@ test()
fds.events = POLLIN;
ret = poll(&fds, 1, 2000);
if (ret != 1)
if (ret != 1) {
errx(1, "timed out waiting for sensor data");
}
/* now go get it */
sz = read(fd, &report, sizeof(report));
if (sz != sizeof(report))
if (sz != sizeof(report)) {
err(1, "periodic read failed");
}
warnx("periodic read %u", i);
warnx("flowx: %0.2f m/s", (double)report.flow_comp_x_m);
@@ -740,14 +774,17 @@ reset()
{
int fd = open(PX4FLOW_DEVICE_PATH, O_RDONLY);
if (fd < 0)
if (fd < 0) {
err(1, "failed ");
}
if (ioctl(fd, SENSORIOCRESET, 0) < 0)
if (ioctl(fd, SENSORIOCRESET, 0) < 0) {
err(1, "driver reset failed");
}
if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0)
if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0) {
err(1, "driver poll restart failed");
}
exit(0);
}
@@ -758,8 +795,9 @@ reset()
void
info()
{
if (g_dev == nullptr)
if (g_dev == nullptr) {
errx(1, "driver not running");
}
printf("state @ %p\n", g_dev);
g_dev->print_info();
@@ -775,32 +813,37 @@ px4flow_main(int argc, char *argv[])
/*
* Start/load the driver.
*/
if (!strcmp(argv[1], "start"))
if (!strcmp(argv[1], "start")) {
px4flow::start();
}
/*
* Stop the driver
*/
if (!strcmp(argv[1], "stop"))
px4flow::stop();
/*
* Stop the driver
*/
if (!strcmp(argv[1], "stop")) {
px4flow::stop();
}
/*
* Test the driver/device.
*/
if (!strcmp(argv[1], "test"))
if (!strcmp(argv[1], "test")) {
px4flow::test();
}
/*
* Reset the driver.
*/
if (!strcmp(argv[1], "reset"))
if (!strcmp(argv[1], "reset")) {
px4flow::reset();
}
/*
* Print driver information.
*/
if (!strcmp(argv[1], "info") || !strcmp(argv[1], "status"))
if (!strcmp(argv[1], "info") || !strcmp(argv[1], "status")) {
px4flow::info();
}
errx(1, "unrecognized command, try 'start', 'test', 'reset' or 'info'");
}
+1
View File
@@ -829,6 +829,7 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg)
case PWM_SERVO_SET_ARM_OK:
case PWM_SERVO_CLEAR_ARM_OK:
case PWM_SERVO_SET_FORCE_SAFETY_OFF:
case PWM_SERVO_SET_FORCE_SAFETY_ON:
// these are no-ops, as no safety switch
break;
+23 -6
View File
@@ -1247,28 +1247,40 @@ PX4IO::io_set_rc_config()
*/
param_get(param_find("RC_MAP_ROLL"), &ichan);
/* subtract one from 1-based index - this might be
* a negative number now
*/
ichan -= 1;
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan - 1] = 0;
input_map[ichan] = 0;
param_get(param_find("RC_MAP_PITCH"), &ichan);
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan - 1] = 1;
input_map[ichan] = 1;
param_get(param_find("RC_MAP_YAW"), &ichan);
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan - 1] = 2;
input_map[ichan] = 2;
param_get(param_find("RC_MAP_THROTTLE"), &ichan);
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan - 1] = 3;
input_map[ichan] = 3;
param_get(param_find("RC_MAP_FLAPS"), &ichan);
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan] = 4;
param_get(param_find("RC_MAP_MODE_SW"), &ichan);
if ((ichan >= 0) && (ichan < (int)_max_rc_input))
input_map[ichan - 1] = 4;
if ((ichan >= 0) && (ichan < (int)_max_rc_input)) {
/* use out of normal bounds index to indicate special channel */
input_map[ichan] = PX4IO_P_RC_CONFIG_ASSIGNMENT_MODESWITCH;
}
/*
* Iterate all possible RC inputs.
@@ -2271,6 +2283,11 @@ PX4IO::ioctl(file * filep, int cmd, unsigned long arg)
ret = io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FORCE_SAFETY_OFF, PX4IO_FORCE_SAFETY_MAGIC);
break;
case PWM_SERVO_SET_FORCE_SAFETY_ON:
/* force safety switch on */
ret = io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FORCE_SAFETY_ON, PX4IO_FORCE_SAFETY_MAGIC);
break;
case PWM_SERVO_SET_FORCE_FAILSAFE:
/* force failsafe mode instantly */
if (arg == 0) {
+3 -1
View File
@@ -74,6 +74,7 @@ enum Rotation {
ROTATION_ROLL_270_YAW_135 = 23,
ROTATION_PITCH_90 = 24,
ROTATION_PITCH_270 = 25,
ROTATION_ROLL_270_YAW_270 = 26,
ROTATION_MAX
};
@@ -109,7 +110,8 @@ const rot_lookup_t rot_lookup[] = {
{270, 0, 90 },
{270, 0, 135 },
{ 0, 90, 0 },
{ 0, 270, 0 }
{ 0, 270, 0 },
{270, 0, 270 }
};
/**
+4 -4
View File
@@ -299,7 +299,7 @@ void TECS::_update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotM
// Calculate throttle demand
// If underspeed condition is set, then demand full throttle
if (_underspeed) {
_throttle_dem_unc = 1.0f;
_throttle_dem = 1.0f;
} else {
// Calculate gain scaler from specific energy error to throttle
@@ -363,10 +363,10 @@ void TECS::_update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotM
} else {
_throttle_dem = ff_throttle;
}
}
// Constrain throttle demand
_throttle_dem = constrain(_throttle_dem, _THRminf, _THRmaxf);
// Constrain throttle demand
_throttle_dem = constrain(_throttle_dem, _THRminf, _THRmaxf);
}
}
void TECS::_detect_bad_descent(void)
-3
View File
@@ -345,9 +345,6 @@ private:
// climbout mode
bool _climbOutDem;
// throttle demand before limiting
float _throttle_dem_unc;
// pitch demand before limiting
float _pitch_dem_unc;
@@ -83,7 +83,7 @@
* | accel_T[1][i] |
* [ accel_T[2][i] ]
*
* b = [ accel_corr_ref[0][i] ] // One measurement per axis is enough
* b = [ accel_corr_ref[0][i] ] // One measurement per side is enough
* | accel_corr_ref[2][i] |
* [ accel_corr_ref[4][i] ]
*
@@ -162,6 +162,11 @@ int do_accel_calibration(int mavlink_fd)
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
mavlink_log_info(mavlink_fd, "You need to put the system on all six sides");
sleep(3);
mavlink_log_info(mavlink_fd, "Follow the instructions on the screen");
sleep(5);
struct accel_scale accel_scale = {
0.0f,
1.0f,
@@ -258,7 +263,7 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
const int samples_num = 2500;
float accel_ref[6][3];
bool data_collected[6] = { false, false, false, false, false, false };
const char *orientation_strs[6] = { "x+", "x-", "y+", "y-", "z+", "z-" };
const char *orientation_strs[6] = { "front", "back", "left", "right", "top", "bottom" };
int sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
@@ -287,29 +292,37 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
break;
}
mavlink_log_info(mavlink_fd, "directions left: %s%s%s%s%s%s",
(!data_collected[0]) ? "x+ " : "",
(!data_collected[1]) ? "x- " : "",
(!data_collected[2]) ? "y+ " : "",
(!data_collected[3]) ? "y- " : "",
(!data_collected[4]) ? "z+ " : "",
(!data_collected[5]) ? "z- " : "");
/* inform user which axes are still needed */
mavlink_log_info(mavlink_fd, "pending: %s%s%s%s%s%s",
(!data_collected[0]) ? "front " : "",
(!data_collected[1]) ? "back " : "",
(!data_collected[2]) ? "left " : "",
(!data_collected[3]) ? "right " : "",
(!data_collected[4]) ? "up " : "",
(!data_collected[5]) ? "down " : "");
/* allow user enough time to read the message */
sleep(3);
int orient = detect_orientation(mavlink_fd, sensor_combined_sub);
if (orient < 0) {
res = ERROR;
break;
}
if (data_collected[orient]) {
mavlink_log_info(mavlink_fd, "%s done, rotate to a different axis", orientation_strs[orient]);
mavlink_log_info(mavlink_fd, "invalid motion, hold still...");
sleep(3);
continue;
}
mavlink_log_info(mavlink_fd, "accel measurement started: %s axis", orientation_strs[orient]);
/* inform user about already handled side */
if (data_collected[orient]) {
mavlink_log_info(mavlink_fd, "%s side done, rotate to a different side", orientation_strs[orient]);
sleep(4);
continue;
}
mavlink_log_info(mavlink_fd, "Hold still, starting to measure %s side", orientation_strs[orient]);
sleep(1);
read_accelerometer_avg(sensor_combined_sub, &(accel_ref[orient][0]), samples_num);
mavlink_log_info(mavlink_fd, "result for %s axis: [ %.2f %.2f %.2f ]", orientation_strs[orient],
mavlink_log_info(mavlink_fd, "result for %s side: [ %.2f %.2f %.2f ]", orientation_strs[orient],
(double)accel_ref[orient][0],
(double)accel_ref[orient][1],
(double)accel_ref[orient][2]);
@@ -400,7 +413,7 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined)
/* is still now */
if (t_still == 0) {
/* first time */
mavlink_log_info(mavlink_fd, "detected rest position, waiting...");
mavlink_log_info(mavlink_fd, "detected rest position, hold still...");
t_still = t;
t_timeout = t + timeout;
@@ -418,6 +431,7 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined)
/* not still, reset still start time */
if (t_still != 0) {
mavlink_log_info(mavlink_fd, "detected motion, hold still...");
sleep(3);
t_still = 0;
}
}
+17 -8
View File
@@ -61,6 +61,15 @@ static const int ERROR = -1;
static const char *sensor_name = "dpress";
#define HUMAN_ASPD_CAL_FAILED_MSG "Calibration failed, see http://px4.io/help/aspd"
static void feedback_calibration_failed(int mavlink_fd)
{
sleep(5);
mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
mavlink_log_critical(mavlink_fd, HUMAN_ASPD_CAL_FAILED_MSG);
}
int do_airspeed_calibration(int mavlink_fd)
{
/* give directions */
@@ -99,7 +108,7 @@ int do_airspeed_calibration(int mavlink_fd)
float analog_scaling = 0.0f;
param_get(param_find("SENS_DPRES_ANSC"), &(analog_scaling));
if (fabsf(analog_scaling) < 0.1f) {
mavlink_log_critical(mavlink_fd, "If analog sens, retry with [SENS_DPRES_ANSC=1000]");
mavlink_log_critical(mavlink_fd, "No airspeed sensor, see http://px4.io/help/aspd");
close(diff_pres_sub);
return ERROR;
}
@@ -138,7 +147,7 @@ int do_airspeed_calibration(int mavlink_fd)
} else if (poll_ret == 0) {
/* any poll failure for 1s is a reason to abort */
mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
feedback_calibration_failed(mavlink_fd);
close(diff_pres_sub);
return ERROR;
}
@@ -175,7 +184,7 @@ int do_airspeed_calibration(int mavlink_fd)
}
} else {
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
feedback_calibration_failed(mavlink_fd);
close(diff_pres_sub);
return ERROR;
}
@@ -207,7 +216,7 @@ int do_airspeed_calibration(int mavlink_fd)
if (fabsf(diff_pres.differential_pressure_raw_pa) < 50.0f) {
if (calibration_counter % 500 == 0) {
mavlink_log_info(mavlink_fd, "Create airflow! (%d, wanted: 50 Pa)",
mavlink_log_info(mavlink_fd, "Create air pressure! (got %d, wanted: 50 Pa)",
(int)diff_pres.differential_pressure_raw_pa);
}
continue;
@@ -215,9 +224,9 @@ int do_airspeed_calibration(int mavlink_fd)
/* do not allow negative values */
if (diff_pres.differential_pressure_raw_pa < 0.0f) {
mavlink_log_critical(mavlink_fd, "Swap static and dynamic ports!");
mavlink_log_info(mavlink_fd, "ERROR: Negative pressure difference detected! (%d Pa)",
(int)diff_pres.differential_pressure_raw_pa);
mavlink_log_critical(mavlink_fd, "Swap static and dynamic ports!");
close(diff_pres_sub);
/* the user setup is wrong, wipe the calibration to force a proper re-calibration */
@@ -235,7 +244,7 @@ int do_airspeed_calibration(int mavlink_fd)
close(diff_pres_sub);
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
feedback_calibration_failed(mavlink_fd);
return ERROR;
} else {
mavlink_log_info(mavlink_fd, "Positive pressure: OK (%d Pa)",
@@ -245,14 +254,14 @@ int do_airspeed_calibration(int mavlink_fd)
} else if (poll_ret == 0) {
/* any poll failure for 1s is a reason to abort */
mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
feedback_calibration_failed(mavlink_fd);
close(diff_pres_sub);
return ERROR;
}
}
if (calibration_counter == maxcount) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_MSG, sensor_name);
feedback_calibration_failed(mavlink_fd);
close(diff_pres_sub);
return ERROR;
}
+162 -91
View File
@@ -207,7 +207,9 @@ void usage(const char *reason);
/**
* React to commands that are sent e.g. from the mavlink module.
*/
bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub);
bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd,
struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos,
orb_advert_t *home_pub);
/**
* Mainloop of commander.
@@ -230,7 +232,8 @@ void print_reject_arm(const char *msg);
void print_status();
transition_result_t check_navigation_state_machine(struct vehicle_status_s *status, struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos);
transition_result_t check_navigation_state_machine(struct vehicle_status_s *status,
struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos);
transition_result_t arm_disarm(bool arm, const int mavlink_fd, const char *armedBy);
@@ -260,7 +263,7 @@ int commander_main(int argc, char *argv[])
daemon_task = task_spawn_cmd("commander",
SCHED_DEFAULT,
SCHED_PRIORITY_MAX - 40,
2950,
3200,
commander_thread_main,
(argv) ? (const char **)&argv[2] : (const char **)NULL);
@@ -393,7 +396,8 @@ transition_result_t arm_disarm(bool arm, const int mavlink_fd_local, const char
// Transition the armed state. By passing mavlink_fd to arming_state_transition it will
// output appropriate error messages if the state cannot transition.
arming_res = arming_state_transition(&status, &safety, arm ? ARMING_STATE_ARMED : ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */, mavlink_fd_local);
arming_res = arming_state_transition(&status, &safety, arm ? ARMING_STATE_ARMED : ARMING_STATE_STANDBY, &armed,
true /* fRunPreArmChecks */, mavlink_fd_local);
if (arming_res == TRANSITION_CHANGED && mavlink_fd) {
mavlink_log_info(mavlink_fd_local, "[cmd] %s by %s", arm ? "ARMED" : "DISARMED", armedBy);
@@ -406,11 +410,12 @@ transition_result_t arm_disarm(bool arm, const int mavlink_fd_local, const char
}
bool handle_command(struct vehicle_status_s *status_local, const struct safety_s *safety_local,
struct vehicle_command_s *cmd, struct actuator_armed_s *armed_local,
struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub)
struct vehicle_command_s *cmd, struct actuator_armed_s *armed_local,
struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub)
{
/* only handle commands that are meant to be handled by this system and component */
if (cmd->target_system != status_local->system_id || ((cmd->target_component != status_local->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components
if (cmd->target_system != status_local->system_id || ((cmd->target_component != status_local->component_id)
&& (cmd->target_component != 0))) { // component_id 0: valid for all components
return false;
}
@@ -537,13 +542,13 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
} else {
mavlink_log_critical(mavlink_fd, "REJ CMD: %.1f %.1f %.1f %.1f %.1f %.1f %.1f %.1f",
(double)cmd->param1,
(double)cmd->param2,
(double)cmd->param3,
(double)cmd->param4,
(double)cmd->param5,
(double)cmd->param6,
(double)cmd->param7);
(double)cmd->param1,
(double)cmd->param2,
(double)cmd->param3,
(double)cmd->param4,
(double)cmd->param5,
(double)cmd->param6,
(double)cmd->param7);
}
}
break;
@@ -554,35 +559,43 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
//XXX update state machine?
armed_local->force_failsafe = true;
warnx("forcing failsafe (termination)");
} else {
armed_local->force_failsafe = false;
warnx("disabling failsafe (termination)");
}
/* param2 is currently used for other failsafe modes */
status_local->engine_failure_cmd = false;
status_local->data_link_lost_cmd = false;
status_local->gps_failure_cmd = false;
status_local->rc_signal_lost_cmd = false;
if ((int)cmd->param2 <= 0) {
/* reset all commanded failure modes */
warnx("reset all non-flighttermination failsafe commands");
} else if ((int)cmd->param2 == 1) {
/* trigger engine failure mode */
status_local->engine_failure_cmd = true;
warnx("engine failure mode commanded");
} else if ((int)cmd->param2 == 2) {
/* trigger data link loss mode */
status_local->data_link_lost_cmd = true;
warnx("data link loss mode commanded");
} else if ((int)cmd->param2 == 3) {
/* trigger gps loss mode */
status_local->gps_failure_cmd = true;
warnx("gps loss mode commanded");
} else if ((int)cmd->param2 == 4) {
/* trigger rc loss mode */
status_local->rc_signal_lost_cmd = true;
warnx("rc loss mode commanded");
}
cmd_result = VEHICLE_CMD_RESULT_ACCEPTED;
}
break;
@@ -633,21 +646,27 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
}
}
break;
case VEHICLE_CMD_NAV_GUIDED_ENABLE: {
transition_result_t res = TRANSITION_DENIED;
static main_state_t main_state_pre_offboard = MAIN_STATE_MANUAL;
if (status_local->main_state != MAIN_STATE_OFFBOARD) {
main_state_pre_offboard = status_local->main_state;
}
if (cmd->param1 > 0.5f) {
res = main_state_transition(status_local, MAIN_STATE_OFFBOARD);
if (res == TRANSITION_DENIED) {
print_reject_mode(status_local, "OFFBOARD");
status_local->offboard_control_set_by_command = false;
} else {
/* Set flag that offboard was set via command, main state is not overridden by rc */
status_local->offboard_control_set_by_command = true;
}
} else {
/* If the mavlink command is used to enable or disable offboard control:
* switch back to previous mode when disabling */
@@ -656,6 +675,7 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s
}
}
break;
case VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
case VEHICLE_CMD_PREFLIGHT_CALIBRATION:
case VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS:
@@ -802,6 +822,7 @@ int commander_thread_main(int argc, char *argv[])
/* publish initial state */
status_pub = orb_advertise(ORB_ID(vehicle_status), &status);
if (status_pub < 0) {
warnx("ERROR: orb_advertise for topic vehicle_status failed (uorb app running?).\n");
warnx("exiting.");
@@ -827,11 +848,14 @@ int commander_thread_main(int argc, char *argv[])
/* init mission state, do it here to allow navigator to use stored mission even if mavlink failed to start */
orb_advert_t mission_pub = -1;
mission_s mission;
if (dm_read(DM_KEY_MISSION_STATE, 0, &mission, sizeof(mission_s)) == sizeof(mission_s)) {
if (mission.dataman_id >= 0 && mission.dataman_id <= 1) {
warnx("loaded mission state: dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count, mission.current_seq);
warnx("loaded mission state: dataman_id=%d, count=%u, current=%d", mission.dataman_id, mission.count,
mission.current_seq);
mavlink_log_info(mavlink_fd, "[cmd] dataman_id=%d, count=%u, current=%d",
mission.dataman_id, mission.count, mission.current_seq);
mission.dataman_id, mission.count, mission.current_seq);
} else {
const char *missionfail = "reading mission state failed";
warnx("%s", missionfail);
@@ -1097,6 +1121,7 @@ int commander_thread_main(int argc, char *argv[])
status.offboard_control_signal_lost = false;
status_changed = true;
}
} else {
if (!status.offboard_control_signal_lost) {
status.offboard_control_signal_lost = true;
@@ -1115,9 +1140,9 @@ int commander_thread_main(int argc, char *argv[])
/* perform system checks when new telemetry link connected */
if (mavlink_fd &&
telemetry_last_heartbeat[i] == 0 &&
telemetry.heartbeat_time > 0 &&
hrt_elapsed_time(&telemetry.heartbeat_time) < datalink_loss_timeout * 1e6) {
telemetry_last_heartbeat[i] == 0 &&
telemetry.heartbeat_time > 0 &&
hrt_elapsed_time(&telemetry.heartbeat_time) < datalink_loss_timeout * 1e6) {
(void)rc_calibration_check(mavlink_fd);
}
@@ -1130,6 +1155,7 @@ int commander_thread_main(int argc, char *argv[])
if (updated) {
orb_copy(ORB_ID(sensor_combined), sensor_sub, &sensors);
/* Check if the barometer is healthy and issue a warning in the GCS if not so.
* Because the barometer is used for calculating AMSL altitude which is used to ensure
* vertical separation from other airtraffic the operator has to know when the
@@ -1142,6 +1168,7 @@ int commander_thread_main(int argc, char *argv[])
status_changed = true;
mavlink_log_critical(mavlink_fd, "baro healthy");
}
} else {
if (!status.barometer_failure) {
status.barometer_failure = true;
@@ -1164,10 +1191,11 @@ int commander_thread_main(int argc, char *argv[])
if (hrt_elapsed_time(&system_power.timestamp) < 200000) {
if (system_power.servo_valid &&
!system_power.brick_valid &&
!system_power.usb_connected) {
!system_power.brick_valid &&
!system_power.usb_connected) {
/* flying only on servo rail, this is unsafe */
status.condition_power_input_valid = false;
} else {
status.condition_power_input_valid = true;
}
@@ -1187,9 +1215,11 @@ int commander_thread_main(int argc, char *argv[])
/* disarm if safety is now on and still armed */
if (status.hil_state == HIL_STATE_OFF && safety.safety_switch_available && !safety.safety_off && armed.armed) {
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY :
ARMING_STATE_STANDBY_ERROR);
if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */, mavlink_fd)) {
if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed,
true /* fRunPreArmChecks */, mavlink_fd)) {
mavlink_log_info(mavlink_fd, "DISARMED by safety switch");
arming_state_changed = true;
}
@@ -1233,7 +1263,8 @@ int commander_thread_main(int argc, char *argv[])
}
}
check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_good, &(status.condition_global_position_valid), &status_changed);
check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_good, &(status.condition_global_position_valid),
&status_changed);
/* update home position */
if (!status.condition_home_position_valid && status.condition_global_position_valid && !armed.armed &&
@@ -1283,8 +1314,11 @@ int commander_thread_main(int argc, char *argv[])
local_eph_good = false;
}
}
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid && local_eph_good, &(status.condition_local_position_valid), &status_changed);
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid, &(status.condition_local_altitude_valid), &status_changed);
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid
&& local_eph_good, &(status.condition_local_position_valid), &status_changed);
check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid,
&(status.condition_local_altitude_valid), &status_changed);
if (status.condition_local_altitude_valid) {
if (status.condition_landed != local_position.landed) {
@@ -1315,7 +1349,8 @@ int commander_thread_main(int argc, char *argv[])
/* get throttle (if armed), as we only care about energy negative throttle also counts */
float throttle = (armed.armed) ? fabsf(actuator_controls.control[3]) : 0.0f;
status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah, throttle);
status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah,
throttle);
}
}
@@ -1372,8 +1407,8 @@ int commander_thread_main(int argc, char *argv[])
last_idle_time = system_load.tasks[0].total_runtime;
/* check if board is connected via USB */
//struct stat statbuf;
//on_usb_power = (stat("/dev/ttyACM0", &statbuf) == 0);
struct stat statbuf;
on_usb_power = (stat("/dev/ttyACM0", &statbuf) == 0);
}
/* if battery voltage is getting lower, warn using buzzer, etc. */
@@ -1383,26 +1418,30 @@ int commander_thread_main(int argc, char *argv[])
status.battery_warning = VEHICLE_BATTERY_WARNING_LOW;
status_changed = true;
} else if (status.condition_battery_voltage_valid && status.battery_remaining < 0.09f && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) {
} else if (!on_usb_power && status.condition_battery_voltage_valid && status.battery_remaining < 0.09f
&& !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) {
/* critical battery voltage, this is rather an emergency, change state machine */
critical_battery_voltage_actions_done = true;
mavlink_log_emergency(mavlink_fd, "CRITICAL BATTERY, LAND IMMEDIATELY");
status.battery_warning = VEHICLE_BATTERY_WARNING_CRITICAL;
if (armed.armed) {
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed, true /* fRunPreArmChecks */, mavlink_fd);
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED_ERROR, &armed, true /* fRunPreArmChecks */,
mavlink_fd);
if (arming_ret == TRANSITION_CHANGED) {
arming_state_changed = true;
}
} else {
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed, true /* fRunPreArmChecks */, mavlink_fd);
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY_ERROR, &armed, true /* fRunPreArmChecks */,
mavlink_fd);
if (arming_ret == TRANSITION_CHANGED) {
arming_state_changed = true;
}
}
status_changed = true;
}
@@ -1411,7 +1450,8 @@ int commander_thread_main(int argc, char *argv[])
/* If in INIT state, try to proceed to STANDBY state */
if (status.arming_state == ARMING_STATE_INIT && low_prio_task == LOW_PRIO_TASK_NONE) {
/* TODO: check for sensors */
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */, mavlink_fd);
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */,
mavlink_fd);
if (arming_ret == TRANSITION_CHANGED) {
arming_state_changed = true;
@@ -1439,23 +1479,25 @@ int commander_thread_main(int argc, char *argv[])
/* Initialize map projection if gps is valid */
if (!map_projection_global_initialized()
&& (gps_position.eph < eph_threshold)
&& (gps_position.epv < epv_threshold)
&& hrt_elapsed_time((hrt_abstime*)&gps_position.timestamp_position) < 1e6) {
&& (gps_position.eph < eph_threshold)
&& (gps_position.epv < epv_threshold)
&& hrt_elapsed_time((hrt_abstime *)&gps_position.timestamp_position) < 1e6) {
/* set reference for global coordinates <--> local coordiantes conversion and map_projection */
globallocalconverter_init((double)gps_position.lat * 1.0e-7, (double)gps_position.lon * 1.0e-7, (float)gps_position.alt * 1.0e-3f, hrt_absolute_time());
globallocalconverter_init((double)gps_position.lat * 1.0e-7, (double)gps_position.lon * 1.0e-7,
(float)gps_position.alt * 1.0e-3f, hrt_absolute_time());
}
/* check if GPS fix is ok */
if (status.circuit_breaker_engaged_gpsfailure_check ||
(gps_position.fix_type >= 3 &&
hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT)) {
(gps_position.fix_type >= 3 &&
hrt_elapsed_time(&gps_position.timestamp_position) < FAILSAFE_DEFAULT_TIMEOUT)) {
/* handle the case where gps was regained */
if (status.gps_failure) {
status.gps_failure = false;
status_changed = true;
mavlink_log_critical(mavlink_fd, "gps regained");
}
} else {
if (!status.gps_failure) {
status.gps_failure = true;
@@ -1477,12 +1519,14 @@ int commander_thread_main(int argc, char *argv[])
armed.force_failsafe = true;
status_changed = true;
static bool flight_termination_printed = false;
if (!flight_termination_printed) {
warnx("Flight termination because of navigator request or geofence");
mavlink_log_critical(mavlink_fd, "GF violation: flight termination");
flight_termination_printed = true;
}
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
mavlink_log_critical(mavlink_fd, "GF violation: flight termination");
}
} // no reset is done here on purpose, on geofence violation we want to stay in flighttermination
@@ -1490,7 +1534,7 @@ int commander_thread_main(int argc, char *argv[])
/* RC input check */
if (!status.rc_input_blocked && sp_man.timestamp != 0 &&
hrt_absolute_time() < sp_man.timestamp + (uint64_t)(rc_loss_timeout * 1e6f)) {
hrt_absolute_time() < sp_man.timestamp + (uint64_t)(rc_loss_timeout * 1e6f)) {
/* handle the case where RC signal was regained */
if (!status.rc_signal_found_once) {
status.rc_signal_found_once = true;
@@ -1515,11 +1559,15 @@ int commander_thread_main(int argc, char *argv[])
if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) {
/* disarm to STANDBY if ARMED or to STANDBY_ERROR if ARMED_ERROR */
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR);
arming_ret = arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */, mavlink_fd);
arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY :
ARMING_STATE_STANDBY_ERROR);
arming_ret = arming_state_transition(&status, &safety, new_arming_state, &armed, true /* fRunPreArmChecks */,
mavlink_fd);
if (arming_ret == TRANSITION_CHANGED) {
arming_state_changed = true;
}
stick_off_counter = 0;
} else {
@@ -1541,8 +1589,11 @@ int commander_thread_main(int argc, char *argv[])
*/
if (status.main_state != MAIN_STATE_MANUAL) {
print_reject_arm("NOT ARMING: Switch to MANUAL mode first.");
} else {
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, true /* fRunPreArmChecks */, mavlink_fd);
arming_ret = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed, true /* fRunPreArmChecks */,
mavlink_fd);
if (arming_ret == TRANSITION_CHANGED) {
arming_state_changed = true;
}
@@ -1565,6 +1616,7 @@ int commander_thread_main(int argc, char *argv[])
} else {
mavlink_log_info(mavlink_fd, "DISARMED by RC");
}
arming_state_changed = true;
} else if (arming_ret == TRANSITION_DENIED) {
@@ -1600,18 +1652,20 @@ int commander_thread_main(int argc, char *argv[])
/* data links check */
bool have_link = false;
for (int i = 0; i < TELEMETRY_STATUS_ORB_ID_NUM; i++) {
if (telemetry_last_heartbeat[i] != 0 &&
hrt_elapsed_time(&telemetry_last_heartbeat[i]) < datalink_loss_timeout * 1e6) {
hrt_elapsed_time(&telemetry_last_heartbeat[i]) < datalink_loss_timeout * 1e6) {
/* handle the case where data link was regained,
* accept datalink as healthy only after datalink_regain_timeout seconds
* */
if (telemetry_lost[i] &&
hrt_elapsed_time(&telemetry_last_dl_loss[i]) > datalink_regain_timeout * 1e6) {
hrt_elapsed_time(&telemetry_last_dl_loss[i]) > datalink_regain_timeout * 1e6) {
mavlink_log_critical(mavlink_fd, "data link %i regained", i);
telemetry_lost[i] = false;
have_link = true;
} else if (!telemetry_lost[i]) {
/* telemetry was healthy also in last iteration
* we don't have to check a timeout */
@@ -1620,6 +1674,7 @@ int commander_thread_main(int argc, char *argv[])
} else {
telemetry_last_dl_loss[i] = hrt_absolute_time();
if (!telemetry_lost[i]) {
mavlink_log_critical(mavlink_fd, "data link %i lost", i);
telemetry_lost[i] = true;
@@ -1647,24 +1702,26 @@ int commander_thread_main(int argc, char *argv[])
* only for fixed wing for now
*/
if (!status.circuit_breaker_engaged_enginefailure_check &&
status.is_rotary_wing == false &&
armed.armed &&
((actuator_controls.control[3] > ef_throttle_thres &&
battery.current_a/actuator_controls.control[3] <
ef_current2throttle_thres) ||
(status.engine_failure))) {
status.is_rotary_wing == false &&
armed.armed &&
((actuator_controls.control[3] > ef_throttle_thres &&
battery.current_a / actuator_controls.control[3] <
ef_current2throttle_thres) ||
(status.engine_failure))) {
/* potential failure, measure time */
if (timestamp_engine_healthy > 0 &&
hrt_elapsed_time(&timestamp_engine_healthy) >
ef_time_thres * 1e6 &&
!status.engine_failure) {
status.engine_failure = true;
status_changed = true;
mavlink_log_critical(mavlink_fd, "Engine Failure");
hrt_elapsed_time(&timestamp_engine_healthy) >
ef_time_thres * 1e6 &&
!status.engine_failure) {
status.engine_failure = true;
status_changed = true;
mavlink_log_critical(mavlink_fd, "Engine Failure");
}
} else {
/* no failure reset flag */
timestamp_engine_healthy = hrt_absolute_time();
if (status.engine_failure) {
status.engine_failure = false;
status_changed = true;
@@ -1691,20 +1748,22 @@ int commander_thread_main(int argc, char *argv[])
* If we are not in a manual (RC stick controlled mode)
* and both failed we want to terminate the flight */
if (status.main_state != MAIN_STATE_MANUAL &&
status.main_state != MAIN_STATE_ACRO &&
status.main_state != MAIN_STATE_ALTCTL &&
status.main_state != MAIN_STATE_POSCTL &&
((status.data_link_lost && status.gps_failure) ||
(status.data_link_lost_cmd && status.gps_failure_cmd))) {
status.main_state != MAIN_STATE_ACRO &&
status.main_state != MAIN_STATE_ALTCTL &&
status.main_state != MAIN_STATE_POSCTL &&
((status.data_link_lost && status.gps_failure) ||
(status.data_link_lost_cmd && status.gps_failure_cmd))) {
armed.force_failsafe = true;
status_changed = true;
static bool flight_termination_printed = false;
if (!flight_termination_printed) {
warnx("Flight termination because of data link loss && gps failure");
mavlink_log_critical(mavlink_fd, "DL and GPS lost: flight termination");
flight_termination_printed = true;
}
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
mavlink_log_critical(mavlink_fd, "DL and GPS lost: flight termination");
}
}
@@ -1713,19 +1772,21 @@ int commander_thread_main(int argc, char *argv[])
* If we are in manual (controlled with RC):
* if both failed we want to terminate the flight */
if ((status.main_state == MAIN_STATE_ACRO ||
status.main_state == MAIN_STATE_MANUAL ||
status.main_state == MAIN_STATE_ALTCTL ||
status.main_state == MAIN_STATE_POSCTL) &&
((status.rc_signal_lost && status.gps_failure) ||
(status.rc_signal_lost_cmd && status.gps_failure_cmd))) {
status.main_state == MAIN_STATE_MANUAL ||
status.main_state == MAIN_STATE_ALTCTL ||
status.main_state == MAIN_STATE_POSCTL) &&
((status.rc_signal_lost && status.gps_failure) ||
(status.rc_signal_lost_cmd && status.gps_failure_cmd))) {
armed.force_failsafe = true;
status_changed = true;
static bool flight_termination_printed = false;
if (!flight_termination_printed) {
warnx("Flight termination because of RC signal loss && gps failure");
flight_termination_printed = true;
}
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 ) {
if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) {
mavlink_log_critical(mavlink_fd, "RC and GPS lost: flight termination");
}
}
@@ -1766,6 +1827,7 @@ int commander_thread_main(int argc, char *argv[])
/* mark home position as set */
status.condition_home_position_valid = true;
}
arming_state_changed = false;
}
@@ -1810,7 +1872,8 @@ int commander_thread_main(int argc, char *argv[])
}
/* play arming and battery warning tunes */
if (!arm_tune_played && armed.armed && (!safety.safety_switch_available || (safety.safety_switch_available && safety.safety_off))) {
if (!arm_tune_played && armed.armed && (!safety.safety_switch_available || (safety.safety_switch_available
&& safety.safety_off))) {
/* play tune when armed */
set_tune(TONE_ARMING_WARNING_TUNE);
arm_tune_played = true;
@@ -1988,6 +2051,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
/* offboard switch overrides main switch */
if (sp_man->offboard_switch == SWITCH_POS_ON) {
res = main_state_transition(status_local, MAIN_STATE_OFFBOARD);
if (res == TRANSITION_DENIED) {
print_reject_mode(status_local, "OFFBOARD");
@@ -2009,6 +2073,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
} else {
res = main_state_transition(status_local, MAIN_STATE_MANUAL);
}
// TRANSITION_DENIED is not possible here
break;
@@ -2023,7 +2088,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
print_reject_mode(status_local, "POSCTL");
}
// fallback to ALTCTL
// fallback to ALTCTL
res = main_state_transition(status_local, MAIN_STATE_ALTCTL);
if (res != TRANSITION_DENIED) {
@@ -2047,14 +2112,14 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
break; // changed successfully or already in this state
}
print_reject_mode(status_local, "AUTO_RTL");
print_reject_mode(status_local, "AUTO_RTL");
// fallback to LOITER if home position not set
res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
// fallback to LOITER if home position not set
res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
} else if (sp_man->loiter_switch == SWITCH_POS_ON) {
res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
@@ -2063,7 +2128,7 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
break; // changed successfully or already in this state
}
print_reject_mode(status_local, "AUTO_LOITER");
print_reject_mode(status_local, "AUTO_LOITER");
} else {
res = main_state_transition(status_local, MAIN_STATE_AUTO_MISSION);
@@ -2072,22 +2137,22 @@ set_main_state_rc(struct vehicle_status_s *status_local, struct manual_control_s
break; // changed successfully or already in this state
}
print_reject_mode(status_local, "AUTO_MISSION");
print_reject_mode(status_local, "AUTO_MISSION");
// fallback to LOITER if home position not set
res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
// fallback to LOITER if home position not set
res = main_state_transition(status_local, MAIN_STATE_AUTO_LOITER);
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
}
// fallback to POSCTL
res = main_state_transition(status_local, MAIN_STATE_POSCTL);
// fallback to POSCTL
res = main_state_transition(status_local, MAIN_STATE_POSCTL);
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
if (res != TRANSITION_DENIED) {
break; // changed successfully or already in this state
}
// fallback to ALTCTL
res = main_state_transition(status_local, MAIN_STATE_ALTCTL);
@@ -2169,6 +2234,7 @@ set_control_mode()
control_mode.flag_control_position_enabled = false;
control_mode.flag_control_velocity_enabled = false;
break;
case OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE:
control_mode.flag_control_rates_enabled = true;
control_mode.flag_control_attitude_enabled = true;
@@ -2177,6 +2243,7 @@ set_control_mode()
control_mode.flag_control_position_enabled = false;
control_mode.flag_control_velocity_enabled = false;
break;
case OFFBOARD_CONTROL_MODE_DIRECT_FORCE:
control_mode.flag_control_rates_enabled = true;
control_mode.flag_control_attitude_enabled = false;
@@ -2186,6 +2253,7 @@ set_control_mode()
control_mode.flag_control_position_enabled = false;
control_mode.flag_control_velocity_enabled = false;
break;
case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_NED:
case OFFBOARD_CONTROL_MODE_DIRECT_LOCAL_OFFSET_NED:
case OFFBOARD_CONTROL_MODE_DIRECT_BODY_NED:
@@ -2198,6 +2266,7 @@ set_control_mode()
control_mode.flag_control_velocity_enabled = true;
//XXX: the flags could depend on sp_offboard.ignore
break;
default:
control_mode.flag_control_rates_enabled = false;
control_mode.flag_control_attitude_enabled = false;
@@ -2206,6 +2275,7 @@ set_control_mode()
control_mode.flag_control_position_enabled = false;
control_mode.flag_control_velocity_enabled = false;
}
break;
case NAVIGATION_STATE_POSCTL:
@@ -2415,7 +2485,8 @@ void *commander_low_prio_loop(void *arg)
int calib_ret = ERROR;
/* try to go to INIT/PREFLIGHT arming state */
if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed, true /* fRunPreArmChecks */, mavlink_fd)) {
if (TRANSITION_DENIED == arming_state_transition(&status, &safety, ARMING_STATE_INIT, &armed,
true /* fRunPreArmChecks */, mavlink_fd)) {
answer_command(cmd, VEHICLE_CMD_RESULT_DENIED);
break;
}
+4 -1
View File
@@ -63,7 +63,10 @@ static const char *sensor_name = "gyro";
int do_gyro_calibration(int mavlink_fd)
{
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
mavlink_log_info(mavlink_fd, "don't move system");
mavlink_log_info(mavlink_fd, "HOLD STILL");
/* wait for the user to respond */
sleep(2);
struct gyro_scale gyro_scale = {
0.0f,
+1 -1
View File
@@ -155,7 +155,7 @@ int do_mag_calibration(int mavlink_fd)
uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval;
unsigned poll_errcount = 0;
mavlink_log_info(mavlink_fd, "rotate in a figure 8 around all axis");
mavlink_log_info(mavlink_fd, "Turn on all sides: front/back,left/right,up/down");
calibration_counter = 0;
@@ -597,12 +597,12 @@ FixedwingEstimator::check_filter_state()
const char* const feedback[] = { 0,
"NaN in states, resetting",
"stale IMU data, resetting",
"stale sensor data, resetting",
"got initial position lock",
"excessive gyro offsets",
"GPS velocity divergence",
"velocity diverted, check accel config",
"excessive covariances",
"unknown condition"};
"unknown condition, resetting"};
// Print out error condition
if (check) {
@@ -614,7 +614,7 @@ FixedwingEstimator::check_filter_state()
}
warnx("reset: %s", feedback[warn_index]);
mavlink_log_critical(_mavlink_fd, "[ekf] re-init: %s", feedback[warn_index]);
mavlink_log_critical(_mavlink_fd, "[ekf check] %s", feedback[warn_index]);
}
struct estimator_status_report rep;
+2 -2
View File
@@ -763,7 +763,7 @@ Mavlink::send_message(const uint8_t msgid, const void *msg)
_last_write_try_time = hrt_absolute_time();
/* check if there is space in the buffer, let it overflow else */
if (buf_free < TX_BUFFER_GAP) {
if ((buf_free < TX_BUFFER_GAP) || (buf_free < packet_len)) {
/* no enough space in buffer to send */
count_txerr();
count_txerrbytes(packet_len);
@@ -1634,7 +1634,7 @@ Mavlink::start(int argc, char *argv[])
task_spawn_cmd(buf,
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT,
2700,
2900,
(main_t)&Mavlink::start_helper,
(const char **)argv);
+32
View File
@@ -341,11 +341,18 @@ private:
/* do not allow top copying this class */
MavlinkStreamStatustext(MavlinkStreamStatustext &);
MavlinkStreamStatustext& operator = (const MavlinkStreamStatustext &);
FILE *fp = nullptr;
protected:
explicit MavlinkStreamStatustext(Mavlink *mavlink) : MavlinkStream(mavlink)
{}
~MavlinkStreamStatustext() {
if (fp) {
fclose(fp);
}
}
void send(const hrt_abstime t)
{
if (!mavlink_logbuffer_is_empty(_mavlink->get_logbuffer())) {
@@ -359,6 +366,31 @@ protected:
strncpy(msg.text, logmsg.text, sizeof(msg.text));
_mavlink->send_message(MAVLINK_MSG_ID_STATUSTEXT, &msg);
/* write log messages in first instance to disk */
if (_mavlink->get_instance_id() == 0) {
if (fp) {
fputs(msg.text, fp);
fputs("\n", fp);
fsync(fileno(fp));
} else {
/* string to hold the path to the log */
char log_file_name[32] = "";
char log_file_path[64] = "";
timespec ts;
clock_gettime(CLOCK_REALTIME, &ts);
/* use GPS time for log file naming, e.g. /fs/microsd/2014-01-19/19_37_52.bin */
time_t gps_time_sec = ts.tv_sec + (ts.tv_nsec / 1e9);
struct tm t;
gmtime_r(&gps_time_sec, &t);
// XXX we do not want to interfere here with the SD log app
strftime(log_file_name, sizeof(log_file_name), "msgs_%Y_%m_%d_%H_%M_%S.txt", &t);
snprintf(log_file_path, sizeof(log_file_path), "/fs/microsd/%s", log_file_name);
fp = fopen(log_file_path, "ab");
}
}
}
}
}
+5 -7
View File
@@ -391,11 +391,9 @@ MavlinkReceiver::handle_message_hil_optical_flow(mavlink_message_t *msg)
f.timestamp = hrt_absolute_time();
f.flow_timestamp = flow.time_usec;
f.flow_raw_x = flow.flow_x;
f.flow_raw_y = flow.flow_y;
f.flow_comp_x_m = flow.flow_comp_m_x;
f.flow_comp_y_m = flow.flow_comp_m_y;
f.ground_distance_m = flow.ground_distance;
f.flow_raw_x = flow.integrated_x;
f.flow_raw_y = flow.integrated_y;
f.ground_distance_m = flow.distance;
f.quality = flow.quality;
f.sensor_id = flow.sensor_id;
@@ -413,7 +411,7 @@ MavlinkReceiver::handle_message_hil_optical_flow(mavlink_message_t *msg)
r.timestamp = hrt_absolute_time();
r.error_count = 0;
r.type = RANGE_FINDER_TYPE_LASER;
r.distance = flow.ground_distance;
r.distance = flow.distance;
r.minimum_distance = 0.0f;
r.maximum_distance = 40.0f; // this is set to match the typical range of real sensors, could be made configurable
r.valid = (r.distance > r.minimum_distance) && (r.distance < r.maximum_distance);
@@ -1398,7 +1396,7 @@ MavlinkReceiver::receive_start(Mavlink *parent)
struct sched_param param;
(void)pthread_attr_getschedparam(&receiveloop_attr, &param);
param.sched_priority = SCHED_PRIORITY_MAX - 40;
param.sched_priority = SCHED_PRIORITY_MAX - 80;
(void)pthread_attr_setschedparam(&receiveloop_attr, &param);
pthread_attr_setstacksize(&receiveloop_attr, 2900);
+6 -1
View File
@@ -60,6 +60,8 @@ static perf_counter_t c_gather_ppm;
static int _dsm_fd;
static uint16_t rc_value_override = 0;
bool dsm_port_input(uint16_t *rssi, bool *dsm_updated, bool *st24_updated)
{
perf_begin(c_gather_dsm);
@@ -316,6 +318,9 @@ controls_tick() {
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
} else if (mapped == PX4IO_P_RC_CONFIG_ASSIGNMENT_MODESWITCH) {
/* pick out override channel, indicated by special mapping */
rc_value_override = SIGNED_TO_REG(scaled);
}
}
}
@@ -409,7 +414,7 @@ controls_tick() {
* requested override.
*
*/
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && (REG_TO_SIGNED(r_rc_values[4]) < RC_CHANNEL_LOW_THRESH))
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && (REG_TO_SIGNED(rc_value_override) < RC_CHANNEL_LOW_THRESH))
override = true;
if (override) {
-7
View File
@@ -60,13 +60,6 @@ extern "C" {
*/
#define FMU_INPUT_DROP_LIMIT_US 500000
/* XXX need to move the RC_CHANNEL_FUNCTION out of rc_channels.h and into systemlib */
#define ROLL 0
#define PITCH 1
#define YAW 2
#define THROTTLE 3
#define OVERRIDE 4
/* current servo arm/disarm state */
static bool mixer_servos_armed = false;
static bool should_arm = false;
+2
View File
@@ -221,6 +221,7 @@ enum { /* DSM bind states */
hence index 12 can safely be used. */
#define PX4IO_P_SETUP_RC_THR_FAILSAFE_US 13 /**< the throttle failsafe pulse length in microseconds */
#define PX4IO_P_SETUP_FORCE_SAFETY_ON 14 /* force safety switch into 'disarmed' (PWM disabled state) */
#define PX4IO_FORCE_SAFETY_MAGIC 22027 /* required argument for force safety (random) */
/* autopilot control values, -10000..10000 */
@@ -246,6 +247,7 @@ enum { /* DSM bind states */
#define PX4IO_P_RC_CONFIG_MAX 2 /**< highest input value */
#define PX4IO_P_RC_CONFIG_DEADZONE 3 /**< band around center that is ignored */
#define PX4IO_P_RC_CONFIG_ASSIGNMENT 4 /**< mapped input value */
#define PX4IO_P_RC_CONFIG_ASSIGNMENT_MODESWITCH 100 /**< magic value for mode switch */
#define PX4IO_P_RC_CONFIG_OPTIONS 5 /**< channel options bitmask */
#define PX4IO_P_RC_CONFIG_OPTIONS_ENABLED (1 << 0)
#define PX4IO_P_RC_CONFIG_OPTIONS_REVERSE (1 << 1)
+6
View File
@@ -124,6 +124,9 @@ heartbeat_blink(void)
{
static bool heartbeat = false;
LED_BLUE(heartbeat = !heartbeat);
#ifdef GPIO_LED4
LED_RING(heartbeat);
#endif
}
static uint64_t reboot_time;
@@ -191,6 +194,9 @@ user_start(int argc, char *argv[])
LED_AMBER(false);
LED_BLUE(false);
LED_SAFETY(false);
#ifdef GPIO_LED4
LED_RING(false);
#endif
/* turn on servo power (if supported) */
#ifdef POWER_SERVO
+1
View File
@@ -140,6 +140,7 @@ extern pwm_limit_t pwm_limit;
#define LED_BLUE(_s) stm32_gpiowrite(GPIO_LED1, !(_s))
#define LED_AMBER(_s) stm32_gpiowrite(GPIO_LED2, !(_s))
#define LED_SAFETY(_s) stm32_gpiowrite(GPIO_LED3, !(_s))
#define LED_RING(_s) stm32_gpiowrite(GPIO_LED4, !(_s))
#ifdef CONFIG_ARCH_BOARD_PX4IO_V1
+8 -1
View File
@@ -603,6 +603,12 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
dsm_bind(value & 0x0f, (value >> 4) & 0xF);
break;
case PX4IO_P_SETUP_FORCE_SAFETY_ON:
if (value == PX4IO_FORCE_SAFETY_MAGIC) {
r_status_flags &= ~PX4IO_P_STATUS_FLAGS_SAFETY_OFF;
}
break;
case PX4IO_P_SETUP_FORCE_SAFETY_OFF:
if (value == PX4IO_FORCE_SAFETY_MAGIC) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_SAFETY_OFF;
@@ -686,7 +692,8 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
if (conf[PX4IO_P_RC_CONFIG_ASSIGNMENT] == UINT8_MAX) {
disabled = true;
} else if (conf[PX4IO_P_RC_CONFIG_ASSIGNMENT] >= PX4IO_RC_MAPPED_CONTROL_CHANNELS) {
} else if ((conf[PX4IO_P_RC_CONFIG_ASSIGNMENT] >= PX4IO_RC_MAPPED_CONTROL_CHANNELS) &&
(conf[PX4IO_P_RC_CONFIG_ASSIGNMENT] != PX4IO_P_RC_CONFIG_ASSIGNMENT_MODESWITCH)) {
count++;
}
+33 -22
View File
@@ -61,7 +61,7 @@
/*
Measured values with Futaba FX-30/R6108SB:
-+100% on TX: PCM 1.100/1.520/1.950ms -> SBus raw values: 350/1024/1700 (100% ATV)
-+140% on TX: PCM 0.930/1.520/2.112ms -> SBus raw values: 78/1024/1964 (140% ATV)
-+140% on TX: PCM 0.930/1.520/2.112ms -> SBus raw values: 78/1024/1964 (140% ATV)
-+152% on TX: PCM 0.884/1.520/2.160ms -> SBus raw values: 1/1024/2047 (140% ATV plus dirty tricks)
*/
@@ -87,13 +87,15 @@ static unsigned partial_frame_count;
unsigned sbus_frame_drops;
static bool sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels);
static bool sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe,
bool *sbus_frame_drop, uint16_t max_channels);
int
sbus_init(const char *device)
{
if (sbus_fd < 0)
if (sbus_fd < 0) {
sbus_fd = open(device, O_RDWR | O_NONBLOCK);
}
if (sbus_fd >= 0) {
struct termios t;
@@ -113,6 +115,7 @@ sbus_init(const char *device)
} else {
debug("S.Bus: open failed");
}
return sbus_fd;
}
@@ -167,8 +170,9 @@ sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sb
ret = read(sbus_fd, &frame[partial_frame_count], SBUS_FRAME_SIZE - partial_frame_count);
/* if the read failed for any reason, just give up here */
if (ret < 1)
if (ret < 1) {
return false;
}
last_rx_time = now;
@@ -180,8 +184,9 @@ sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sb
/*
* If we don't have a full frame, return
*/
if (partial_frame_count < SBUS_FRAME_SIZE)
if (partial_frame_count < SBUS_FRAME_SIZE) {
return false;
}
/*
* Great, it looks like we might have a frame. Go ahead and
@@ -228,7 +233,8 @@ static const struct sbus_bit_pick sbus_decoder[SBUS_INPUT_CHANNELS][3] = {
};
static bool
sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_values)
sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop,
uint16_t max_values)
{
/* check frame boundary markers to avoid out-of-sync cases */
if ((frame[0] != 0x0f)) {
@@ -237,23 +243,27 @@ sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool
}
switch (frame[24]) {
case 0x00:
case 0x00:
/* this is S.BUS 1 */
break;
case 0x03:
case 0x03:
/* S.BUS 2 SLOT0: RX battery and external voltage */
break;
case 0x83:
case 0x83:
/* S.BUS 2 SLOT1 */
break;
case 0x43:
case 0xC3:
case 0x23:
case 0xA3:
case 0x63:
case 0xE3:
case 0x43:
case 0xC3:
case 0x23:
case 0xA3:
case 0x63:
case 0xE3:
break;
default:
default:
/* we expect one of the bits above, but there are some we don't know yet */
break;
}
@@ -283,7 +293,7 @@ sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool
/* convert 0-2048 values to 1000-2000 ppm encoding in a not too sloppy fashion */
values[channel] = (uint16_t)(value * SBUS_SCALE_FACTOR +.5f) + SBUS_SCALE_OFFSET;
values[channel] = (uint16_t)(value * SBUS_SCALE_FACTOR + .5f) + SBUS_SCALE_OFFSET;
}
/* decode switch channels if data fields are wide enough */
@@ -304,16 +314,17 @@ sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool
/* report that we failed to read anything valid off the receiver */
*sbus_failsafe = true;
*sbus_frame_drop = true;
}
else if (frame[SBUS_FLAGS_BYTE] & (1 << SBUS_FRAMELOST_BIT)) { /* a frame was lost */
} else if (frame[SBUS_FLAGS_BYTE] & (1 << SBUS_FRAMELOST_BIT)) { /* a frame was lost */
/* set a special warning flag
*
* Attention! This flag indicates a skipped frame only, not a total link loss! Handling this
* condition as fail-safe greatly reduces the reliability and range of the radio link,
*
* Attention! This flag indicates a skipped frame only, not a total link loss! Handling this
* condition as fail-safe greatly reduces the reliability and range of the radio link,
* e.g. by prematurely issueing return-to-launch!!! */
*sbus_failsafe = false;
*sbus_frame_drop = true;
} else {
*sbus_failsafe = false;
*sbus_frame_drop = false;
+36 -4
View File
@@ -90,6 +90,7 @@
#include <uORB/topics/system_power.h>
#include <uORB/topics/servorail_status.h>
#include <uORB/topics/wind_estimate.h>
#include <uORB/topics/encoders.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
@@ -628,6 +629,9 @@ void sdlog2_start_log()
perf_print_all(perf_fd);
close(perf_fd);
/* reset performance counters to get in-flight min and max values in post flight log */
perf_reset_all();
logging_enabled = true;
}
@@ -951,6 +955,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct servorail_status_s servorail_status;
struct satellite_info_s sat_info;
struct wind_estimate_s wind_estimate;
struct encoders_s encoders;
} buf;
memset(&buf, 0, sizeof(buf));
@@ -993,6 +998,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct log_GS1B_s log_GS1B;
struct log_TECS_s log_TECS;
struct log_WIND_s log_WIND;
struct log_ENCD_s log_ENCD;
} body;
} log_msg = {
LOG_PACKET_HEADER_INIT(0)
@@ -1030,12 +1036,12 @@ int sdlog2_thread_main(int argc, char *argv[])
int system_power_sub;
int servorail_status_sub;
int wind_sub;
int encoders_sub;
} subs;
subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command));
subs.status_sub = orb_subscribe(ORB_ID(vehicle_status));
subs.gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
subs.sat_info_sub = orb_subscribe(ORB_ID(satellite_info));
subs.sensor_sub = orb_subscribe(ORB_ID(sensor_combined));
subs.att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
subs.att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
@@ -1054,9 +1060,6 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.esc_sub = orb_subscribe(ORB_ID(esc_status));
subs.global_vel_sp_sub = orb_subscribe(ORB_ID(vehicle_global_velocity_setpoint));
subs.battery_sub = orb_subscribe(ORB_ID(battery_status));
for (int i = 0; i < TELEMETRY_STATUS_ORB_ID_NUM; i++) {
subs.telemetry_subs[i] = orb_subscribe(telemetry_status_orb_id[i]);
}
subs.range_finder_sub = orb_subscribe(ORB_ID(sensor_range_finder));
subs.estimator_status_sub = orb_subscribe(ORB_ID(estimator_status));
subs.tecs_status_sub = orb_subscribe(ORB_ID(tecs_status));
@@ -1065,6 +1068,25 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.wind_sub = orb_subscribe(ORB_ID(wind_estimate));
/* we need to rate-limit wind, as we do not need the full update rate */
orb_set_interval(subs.wind_sub, 90);
subs.encoders_sub = orb_subscribe(ORB_ID(encoders));
/* add new topics HERE */
for (int i = 0; i < TELEMETRY_STATUS_ORB_ID_NUM; i++) {
subs.telemetry_subs[i] = orb_subscribe(telemetry_status_orb_id[i]);
}
if (_extended_logging) {
subs.sat_info_sub = orb_subscribe(ORB_ID(satellite_info));
}
/* close non-needed fd's */
/* close stdin */
close(0);
/* close stdout */
close(1);
thread_running = true;
@@ -1649,6 +1671,16 @@ int sdlog2_thread_main(int argc, char *argv[])
LOGBUFFER_WRITE_AND_COUNT(WIND);
}
/* --- ENCODERS --- */
if (copy_if_updated(ORB_ID(encoders), subs.encoders_sub, &buf.encoders)) {
log_msg.msg_type = LOG_ENCD_MSG;
log_msg.body.log_ENCD.cnt0 = buf.encoders.counts[0];
log_msg.body.log_ENCD.vel0 = buf.encoders.velocity[0];
log_msg.body.log_ENCD.cnt1 = buf.encoders.counts[1];
log_msg.body.log_ENCD.vel1 = buf.encoders.velocity[1];
LOGBUFFER_WRITE_AND_COUNT(ENCD);
}
/* signal the other thread new data, but not yet unlock */
if (logbuffer_count(&lb) > MIN_BYTES_TO_WRITE) {
/* only request write if several packets can be written at once */
+11
View File
@@ -407,6 +407,16 @@ struct log_VISN_s {
float qw;
};
/* --- ENCODERS - ENCODER DATA --- */
#define LOG_ENCD_MSG 39
struct log_ENCD_s {
int64_t cnt0;
float vel0;
int64_t cnt1;
float vel1;
};
/********** SYSTEM MESSAGES, ID > 0x80 **********/
/* --- TIME - TIME STAMP --- */
@@ -471,6 +481,7 @@ static const struct log_format_s log_formats[] = {
LOG_FORMAT(GS1B, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"),
LOG_FORMAT(TECS, "fffffffffffffB", "ASP,AF,FSP,F,FF,AsSP,AsF,AsDSP,AsD,TERSP,TER,EDRSP,EDR,M"),
LOG_FORMAT(WIND, "ffff", "X,Y,CovX,CovY"),
LOG_FORMAT(ENCD, "qfqf", "cnt0,vel0,cnt1,vel1"),
/* system-level messages, ID >= 0x80 */
/* FMT: don't write format of format message, it's useless */
+3
View File
@@ -201,6 +201,9 @@ ORB_DEFINE(telemetry_status_1, struct telemetry_status_s);
ORB_DEFINE(telemetry_status_2, struct telemetry_status_s);
ORB_DEFINE(telemetry_status_3, struct telemetry_status_s);
#include "topics/test_motor.h"
ORB_DEFINE(test_motor, struct test_motor_s);
#include "topics/debug_key_value.h"
ORB_DEFINE(debug_key_value, struct debug_key_value_s);
+7 -3
View File
@@ -34,6 +34,8 @@
/**
* @file rc_channels.h
* Definition of the rc_channels uORB topic.
*
* @deprecated DO NOT USE FOR NEW CODE
*/
#ifndef RC_CHANNELS_H_
@@ -63,10 +65,13 @@ enum RC_CHANNELS_FUNCTION {
AUX_2,
AUX_3,
AUX_4,
AUX_5,
RC_CHANNELS_FUNCTION_MAX /**< Indicates the number of functions. There can be more functions than RC channels. */
AUX_5
};
// MAXIMUM FUNCTIONS IS != MAXIMUM RC INPUT CHANNELS
#define RC_CHANNELS_FUNCTION_MAX 18
/**
* @addtogroup topics
* @{
@@ -76,7 +81,6 @@ struct rc_channels_s {
uint64_t timestamp_last_valid; /**< Timestamp of last valid RC signal */
float channels[RC_CHANNELS_FUNCTION_MAX]; /**< Scaled to -1..1 (throttle: 0..1) */
uint8_t channel_count; /**< Number of valid channels */
char function_name[RC_CHANNELS_FUNCTION_MAX][20]; /**< String array to store the names of the functions */
int8_t function[RC_CHANNELS_FUNCTION_MAX]; /**< Functions mapping */
uint8_t rssi; /**< Receive signal strength index */
bool signal_lost; /**< Control signal lost, should be checked together with topic timeout */
+70
View File
@@ -0,0 +1,70 @@
/****************************************************************************
*
* Copyright (C) 2014 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 test_motor.h
*
* Test a single drive motor while the vehicle is disarmed
*
* Publishing values to this topic causes a single motor to spin, e.g. for
* ground test purposes. This topic will be ignored while the vehicle is armed.
*
*/
#ifndef TOPIC_TEST_MOTOR_H
#define TOPIC_TEST_MOTOR_H
#include <stdint.h>
#include "../uORB.h"
#define NUM_MOTOR_OUTPUTS 8
/**
* @addtogroup topics
* @{
*/
struct test_motor_s {
uint64_t timestamp; /**< output timestamp in us since system boot */
unsigned motor_number; /**< number of motor to spin */
float value; /**< output data, in natural output units */
};
/**
* @}
*/
/* actuator output sets; this list can be expanded as more drivers emerge */
ORB_DECLARE(test_motor);
#endif
+41
View File
@@ -0,0 +1,41 @@
############################################################################
#
# Copyright (c) 2014 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.
#
############################################################################
#
# Build the motor_test tool.
#
MODULE_COMMAND = motor_test
SRCS = motor_test.c
MODULE_STACKSIZE = 4096
+128
View File
@@ -0,0 +1,128 @@
/****************************************************************************
*
* Copyright (C) 2014 PX4 Development Team. All rights reserved.
* Author: Holger Steinhaus <hsteinhaus@gmx.de>
*
* 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 motor_test.c
*
* Tool for drive testing
*/
#include <nuttx/config.h>
#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include <unistd.h>
#include <arch/board/board.h>
#include <drivers/drv_hrt.h>
#include <uORB/topics/test_motor.h>
#include "systemlib/systemlib.h"
#include "systemlib/err.h"
__EXPORT int motor_test_main(int argc, char *argv[]);
static void motor_test(unsigned channel, float value);
static void usage(const char *reason);
void motor_test(unsigned channel, float value)
{
orb_advert_t _test_motor_pub;
struct test_motor_s _test_motor;
_test_motor.motor_number = channel;
_test_motor.timestamp = hrt_absolute_time();
_test_motor.value = value;
if (_test_motor_pub > 0) {
/* publish armed state */
orb_publish(ORB_ID(test_motor), _test_motor_pub, &_test_motor);
} else {
/* advertise and publish */
_test_motor_pub = orb_advertise(ORB_ID(test_motor), &_test_motor);
}
}
static void usage(const char *reason)
{
if (reason != NULL)
warnx("%s", reason);
errx(1,
"usage:\n"
"motor_test\n"
" -m <channel> Motor to test (0..7)\n"
" -p <power> Power (0..100)\n");
}
int motor_test_main(int argc, char *argv[])
{
unsigned long channel, lval;
float value;
int ch;
if (argc != 5) {
usage("please specify motor and power");
}
while ((ch = getopt(argc, argv, "m:p:")) != EOF) {
switch (ch) {
case 'm':
/* Read in channels supplied as one int and convert to mask: 1234 -> 0xF */
channel = strtoul(optarg, NULL, 0);
break;
case 'p':
/* Read in custom low value */
lval = strtoul(optarg, NULL, 0);
if (lval > 100)
usage("value invalid");
value = (float)lval/100.f;
break;
default:
usage(NULL);
}
}
motor_test(channel, value);
printf("motor %d set to %.2f\n", channel, value);
exit(0);
}
+3 -1
View File
@@ -38,6 +38,8 @@
MODULE_COMMAND = nshterm
SRCS = nshterm.c
MODULE_STACKSIZE = 1400
MODULE_STACKSIZE = 1600
MAXOPTIMIZATION = -Os
MODULE_PRIORITY = "SCHED_PRIORITY_DEFAULT-30"
+2 -2
View File
@@ -87,7 +87,7 @@ nshterm_main(int argc, char *argv[])
/* Back up the original uart configuration to restore it after exit */
if ((termios_state = tcgetattr(fd, &uart_config)) < 0) {
warnx("ERROR get termios config %s: %d\n", argv[1], termios_state);
warnx("ERR get config %s: %d\n", argv[1], termios_state);
close(fd);
return -1;
}
@@ -96,7 +96,7 @@ nshterm_main(int argc, char *argv[])
uart_config.c_oflag |= (ONLCR | OPOST/* | OCRNL*/);
if ((termios_state = tcsetattr(fd, TCSANOW, &uart_config)) < 0) {
warnx("ERROR setting baudrate / termios config for %s (tcsetattr)\n", argv[1]);
warnx("ERR set config %s\n", argv[1]);
close(fd);
return -1;
}
+2
View File
@@ -110,7 +110,9 @@ const struct {
{"conv", test_conv, OPT_NOJIGTEST | OPT_NOALLTEST},
{"mount", test_mount, OPT_NOJIGTEST | OPT_NOALLTEST},
{"mtd", test_mtd, 0},
#ifndef TESTS_MATHLIB_DISABLE
{"mathlib", test_mathlib, 0},
#endif
{"help", test_help, OPT_NOALLTEST | OPT_NOHELP | OPT_NOJIGTEST},
{NULL, NULL, 0}
};