This commit is contained in:
Julian Oes
2012-11-05 16:22:21 -08:00
20 changed files with 668 additions and 184 deletions
+18 -4
View File
@@ -57,15 +57,23 @@
#define RC_INPUT_DEVICE_PATH "/dev/input_rc"
/**
* Maximum number of R/C input channels in the system.
* Maximum number of R/C input channels in the system. S.Bus has up to 18 channels.
*/
#define RC_INPUT_MAX_CHANNELS 16
#define RC_INPUT_MAX_CHANNELS 18
/**
* Input signal type, value is a control position from zero to 100
* percent.
*/
typedef uint8_t rc_input_t;
typedef uint16_t rc_input_t;
enum RC_INPUT_SOURCE {
RC_INPUT_SOURCE_UNKNOWN = 0,
RC_INPUT_SOURCE_PX4FMU_PPM,
RC_INPUT_SOURCE_PX4IO_PPM,
RC_INPUT_SOURCE_PX4IO_SPEKTRUM,
RC_INPUT_SOURCE_PX4IO_SBUS
};
/**
* R/C input status structure.
@@ -74,10 +82,16 @@ typedef uint8_t rc_input_t;
* on the board involved.
*/
struct rc_input_values {
/** decoding time */
uint64_t timestamp;
/** number of channels actually being seen */
uint32_t channel_count;
/** desired pulse widths for each of the supported channels */
/** Input source */
enum RC_INPUT_SOURCE input_source;
/** measured pulse widths for each of the supported channels */
rc_input_t values[RC_INPUT_MAX_CHANNELS];
};
+81 -7
View File
@@ -61,9 +61,10 @@
#include <drivers/device/device.h>
#include <drivers/drv_rc_input.h>
#include <drivers/drv_pwm_output.h>
#include <systemlib/mixer/mixer.h>
#include <drivers/drv_hrt.h>
#include <drivers/drv_mixer.h>
#include <systemlib/mixer/mixer.h>
#include <systemlib/perf_counter.h>
#include <systemlib/hx_stream.h>
#include <systemlib/err.h>
@@ -87,6 +88,8 @@ public:
virtual int ioctl(file *filp, int cmd, unsigned long arg);
void set_rx_mode(unsigned mode);
private:
static const unsigned _max_actuators = PX4IO_OUTPUT_CHANNELS;
@@ -103,6 +106,9 @@ private:
int _t_armed; ///< system armed control topic
actuator_armed_s _armed; ///< system armed state
orb_advert_t _to_input_rc; ///< rc inputs from io
rc_input_values _input_rc; ///< rc input values
orb_advert_t _t_outputs; ///< mixed outputs topic
actuator_outputs_s _outputs; ///< mixed outputs
@@ -114,6 +120,9 @@ private:
// XXX how should this work?
bool _send_needed; ///< If true, we need to send a packet to IO
bool _config_needed; ///< if true, we need to set a config update to IO
uint8_t _rx_mode; ///< the current RX mode on IO
/**
* Trampoline to the worker task
@@ -145,6 +154,11 @@ private:
*/
void io_send();
/**
* Send a config packet to PX4IO
*/
void config_send();
/**
* Mixer control callback; invoked to fetch a control from a specific
* group/index during mixing.
@@ -176,7 +190,9 @@ PX4IO::PX4IO() :
_mixers(nullptr),
_primary_pwm_device(false),
_switch_armed(false),
_send_needed(false)
_send_needed(false),
_config_needed(false),
_rx_mode(RX_MODE_PPM_ONLY)
{
/* we need this potentially before it could be set in task_main */
g_dev = this;
@@ -305,9 +321,14 @@ PX4IO::task_main()
orb_set_interval(_t_armed, 200); /* 5Hz update rate */
/* advertise the mixed control outputs */
memset(&_outputs, 0, sizeof(_outputs));
_t_outputs = orb_advertise(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1),
&_outputs);
/* advertise the rc inputs */
memset(&_input_rc, 0, sizeof(_input_rc));
_to_input_rc = orb_advertise(ORB_ID(input_rc), &_input_rc);
/* poll descriptor */
pollfd fds[3];
fds[0].fd = _serial_fd;
@@ -373,6 +394,12 @@ PX4IO::task_main()
_send_needed = false;
io_send();
}
/* send a config packet to IO if required */
if (_config_needed) {
_config_needed = false;
config_send();
}
}
out:
@@ -438,7 +465,14 @@ PX4IO::rx_callback(const uint8_t *buffer, size_t bytes_received)
}
_connected = true;
/* XXX handle R/C inputs here ... needs code sharing/library */
/* publish raw rc channel values from IO */
_input_rc.timestamp = hrt_absolute_time();
for (int i = 0; i < rep->channel_count; i++)
{
_input_rc.values[i] = rep->rc_channel[i];
}
orb_publish(ORB_ID(input_rc), _to_input_rc, &_input_rc);
/* remember the latched arming switch state */
_switch_armed = rep->armed;
@@ -473,6 +507,20 @@ PX4IO::io_send()
debug("send error %d", ret);
}
void
PX4IO::config_send()
{
px4io_config cfg;
int ret;
cfg.f2i_config_magic = F2I_CONFIG_MAGIC;
cfg.serial_rx_mode = _rx_mode;
ret = hx_stream_send(_io_stream, &cfg, sizeof(cfg));
if (ret)
debug("config error %d", ret);
}
int
PX4IO::ioctl(file *filep, int cmd, unsigned long arg)
{
@@ -586,6 +634,15 @@ PX4IO::ioctl(file *filep, int cmd, unsigned long arg)
return ret;
}
void
PX4IO::set_rx_mode(unsigned mode)
{
if (mode != _rx_mode) {
_rx_mode = mode;
_config_needed = true;
}
}
extern "C" __EXPORT int px4io_main(int argc, char *argv[]);
namespace
@@ -642,9 +699,6 @@ px4io_main(int argc, char *argv[])
exit(0);
}
if (!strcmp(argv[1], "test"))
test();
/* note, stop not currently implemented */
if (!strcmp(argv[1], "update")) {
@@ -690,5 +744,25 @@ px4io_main(int argc, char *argv[])
return ret;
}
errx(1, "need a verb, only support 'start' and 'update'");
if (!strcmp(argv[1], "rx_spektrum6")) {
if (g_dev == nullptr)
errx(1, "not started");
g_dev->set_rx_mode(RX_MODE_SPEKTRUM_6);
}
if (!strcmp(argv[1], "rx_spektrum7")) {
if (g_dev == nullptr)
errx(1, "not started");
g_dev->set_rx_mode(RX_MODE_SPEKTRUM_7);
}
if (!strcmp(argv[1], "rx_sbus")) {
if (g_dev == nullptr)
errx(1, "not started");
g_dev->set_rx_mode(RX_MODE_FUTABA_SBUS);
}
if (!strcmp(argv[1], "test"))
test();
errx(1, "need a command, try 'start', 'test', 'rx_spektrum6', 'rx_spektrum7', 'rx_sbus' or 'update'");
}
+1 -1
View File
@@ -338,7 +338,7 @@ static void hrt_call_invoke(void);
/* decoded PPM buffer */
#define PPM_MAX_CHANNELS 12
__EXPORT uint16_t ppm_buffer[PPM_MAX_CHANNELS];
__EXPORT unsigned ppm_decoded_channels;
__EXPORT unsigned ppm_decoded_channels = 0;
__EXPORT uint64_t ppm_last_valid_decode = 0;
/* PPM edge history */
+7 -8
View File
@@ -589,16 +589,15 @@ int mavlink_thread_main(int argc, char *argv[])
/* 2 Hz */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_MANUAL_CONTROL, 100);
} else if (baudrate >= 115200) {
/* 50 Hz / 20 ms */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_HIGHRES_IMU, 200);
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_RAW_IMU, 200);
/* 20 Hz / 50 ms */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_ATTITUDE, 200);
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, 200);
/* 10 Hz / 100 ms */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_HIGHRES_IMU, 50);
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_RAW_IMU, 50);
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_ATTITUDE, 50);
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, 50);
/* 5 Hz / 100 ms */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, 200);
/* 1 Hz */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_MANUAL_CONTROL, 1000);
/* 2 Hz */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_MANUAL_CONTROL, 500);
} else if (baudrate >= 57600) {
/* 10 Hz / 100 ms */
set_mavlink_interval_limit(&mavlink_subs, MAVLINK_MSG_ID_RAW_IMU, 300);
-4
View File
@@ -397,10 +397,6 @@ handle_message(mavlink_message_t *msg)
rc_hil.timestamp = hrt_absolute_time();
rc_hil.chan_count = 4;
rc_hil.chan[0].raw = 1500 + man.x / 2;
rc_hil.chan[1].raw = 1500 + man.y / 2;
rc_hil.chan[2].raw = 1500 + man.r / 2;
rc_hil.chan[3].raw = 1500 + man.z / 2;
rc_hil.chan[0].scaled = man.x / 1000.0f;
rc_hil.chan[1].scaled = man.y / 1000.0f;
+25 -10
View File
@@ -67,6 +67,7 @@ struct vehicle_global_position_s global_pos;
struct vehicle_local_position_s local_pos;
struct vehicle_status_s v_status;
struct rc_channels_s rc;
struct rc_input_values rc_raw;
struct actuator_armed_s armed;
struct mavlink_subscriptions mavlink_subs;
@@ -99,6 +100,7 @@ static void l_vehicle_attitude(struct listener *l);
static void l_vehicle_gps_position(struct listener *l);
static void l_vehicle_status(struct listener *l);
static void l_rc_channels(struct listener *l);
static void l_input_rc(struct listener *l);
static void l_global_position(struct listener *l);
static void l_local_position(struct listener *l);
static void l_global_position_setpoint(struct listener *l);
@@ -116,6 +118,7 @@ struct listener listeners[] = {
{l_vehicle_gps_position, &mavlink_subs.gps_sub, 0},
{l_vehicle_status, &status_sub, 0},
{l_rc_channels, &rc_sub, 0},
{l_input_rc, &mavlink_subs.input_rc_sub, 0},
{l_global_position, &mavlink_subs.global_pos_sub, 0},
{l_local_position, &mavlink_subs.local_pos_sub, 0},
{l_global_position_setpoint, &mavlink_subs.spg_sub, 0},
@@ -274,21 +277,29 @@ l_rc_channels(struct listener *l)
{
/* copy rc channels into local buffer */
orb_copy(ORB_ID(rc_channels), rc_sub, &rc);
// XXX Add RC channels scaled message here
}
void
l_input_rc(struct listener *l)
{
/* copy rc channels into local buffer */
orb_copy(ORB_ID(input_rc), mavlink_subs.input_rc_sub, &rc_raw);
if (gcs_link)
/* Channels are sent in MAVLink main loop at a fixed interval */
mavlink_msg_rc_channels_raw_send(chan,
rc.timestamp / 1000,
rc_raw.timestamp / 1000,
0,
rc.chan[0].raw,
rc.chan[1].raw,
rc.chan[2].raw,
rc.chan[3].raw,
rc.chan[4].raw,
rc.chan[5].raw,
rc.chan[6].raw,
rc.chan[7].raw,
rc.rssi);
(rc_raw.channel_count > 0) ? rc_raw.values[0] : UINT16_MAX,
(rc_raw.channel_count > 1) ? rc_raw.values[1] : UINT16_MAX,
(rc_raw.channel_count > 2) ? rc_raw.values[2] : UINT16_MAX,
(rc_raw.channel_count > 3) ? rc_raw.values[3] : UINT16_MAX,
(rc_raw.channel_count > 4) ? rc_raw.values[4] : UINT16_MAX,
(rc_raw.channel_count > 5) ? rc_raw.values[5] : UINT16_MAX,
(rc_raw.channel_count > 6) ? rc_raw.values[6] : UINT16_MAX,
(rc_raw.channel_count > 7) ? rc_raw.values[7] : UINT16_MAX,
255);
}
void
@@ -584,6 +595,10 @@ uorb_receive_start(void)
rc_sub = orb_subscribe(ORB_ID(rc_channels));
orb_set_interval(rc_sub, 100); /* 10Hz updates */
/* --- RC RAW VALUE --- */
mavlink_subs.input_rc_sub = orb_subscribe(ORB_ID(input_rc));
orb_set_interval(mavlink_subs.input_rc_sub, 100);
/* --- GLOBAL POS VALUE --- */
mavlink_subs.global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
orb_set_interval(mavlink_subs.global_pos_sub, 1000); /* 1Hz active updates */
+2
View File
@@ -57,6 +57,7 @@
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/debug_key_value.h>
#include <drivers/drv_rc_input.h>
struct mavlink_subscriptions {
int sensor_sub;
@@ -75,6 +76,7 @@ struct mavlink_subscriptions {
int spl_sub;
int spg_sub;
int debug_key_value;
int input_rc_sub;
};
extern struct mavlink_subscriptions mavlink_subs;
+3 -4
View File
@@ -360,7 +360,7 @@ void check_waypoints_reached(uint64_t now, const struct vehicle_global_position_
float dist = -1.0f;
if (coordinate_frame == (int)MAV_FRAME_GLOBAL) {
dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, global_pos->lat, global_pos->lon, global_pos->alt);
dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, (float)global_pos->lat * 1e-7f, (float)global_pos->lon * 1e-7f, global_pos->alt);
} else if (coordinate_frame == (int)MAV_FRAME_GLOBAL_RELATIVE_ALT) {
dist = mavlink_wpm_distance_to_point_global_wgs84(wpm->current_active_wp_id, global_pos->lat, global_pos->lon, global_pos->relative_alt);
@@ -376,14 +376,13 @@ void check_waypoints_reached(uint64_t now, const struct vehicle_global_position_
if (dist >= 0.f && dist <= orbit /*&& wpm->yaw_reached*/) { //TODO implement yaw
wpm->pos_reached = true;
if (counter % 10 == 0)
if (counter % 100 == 0)
printf("Setpoint reached: %0.4f, orbit: %.4f\n", dist, orbit);
}
// else
// {
// if(counter % 100 == 0)
// printf("Setpoint not reached yet: %0.4f, orbit: %.4f\n",dist,orbit);
// printf("Setpoint not reached yet: %0.4f, orbit: %.4f, coordinate frame: %d\n",dist, orbit, coordinate_frame);
// }
}
@@ -196,12 +196,14 @@ multirotor_pos_control_thread_main(int argc, char *argv[])
float x_setpoint = 0.0f;
// XXX enable switching between Vicon and local position estimate
/* local pos is the Vicon position */
att_sp.pitch_body = (local_pos.x - x_setpoint) * p.p * dT;
// XXX just an example, lacks rotation around world-body transformation
att_sp.pitch_body = (local_pos.x - x_setpoint) * p.p;
att_sp.roll_body = 0.0f;
att_sp.yaw_body = 0.0f;
att_sp.thrust = 0.4f;
att_sp.thrust = 0.3f;
att_sp.timestamp = hrt_absolute_time();
/* publish new attitude setpoint */
+44 -7
View File
@@ -116,18 +116,32 @@ int frame_rx;
int frame_bad;
static void
comms_handle_frame(void *arg, const void *buffer, size_t length)
comms_handle_config(const void *buffer, size_t length)
{
struct px4io_command *cmd = (struct px4io_command *)buffer;
const struct px4io_config *cfg = (struct px4io_config *)buffer;
/* make sure it's what we are expecting */
if ((length != sizeof(struct px4io_command)) ||
(cmd->f2i_magic != F2I_MAGIC)) {
frame_bad++;
if (length != sizeof(*cfg)) {
frame_bad++;
return;
}
frame_rx++;
mixer_set_serial_mode(cfg->serial_rx_mode);
}
static void
comms_handle_command(const void *buffer, size_t length)
{
const struct px4io_command *cmd = (struct px4io_command *)buffer;
if (length != sizeof(*cmd)) {
frame_bad++;
return;
}
frame_rx++;
irqstate_t flags = irqsave();
/* fetch new PWM output values */
@@ -146,6 +160,29 @@ comms_handle_frame(void *arg, const void *buffer, size_t length)
for (unsigned i = 0; i < PX4IO_RELAY_CHANNELS; i++)
system_state.relays[i] = cmd->relay_state[i];
out:
irqrestore(flags);
}
static void
comms_handle_frame(void *arg, const void *buffer, size_t length)
{
const uint16_t *type = (const uint16_t *)buffer;
/* make sure it's what we are expecting */
if (length > 2) {
switch (*type) {
case F2I_MAGIC:
comms_handle_command(buffer, length);
break;
case F2I_CONFIG_MAGIC:
comms_handle_config(buffer, length);
break;
default:
break;
}
}
frame_bad++;
}
+179 -24
View File
@@ -40,10 +40,13 @@
#include <sys/types.h>
#include <stdbool.h>
#include <string.h>
#include <assert.h>
#include <errno.h>
#include <fcntl.h>
#include <termios.h>
#include <unistd.h>
#include <fcntl.h>
#include <drivers/drv_pwm_output.h>
#include <drivers/drv_hrt.h>
@@ -64,6 +67,11 @@ static unsigned mixer_input_drops;
static unsigned fmu_input_drops;
#define FMU_INPUT_DROP_LIMIT 20
/*
* Serial port fd for serial RX protocols
*/
static int rx_port = -1;
/*
* HRT periodic call used to check for control input data.
*/
@@ -98,12 +106,47 @@ struct mixer {
int
mixer_init(void)
{
/* open the serial port */
rx_port = open("/dev/ttyS0", O_RDONLY | O_NONBLOCK);
/* look for control data at 50Hz */
hrt_call_every(&mixer_input_call, 1000, 20000, mixer_tick, NULL);
return 0;
}
void
mixer_set_serial_mode(uint8_t serial_mode)
{
if (serial_mode == system_state.serial_rx_mode)
return;
struct termios t;
tcgetattr(rx_port, &t);
switch (serial_mode) {
case RX_MODE_PPM_ONLY:
break;
case RX_MODE_SPEKTRUM_6:
case RX_MODE_SPEKTRUM_7:
/* 115200, no parity, one stop bit */
cfsetspeed(&t, 115200);
t.c_cflag &= ~(CSTOPB | PARENB);
break;
case RX_MODE_FUTABA_SBUS:
/* 100000, even parity, two stop bits */
cfsetspeed(&t, 100000);
t.c_cflag |= (CSTOPB | PARENB);
break;
default:
return;
}
tcsetattr(rx_port, TCSANOW, &t);
system_state.serial_rx_mode = serial_mode;
}
static void
mixer_tick(void *arg)
{
@@ -180,23 +223,146 @@ mixer_tick(void *arg)
}
}
static void
mixer_update(int mixer, uint16_t *inputs, int input_count)
{
/* simple passthrough for now */
if (mixer < input_count) {
mixers[mixer].current_value = inputs[mixer];
} else {
mixers[mixer].current_value = 0;
}
}
static bool
mixer_get_spektrum_input(void)
{
static uint8_t buf[16];
static unsigned count;
/* always read as much data as we can into the buffer */
if (count >= sizeof(buf))
count = 0;
ssize_t result = read(rx_port, buf, sizeof(buf) - count);
/* no data or an error */
if (result <= 0)
return false;
count += result;
/* if there are more than two bytes in the buffer, check for sync */
if (count >= 2) {
if ((buf[0] != 0x3) || (buf[1] != 0x1)) {
/* not in sync; look for a possible sync marker */
for (unsigned i = 1; i < count; i++) {
if (buf[i] == 0x3) {
/* could be a frame marker; move buffer bytes */
count -= i;
memmove(buf, buf + i, count);
break;
}
}
}
}
if (count < sizeof(buf))
return false;
/* we got a frame; decode it */
const uint16_t *channels = (const uint16_t *)&buf[2];
/*
* Channel assignment for DX6i vs. DX7 is different.
*
* DX7 etc. is:
*
* 0: Aileron
* 1: Flaps
* 2: Gear
* 3: Elevator
* 4: Aux2
* 5: Throttle
* 6: Rudder
*
* DX6i is:
*
* 0: Aileron
* 1: Flaps
* 2: Elevator
* 3: Rudder
* 4: Throttle
* 5: Gear
* 6: <notused>
*
* We convert these to our standard Futaba-style assignment:
*
* 0: Throttle (Throttle)
* 1: Roll (Aileron)
* 2: Pitch (Elevator)
* 3: Yaw (Rudder)
* 4: Override (Flaps)
* 5: FUNC_0 (Gear)
* 6: FUNC_1 (Aux2)
*/
if (system_state.serial_rx_mode == RX_MODE_SPEKTRUM_7) {
system_state.rc_channel_data[0] = channels[5]; /* Throttle */
system_state.rc_channel_data[1] = channels[0]; /* Roll */
system_state.rc_channel_data[2] = channels[3]; /* Pitch */
system_state.rc_channel_data[3] = channels[6]; /* Yaw */
system_state.rc_channel_data[4] = channels[1]; /* Override */
system_state.rc_channel_data[5] = channels[2]; /* FUNC_0 */
system_state.rc_channel_data[6] = channels[4]; /* FUNC_1 */
system_state.rc_channels = 7;
} else {
system_state.rc_channel_data[0] = channels[4]; /* Throttle */
system_state.rc_channel_data[1] = channels[0]; /* Roll */
system_state.rc_channel_data[2] = channels[2]; /* Pitch */
system_state.rc_channel_data[3] = channels[3]; /* Yaw */
system_state.rc_channel_data[4] = channels[1]; /* Override */
system_state.rc_channel_data[5] = channels[5]; /* FUNC_0 */
system_state.rc_channels = 6;
}
count = 0;
return true;
}
static bool
mixer_get_sbus_input(void)
{
/* XXX not implemented yet */
return false;
}
static void
mixer_get_rc_input(void)
{
/*
* XXX currently only supporting PPM
*
* XXX check timestamp to ensure current
*/
if (ppm_decoded_channels > 0) {
bool got_input = false;
switch (system_state.serial_rx_mode) {
case RX_MODE_PPM_ONLY:
if (ppm_decoded_channels > 0) {
/* copy channel data */
system_state.rc_channels = ppm_decoded_channels;
for (unsigned i = 0; i < ppm_decoded_channels; i++)
system_state.rc_channel_data[i] = ppm_buffer[i];
got_input = true;
}
break;
case RX_MODE_SPEKTRUM_6:
case RX_MODE_SPEKTRUM_7:
got_input = mixer_get_spektrum_input();
break;
case RX_MODE_FUTABA_SBUS:
got_input = mixer_get_sbus_input();
break;
default:
break;
}
if (got_input) {
mixer_input_drops = 0;
system_state.fmu_report_due = true;
/* copy channel data */
system_state.rc_channels = ppm_decoded_channels;
for (unsigned i = 0; i < ppm_decoded_channels; i++)
system_state.rc_channel_data[i] = ppm_buffer[i];
} else {
/*
* No data; count the 'frame drops' and once we hit the limit
@@ -213,14 +379,3 @@ mixer_get_rc_input(void)
}
}
}
static void
mixer_update(int mixer, uint16_t *inputs, int input_count)
{
/* simple passthrough for now */
if (mixer < input_count) {
mixers[mixer].current_value = inputs[mixer];
} else {
mixers[mixer].current_value = 0;
}
}
+12
View File
@@ -62,6 +62,18 @@ struct px4io_command {
bool arm_ok;
};
/* config message from FMU to IO */
struct px4io_config {
uint16_t f2i_config_magic;
#define F2I_CONFIG_MAGIC 0x6366
uint8_t serial_rx_mode;
#define RX_MODE_PPM_ONLY 0
#define RX_MODE_SPEKTRUM_6 1
#define RX_MODE_SPEKTRUM_7 2
#define RX_MODE_FUTABA_SBUS 3
};
/* report from IO to FMU */
struct px4io_report {
uint16_t i2f_magic;
+7 -7
View File
@@ -102,7 +102,7 @@ int user_start(int argc, char *argv[])
safety_init();
/* set up some timers for the main loop */
timers[TIMER_BLINK_AMBER] = 250; /* heartbeat blink @ 2Hz */
timers[TIMER_BLINK_BLUE] = 250; /* heartbeat blink @ 2Hz */
timers[TIMER_STATUS_PRINT] = 1000; /* print status message @ 1Hz */
/*
@@ -114,21 +114,21 @@ int user_start(int argc, char *argv[])
comms_check();
/* blink the heartbeat LED */
if (timers[TIMER_BLINK_AMBER] == 0) {
timers[TIMER_BLINK_AMBER] = 250;
LED_AMBER(heartbeat = !heartbeat);
if (timers[TIMER_BLINK_BLUE] == 0) {
timers[TIMER_BLINK_BLUE] = 250;
LED_BLUE(heartbeat = !heartbeat);
}
/* blink the failsafe LED if we don't have FMU input */
if (!system_state.mixer_use_fmu) {
if (timers[TIMER_BLINK_BLUE] == 0) {
timers[TIMER_BLINK_BLUE] = 125;
if (timers[TIMER_BLINK_AMBER] == 0) {
timers[TIMER_BLINK_AMBER] = 125;
failsafe = !failsafe;
}
} else {
failsafe = false;
}
LED_BLUE(failsafe);
LED_AMBER(failsafe);
/* print some simple status */
if (timers[TIMER_STATUS_PRINT] == 0) {
+9 -2
View File
@@ -101,6 +101,12 @@ struct sys_state_s
* If true, new control data from the FMU has been received.
*/
bool fmu_data_received;
/*
* Current serial interface mode, per the serial_rx_mode parameter
* in the config packet.
*/
uint8_t serial_rx_mode;
};
extern struct sys_state_s system_state;
@@ -123,8 +129,8 @@ extern volatile int timers[TIMER_NUM_TIMERS];
/*
* GPIO handling.
*/
#define LED_AMBER(_s) stm32_gpiowrite(GPIO_LED1, !(_s))
#define LED_BLUE(_s) stm32_gpiowrite(GPIO_LED2, !(_s))
#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 POWER_SERVO(_s) stm32_gpiowrite(GPIO_SERVO_PWR_EN, (_s))
@@ -141,6 +147,7 @@ extern volatile int timers[TIMER_NUM_TIMERS];
* Mixer
*/
extern int mixer_init(void);
extern void mixer_set_serial_mode(uint8_t newmode);
/*
* Safety switch/LED.
+118 -86
View File
@@ -58,11 +58,13 @@
#include <drivers/drv_gyro.h>
#include <drivers/drv_mag.h>
#include <drivers/drv_baro.h>
#include <drivers/drv_rc_input.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>
#include <systemlib/perf_counter.h>
#include <systemlib/ppm_decode.h>
#include <uORB/uORB.h>
@@ -143,6 +145,7 @@ private:
int _gyro_sub; /**< raw gyro data subscription */
int _accel_sub; /**< raw accel data subscription */
int _mag_sub; /**< raw mag data subscription */
int _rc_sub; /**< raw rc channels data subscription */
int _baro_sub; /**< raw baro data subscription */
int _vstatus_sub; /**< vehicle status subscription */
int _params_sub; /**< notification of parameter updates */
@@ -162,6 +165,7 @@ private:
float rev[_rc_max_chan_count];
float dz[_rc_max_chan_count];
float ex[_rc_max_chan_count];
float scaling_factor[_rc_max_chan_count];
float gyro_offset[3];
float mag_offset[3];
@@ -331,6 +335,7 @@ Sensors::Sensors() :
_gyro_sub(-1),
_accel_sub(-1),
_mag_sub(-1),
_rc_sub(-1),
_baro_sub(-1),
_vstatus_sub(-1),
_params_sub(-1),
@@ -464,14 +469,13 @@ Sensors::parameters_update()
warnx("Failed getting exponential gain for chan %d", i);
}
_rc.chan[i].scaling_factor = (1.0f / ((_parameters.max[i] - _parameters.min[i]) / 2.0f) * _parameters.rev[i]);
_parameters.scaling_factor[i] = (1.0f / ((_parameters.max[i] - _parameters.min[i]) / 2.0f) * _parameters.rev[i]);
/* handle blowup in the scaling factor calculation */
if (isnan(_rc.chan[i].scaling_factor) || isinf(_rc.chan[i].scaling_factor)) {
_rc.chan[i].scaling_factor = 0;
if (isnan(_parameters.scaling_factor[i]) || isinf(_parameters.scaling_factor[i])) {
_parameters.scaling_factor[i] = 0;
}
_rc.chan[i].mid = _parameters.trim[i];
}
/* update RC function mappings */
@@ -856,99 +860,126 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
void
Sensors::ppm_poll()
{
struct manual_control_setpoint_s manual_control;
/* fake low-level driver, directly pulling from driver variables */
static orb_advert_t rc_input_pub = -1;
struct rc_input_values raw;
/* check to see whether a new frame has been decoded */
if (_ppm_last_valid == ppm_last_valid_decode)
return;
/* require at least two chanels to consider the signal valid */
if (ppm_decoded_channels < 4)
return;
raw.timestamp = ppm_last_valid_decode;
unsigned channel_limit = ppm_decoded_channels;
if (channel_limit > _rc_max_chan_count)
channel_limit = _rc_max_chan_count;
if (ppm_decoded_channels > 1) {
/* we are accepting this decode */
_ppm_last_valid = ppm_last_valid_decode;
/* Read out values from HRT */
for (unsigned int i = 0; i < channel_limit; i++) {
_rc.chan[i].raw = ppm_buffer[i];
/* scale around the mid point differently for lower and upper range */
if (ppm_buffer[i] > (_parameters.trim[i] + _parameters.dz[i])) {
_rc.chan[i].scaled = (ppm_buffer[i] - _parameters.trim[i]) / (float)(_parameters.max[i] - _parameters.trim[i]);
} else if (ppm_buffer[i] < (_parameters.trim[i] - _parameters.dz[i])) {
/* division by zero impossible for trim == min (as for throttle), as this falls in the above if clause */
_rc.chan[i].scaled = -((_parameters.trim[i] - ppm_buffer[i]) / (float)(_parameters.trim[i] - _parameters.min[i]));
} else {
/* in the configured dead zone, output zero */
_rc.chan[i].scaled = 0.0f;
for (int i = 0; i < ppm_decoded_channels; i++) {
raw.values[i] = ppm_buffer[i];
}
/* reverse channel if required */
if (i == _rc.function[THROTTLE]) {
if ((int)_parameters.rev[i] == -1) {
_rc.chan[i].scaled = 1.0f + -1.0f * _rc.chan[i].scaled;
raw.channel_count = ppm_decoded_channels;
/* publish to object request broker */
if (rc_input_pub <= 0) {
rc_input_pub = orb_advertise(ORB_ID(input_rc), &raw);
} else {
orb_publish(ORB_ID(input_rc), rc_input_pub, &raw);
}
}
/* read low-level values from FMU or IO RC inputs (PPM, Spektrum, S.Bus) */
bool rc_updated;
orb_check(_rc_sub, &rc_updated);
if (rc_updated) {
struct rc_input_values rc_input;
orb_copy(ORB_ID(input_rc), _rc_sub, &rc_input);
struct manual_control_setpoint_s manual_control;
/* require at least two chanels to consider the signal valid */
if (rc_input.channel_count < 2)
return;
unsigned channel_limit = rc_input.channel_count;
if (channel_limit > _rc_max_chan_count)
channel_limit = _rc_max_chan_count;
/* we are accepting this message */
_ppm_last_valid = rc_input.timestamp;
/* Read out values from raw message */
for (unsigned int i = 0; i < channel_limit; i++) {
/* scale around the mid point differently for lower and upper range */
if (rc_input.values[i] > (_parameters.trim[i] + _parameters.dz[i])) {
_rc.chan[i].scaled = (rc_input.values[i] - _parameters.trim[i]) / (float)(_parameters.max[i] - _parameters.trim[i]);
} else if (rc_input.values[i] < (_parameters.trim[i] - _parameters.dz[i])) {
/* division by zero impossible for trim == min (as for throttle), as this falls in the above if clause */
_rc.chan[i].scaled = -((_parameters.trim[i] - rc_input.values[i]) / (float)(_parameters.trim[i] - _parameters.min[i]));
} else {
/* in the configured dead zone, output zero */
_rc.chan[i].scaled = 0.0f;
}
} else {
_rc.chan[i].scaled *= _parameters.rev[i];
/* reverse channel if required */
if (i == _rc.function[THROTTLE]) {
if ((int)_parameters.rev[i] == -1) {
_rc.chan[i].scaled = 1.0f + -1.0f * _rc.chan[i].scaled;
}
} else {
_rc.chan[i].scaled *= _parameters.rev[i];
}
/* handle any parameter-induced blowups */
if (isnan(_rc.chan[i].scaled) || isinf(_rc.chan[i].scaled))
_rc.chan[i].scaled = 0.0f;
}
/* handle any parameter-induced blowups */
if (isnan(_rc.chan[i].scaled) || isinf(_rc.chan[i].scaled))
_rc.chan[i].scaled = 0.0f;
_rc.chan_count = rc_input.channel_count;
_rc.timestamp = rc_input.timestamp;
//_rc.chan[i].scaled = (ppm_buffer[i] - _rc.chan[i].mid) * _rc.chan[i].scaling_factor;
manual_control.timestamp = rc_input.timestamp;
/* roll input - rolling right is stick-wise and rotation-wise positive */
manual_control.roll = _rc.chan[_rc.function[ROLL]].scaled;
if (manual_control.roll < -1.0f) manual_control.roll = -1.0f;
if (manual_control.roll > 1.0f) manual_control.roll = 1.0f;
if (!isnan(_parameters.rc_scale_roll) || !isinf(_parameters.rc_scale_roll)) {
manual_control.roll *= _parameters.rc_scale_roll;
}
/*
* pitch input - stick down is negative, but stick down is pitching up (pos) in NED,
* so reverse sign.
*/
manual_control.pitch = -1.0f * _rc.chan[_rc.function[PITCH]].scaled;
if (manual_control.pitch < -1.0f) manual_control.pitch = -1.0f;
if (manual_control.pitch > 1.0f) manual_control.pitch = 1.0f;
if (!isnan(_parameters.rc_scale_pitch) || !isinf(_parameters.rc_scale_pitch)) {
manual_control.pitch *= _parameters.rc_scale_pitch;
}
/* yaw input - stick right is positive and positive rotation */
manual_control.yaw = _rc.chan[_rc.function[YAW]].scaled * _parameters.rc_scale_yaw;
if (manual_control.yaw < -1.0f) manual_control.yaw = -1.0f;
if (manual_control.yaw > 1.0f) manual_control.yaw = 1.0f;
if (!isnan(_parameters.rc_scale_yaw) || !isinf(_parameters.rc_scale_yaw)) {
manual_control.yaw *= _parameters.rc_scale_yaw;
}
/* throttle input */
manual_control.throttle = _rc.chan[_rc.function[THROTTLE]].scaled;
if (manual_control.throttle < 0.0f) manual_control.throttle = 0.0f;
if (manual_control.throttle > 1.0f) manual_control.throttle = 1.0f;
/* mode switch input */
manual_control.override_mode_switch = _rc.chan[_rc.function[OVERRIDE]].scaled;
if (manual_control.override_mode_switch < -1.0f) manual_control.override_mode_switch = -1.0f;
if (manual_control.override_mode_switch > 1.0f) manual_control.override_mode_switch = 1.0f;
orb_publish(ORB_ID(rc_channels), _rc_pub, &_rc);
orb_publish(ORB_ID(manual_control_setpoint), _manual_control_pub, &manual_control);
}
_rc.chan_count = ppm_decoded_channels;
_rc.timestamp = ppm_last_valid_decode;
manual_control.timestamp = ppm_last_valid_decode;
/* roll input - rolling right is stick-wise and rotation-wise positive */
manual_control.roll = _rc.chan[_rc.function[ROLL]].scaled;
if (manual_control.roll < -1.0f) manual_control.roll = -1.0f;
if (manual_control.roll > 1.0f) manual_control.roll = 1.0f;
if (!isnan(_parameters.rc_scale_roll) || !isinf(_parameters.rc_scale_roll)) {
manual_control.roll *= _parameters.rc_scale_roll;
}
/*
* pitch input - stick down is negative, but stick down is pitching up (pos) in NED,
* so reverse sign.
*/
manual_control.pitch = -1.0f * _rc.chan[_rc.function[PITCH]].scaled;
if (manual_control.pitch < -1.0f) manual_control.pitch = -1.0f;
if (manual_control.pitch > 1.0f) manual_control.pitch = 1.0f;
if (!isnan(_parameters.rc_scale_pitch) || !isinf(_parameters.rc_scale_pitch)) {
manual_control.pitch *= _parameters.rc_scale_pitch;
}
/* yaw input - stick right is positive and positive rotation */
manual_control.yaw = _rc.chan[_rc.function[YAW]].scaled * _parameters.rc_scale_yaw;
if (manual_control.yaw < -1.0f) manual_control.yaw = -1.0f;
if (manual_control.yaw > 1.0f) manual_control.yaw = 1.0f;
if (!isnan(_parameters.rc_scale_yaw) || !isinf(_parameters.rc_scale_yaw)) {
manual_control.yaw *= _parameters.rc_scale_yaw;
}
/* throttle input */
manual_control.throttle = _rc.chan[_rc.function[THROTTLE]].scaled;
if (manual_control.throttle < 0.0f) manual_control.throttle = 0.0f;
if (manual_control.throttle > 1.0f) manual_control.throttle = 1.0f;
/* mode switch input */
manual_control.override_mode_switch = _rc.chan[_rc.function[OVERRIDE]].scaled;
if (manual_control.override_mode_switch < -1.0f) manual_control.override_mode_switch = -1.0f;
if (manual_control.override_mode_switch > 1.0f) manual_control.override_mode_switch = 1.0f;
orb_publish(ORB_ID(rc_channels), _rc_pub, &_rc);
orb_publish(ORB_ID(manual_control_setpoint), _manual_control_pub, &manual_control);
}
#endif
@@ -979,6 +1010,7 @@ Sensors::task_main()
_gyro_sub = orb_subscribe(ORB_ID(sensor_gyro));
_accel_sub = orb_subscribe(ORB_ID(sensor_accel));
_mag_sub = orb_subscribe(ORB_ID(sensor_mag));
_rc_sub = orb_subscribe(ORB_ID(input_rc));
_baro_sub = orb_subscribe(ORB_ID(sensor_baro));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_params_sub = orb_subscribe(ORB_ID(parameter_update));
+144
View File
@@ -47,6 +47,150 @@
#include <systemlib/geo/geo.h>
#include <math.h>
/* values for map projection */
static double phi_1;
static double sin_phi_1;
static double cos_phi_1;
static double lambda_0;
static double scale;
/**
* Initializes the map transformation.
*
* Initializes the transformation between the geographic coordinate system and the azimuthal equidistant plane
* @param lat in degrees (47.1234567°, not 471234567°)
* @param lon in degrees (8.1234567°, not 81234567°)
*/
__EXPORT static void map_projection_init(double lat_0, double lon_0) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567
{
/* notation and formulas according to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */
phi_1 = lat_0 / 180.0 * M_PI;
lambda_0 = lon_0 / 180.0 * M_PI;
sin_phi_1 = sin(phi_1);
cos_phi_1 = cos(phi_1);
/* calculate local scale by using the relation of true distance and the distance on plane */ //TODO: this is a quick solution, there are probably easier ways to determine the scale
/* 1) calculate true distance d on sphere to a point: http://www.movable-type.co.uk/scripts/latlong.html */
const double r_earth = 6371000;
double lat1 = phi_1;
double lon1 = lambda_0;
double lat2 = phi_1 + 0.5 / 180 * M_PI;
double lon2 = lambda_0 + 0.5 / 180 * M_PI;
double sin_lat_2 = sin(lat2);
double cos_lat_2 = cos(lat2);
double d = acos(sin(lat1) * sin_lat_2 + cos(lat1) * cos_lat_2 * cos(lon2 - lon1)) * r_earth;
/* 2) calculate distance rho on plane */
double k_bar = 0;
double c = acos(sin_phi_1 * sin_lat_2 + cos_phi_1 * cos_lat_2 * cos(lon2 - lambda_0));
if (0 != c)
k_bar = c / sin(c);
double x2 = k_bar * (cos_lat_2 * sin(lon2 - lambda_0)); //Projection of point 2 on plane
double y2 = k_bar * ((cos_phi_1 * sin_lat_2 - sin_phi_1 * cos_lat_2 * cos(lon2 - lambda_0)));
double rho = sqrt(pow(x2, 2) + pow(y2, 2));
scale = d / rho;
}
/**
* Transforms a point in the geographic coordinate system to the local azimuthal equidistant plane
* @param x north
* @param y east
* @param lat in degrees (47.1234567°, not 471234567°)
* @param lon in degrees (8.1234567°, not 81234567°)
*/
__EXPORT static void map_projection_project(double lat, double lon, float *x, float *y)
{
/* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */
double phi = lat / 180.0 * M_PI;
double lambda = lon / 180.0 * M_PI;
double sin_phi = sin(phi);
double cos_phi = cos(phi);
double k_bar = 0;
/* using small angle approximation (formula in comment is without aproximation) */
double c = acos(sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2)); //double c = acos( sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * cos(lambda - lambda_0) );
if (0 != c)
k_bar = c / sin(c);
/* using small angle approximation (formula in comment is without aproximation) */
*y = k_bar * (cos_phi * (lambda - lambda_0)) * scale;//*y = k_bar * (cos_phi * sin(lambda - lambda_0)) * scale;
*x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2))) * scale; // *x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * cos(lambda - lambda_0))) * scale;
// printf("%phi_1=%.10f, lambda_0 =%.10f\n", phi_1, lambda_0);
}
/**
* Transforms a point in the local azimuthal equidistant plane to the geographic coordinate system
*
* @param x north
* @param y east
* @param lat in degrees (47.1234567°, not 471234567°)
* @param lon in degrees (8.1234567°, not 81234567°)
*/
__EXPORT static void map_projection_reproject(float x, float y, double *lat, double *lon)
{
/* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */
double x_descaled = x / scale;
double y_descaled = y / scale;
double c = sqrt(pow(x_descaled, 2) + pow(y_descaled, 2));
double sin_c = sin(c);
double cos_c = cos(c);
double lat_sphere = 0;
if (c != 0)
lat_sphere = asin(cos_c * sin_phi_1 + (x_descaled * sin_c * cos_phi_1) / c);
else
lat_sphere = asin(cos_c * sin_phi_1);
// printf("lat_sphere = %.10f\n",lat_sphere);
double lon_sphere = 0;
if (phi_1 == M_PI / 2) {
//using small angle approximation (formula in comment is without aproximation)
lon_sphere = (lambda_0 - y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(-y_descaled, x_descaled));
} else if (phi_1 == -M_PI / 2) {
//using small angle approximation (formula in comment is without aproximation)
lon_sphere = (lambda_0 + y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(y_descaled, x_descaled));
} else {
lon_sphere = (lambda_0 + atan2(y_descaled * sin_c , c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c));
//using small angle approximation
// double denominator = (c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c);
// if(denominator != 0)
// {
// lon_sphere = (lambda_0 + (y_descaled * sin_c) / denominator);
// }
// else
// {
// ...
// }
}
// printf("lon_sphere = %.10f\n",lon_sphere);
*lat = lat_sphere * 180.0 / M_PI;
*lon = lon_sphere * 180.0 / M_PI;
}
__EXPORT float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
{
double lat_now_rad = lat_now / 180.0d * M_PI;
+7 -1
View File
@@ -55,6 +55,12 @@ typedef struct {
float bearing; // Bearing in radians to closest point on line/arc
} crosstrack_error_s;
__EXPORT static void map_projection_init(double lat_0, double lon_0);
__EXPORT static void map_projection_project(double lat, double lon, float *x, float *y);
__EXPORT static void map_projection_reproject(float x, float y, double *lat, double *lon);
__EXPORT float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next);
__EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next);
@@ -69,4 +75,4 @@ __EXPORT crosstrack_error_s get_distance_to_arc(double lat_now, double lon_now,
float _wrap180(float bearing);
float _wrap360(float bearing);
float _wrapPI(float bearing);
float _wrap2PI(float bearing);
float _wrap2PI(float bearing);
+2 -2
View File
@@ -172,9 +172,9 @@ __EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, flo
// Calculate the output. Limit output magnitude to pid->limit
float output = (pid->error_previous * pid->kp) + (i * pid->ki) + (d * pid->kd);
//if (output > pid->limit) output = pid->limit;
if (output > pid->limit) output = pid->limit;
//if (output < -pid->limit) output = -pid->limit;
if (output < -pid->limit) output = -pid->limit;
if (isfinite(output)) {
pid->last_output = output;
+1 -13
View File
@@ -50,14 +50,6 @@
* @{
*/
enum RC_CHANNELS_STATUS
{
UNKNOWN = 0,
KNOWN = 1,
SIGNAL = 2,
TIMEOUT = 3
};
/**
* This defines the mapping of the RC functions.
* The value assigned to the specific function corresponds to the entry of
@@ -85,12 +77,7 @@ struct rc_channels_s {
uint64_t timestamp; /**< In microseconds since boot time. */
uint64_t timestamp_last_valid; /**< timestamp of last valid RC signal. */
struct {
uint16_t mid; /**< midpoint (0). */
float scaling_factor; /**< scaling factor from raw counts to -1..+1 */
uint16_t raw; /**< current raw value */
float scaled; /**< Scaled to -1..1 (throttle: 0..1) */
uint16_t override;
enum RC_CHANNELS_STATUS status; /**< status of the channel */
} chan[RC_CHANNELS_FUNCTION_MAX];
uint8_t chan_count; /**< maximum number of valid channels */
@@ -98,6 +85,7 @@ struct rc_channels_s {
char function_name[RC_CHANNELS_FUNCTION_MAX][20];
uint8_t function[RC_CHANNELS_FUNCTION_MAX];
uint8_t rssi; /**< Overall receive signal strength */
bool is_valid; /**< Inputs are valid, no timeout */
}; /**< radio control channels. */
/**
+4 -2
View File
@@ -155,6 +155,8 @@ CONFIG_STM32_ADC3=n
# CONFIG_USARTn_PARTIY - 0=no parity, 1=odd parity, 2=even parity
# CONFIG_USARTn_2STOP - Two stop bits
#
CONFIG_SERIAL_TERMIOS=y
CONFIG_USART1_SERIAL_CONSOLE=y
CONFIG_USART2_SERIAL_CONSOLE=n
CONFIG_USART3_SERIAL_CONSOLE=n
@@ -163,11 +165,11 @@ CONFIG_USART1_TXBUFSIZE=32
CONFIG_USART2_TXBUFSIZE=32
CONFIG_USART3_TXBUFSIZE=32
CONFIG_USART1_RXBUFSIZE=32
CONFIG_USART1_RXBUFSIZE=64
CONFIG_USART2_RXBUFSIZE=128
CONFIG_USART3_RXBUFSIZE=32
CONFIG_USART1_BAUD=57600
CONFIG_USART1_BAUD=115200
CONFIG_USART2_BAUD=115200
CONFIG_USART3_BAUD=115200