Iridium driver and support

Mavlink module implement HIGH_LATENCY (Iridium)
This commit is contained in:
Daniel Agar
2016-11-18 14:59:07 -05:00
committed by Lorenz Meier
parent 77e482a30e
commit bce7ecb0f6
14 changed files with 1450 additions and 16 deletions
+5
View File
@@ -600,6 +600,11 @@ then
then
mavlink start -d $MAVLINK_COMPANION_DEVICE -b 57600 -r 1000
fi
if param compare SYS_COMPANION 419200
then
iridiumsbd start -d /dev/ttyS2
mavlink start -d /dev/iridium -b 19200 -m iridium -r 10
fi
if param compare SYS_COMPANION 1921600
then
mavlink start -d $MAVLINK_COMPANION_DEVICE -b 921600 -r 20000
@@ -48,6 +48,7 @@ set(config_module_list
drivers/bst
#drivers/snapdragon_rc_pwm
drivers/lis3mdl
drivers/iridiumsbd
#
# System commands
@@ -23,6 +23,7 @@ set(config_module_list
drivers/hott
drivers/hott/hott_sensors
drivers/hott/hott_telemetry
drivers/iridiumsbd
drivers/l3gd20
drivers/led
drivers/lis3mdl
@@ -50,6 +50,7 @@ set(config_module_list
drivers/bma180
drivers/bmi160
drivers/tap_esc
drivers/iridiumsbd
#
# System commands
+1
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@@ -3,6 +3,7 @@ uint8 TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO = 1
uint8 TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET = 2
uint8 TELEMETRY_STATUS_RADIO_TYPE_WIRE = 3
uint8 TELEMETRY_STATUS_RADIO_TYPE_USB = 4
uint8 TELEMETRY_STATUS_RADIO_TYPE_IRIDIUM = 5
uint64 heartbeat_time # Time of last received heartbeat from remote system
uint64 telem_time # Time of last received telemetry status packet, 0 for none
+8
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@@ -0,0 +1,8 @@
#pragma once
#include <stdint.h>
#include <sys/ioctl.h>
#include "board_config.h"
#define IRIDIUMSBD_DEVICE_PATH "/dev/iridium"
+45
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@@ -0,0 +1,45 @@
############################################################################
#
# Copyright (c) 2016 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.
#
############################################################################
px4_add_module(
MODULE drivers__iridiumsbd
MAIN iridiumsbd
STACK 1024
STACK_MAIN 1024
COMPILE_FLAGS
-Os
SRCS
IridiumSBD.cpp
iridiumsbd_params.c
DEPENDS
platforms__common
)
File diff suppressed because it is too large Load Diff
+283
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@@ -0,0 +1,283 @@
/****************************************************************************
*
* Copyright (c) 2016 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.
*
****************************************************************************/
#pragma once
#include <stdlib.h>
#include <stdbool.h>
#include <drivers/device/device.h>
#include <drivers/drv_hrt.h>
#include <uORB/uORB.h>
#include <uORB/topics/telemetry_status.h>
typedef enum {
SATCOM_OK = 0,
SATCOM_NO_MSG = -1,
SATCOM_ERROR = -255,
} satcom_status;
typedef enum {
SATCOM_UART_OK = 0,
SATCOM_UART_OPEN_FAIL = -1,
} satcom_uart_status;
typedef enum {
SATCOM_READ_OK = 0,
SATCOM_READ_TIMEOUT = -1,
SATCOM_READ_PARSING_FAIL = -2,
} satcom_read_status;
typedef enum {
SATCOM_RESULT_OK,
SATCOM_RESULT_ERROR,
SATCOM_RESULT_SBDRING,
SATCOM_RESULT_READY,
SATCOM_RESULT_HWFAIL,
SATCOM_RESULT_NA,
} satcom_result_code;
//typedef struct
//{
// uint8_t info;
// uint8_t result_code;
//} satcom_at_msg;
typedef enum {
SATCOM_STATE_STANDBY,
SATCOM_STATE_CSQ,
SATCOM_STATE_SBDSESSION,
SATCOM_STATE_TEST,
} satcom_state;
const char *satcom_state_string[4] = {"STANDBY", "SIGNAL CHECK", "SBD SESSION", "TEST"};
extern "C" __EXPORT int iridiumsbd_main(int argc, char *argv[]);
#define SATCOM_TX_BUF_LEN 50 // TX buffer size - maximum for a SBD MO message is 340, but billed per 50
#define SATCOM_RX_MSG_BUF_LEN 300 // RX buffer size for MT messages
#define SATCOM_RX_COMMAND_BUF_LEN 50 // RX buffer size for other commands
#define SATCOM_TX_STACKING_TIME 3000000 // time to wait for additional mavlink messages, TODO make this a param
#define SATCOM_SIGNAL_REFRESH_DELAY 5000000 // update signal quality every 5s
class IridiumSBD : public device::CDev
{
public:
static IridiumSBD *instance;
static int task_handle;
bool task_should_exit = false;
int uart_fd = -1;
int param_read_interval_s;
hrt_abstime last_signal_check = 0;
uint8_t signal_quality = 0;
orb_advert_t telemetry_status_pub = nullptr;
bool test_pending = false;
char test_command[32];
hrt_abstime test_timer = 0;
uint8_t rx_command_buf[SATCOM_RX_COMMAND_BUF_LEN] = {0};
int rx_command_len = 0;
uint8_t rx_msg_buf[SATCOM_RX_MSG_BUF_LEN] = {0};
int rx_msg_end_idx = 0;
int rx_msg_read_idx = 0;
uint8_t tx_buf[SATCOM_TX_BUF_LEN] = {0};
int tx_buf_write_idx = 0;
bool ring_pending = false;
bool rx_session_pending = false;
bool rx_read_pending = false;
bool tx_session_pending = false;
hrt_abstime last_write_time = 0;
hrt_abstime last_read_time = 0;
satcom_state state = SATCOM_STATE_STANDBY;
satcom_state new_state = SATCOM_STATE_STANDBY;
pthread_mutex_t tx_buf_mutex = pthread_mutex_t();
bool verbose = false;
/*
* Constructor
*/
IridiumSBD();
/*
* Start the driver
*/
static int start(int argc, char *argv[]);
/*
* Stop the driver
*/
static int stop();
/*
* Display driver status
*/
static void status();
/*
* Run a basic driver test
*/
static void test(int argc, char *argv[]);
/*
* Entry point of the task, has to be a static function
*/
static void main_loop_helper(int argc, char *argv[]);
/*
* Main driver loop
*/
void main_loop(int argc, char *argv[]);
/*
* Use to send mavlink messages directly
*/
ssize_t write(struct file *filp, const char *buffer, size_t buflen);
/*
* Use to read received mavlink messages directly
*/
ssize_t read(struct file *filp, char *buffer, size_t buflen);
/*
* Passes everything to CDev
*/
int ioctl(struct file *filp, int cmd, unsigned long arg);
/*
* Get the poll state
*/
pollevent_t poll_state(struct file *filp);
/*
* Open and configure the given UART port
*/
satcom_uart_status open_uart(char *uart_name);
/*
*
*/
void write_tx_buf();
/*
*
*/
void read_rx_buf();
/*
*
*/
bool clear_mo_buffer();
/*
* Perform a SBD session, sending the message from the MO buffer (if previously written)
* and retrieving a MT message from the Iridium system (if there is one waiting)
* This will also update the registration needed for SBD RING
*/
int sbd_session(void);
/*
* Get the network signal strength
*/
void start_csq(void);
/*
*
*/
satcom_result_code read_at_command();
/*
*
*/
satcom_result_code read_at_msg();
/*
*
*/
satcom_result_code read_at(uint8_t *rx_buf, int *rx_len);
/*
*
*/
void schedule_test(void);
/*
*
*/
void standby_loop(void);
/*
*
*/
void csq_loop(void);
/*
*
*/
void sbdsession_loop(void);
/*
*
*/
void test_loop(void);
/*
* TEST
*/
void start_test(void);
/*
*
*/
void start_sbd_session(void);
/*
* Checks if the modem responds to the "AT" command
*/
bool is_modem_ready(void);
/*
* Send a AT command to the modem
*/
void write_at(const char *command);
};
@@ -0,0 +1,11 @@
#include <systemlib/param/param.h>
/**
* Satellite radio read interval
*
* @unit s
* @min 0
* @max 300
* @group Iridium SBD
*/
PARAM_DEFINE_INT32(ISBD_READINT, 10);
+20 -7
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@@ -1818,6 +1818,10 @@ Mavlink::task_main(int argc, char *argv[])
} else if (strcmp(myoptarg, "config") == 0) {
_mode = MAVLINK_MODE_CONFIG;
} else if (strcmp(myoptarg, "iridium") == 0) {
_mode = MAVLINK_MODE_IRIDIUM;
_rstatus.type = telemetry_status_s::TELEMETRY_STATUS_RADIO_TYPE_IRIDIUM;
}
break;
@@ -1935,14 +1939,18 @@ Mavlink::task_main(int argc, char *argv[])
/* add default streams depending on mode */
/* HEARTBEAT is constant rate stream, rate never adjusted */
configure_stream("HEARTBEAT", 1.0f);
if (_mode != MAVLINK_MODE_IRIDIUM) {
/* STATUSTEXT stream is like normal stream but gets messages from logbuffer instead of uORB */
configure_stream("STATUSTEXT", 20.0f);
/* HEARTBEAT is constant rate stream, rate never adjusted */
configure_stream("HEARTBEAT", 1.0f);
/* COMMAND_LONG stream: use high rate to avoid commands skipping */
configure_stream("COMMAND_LONG", 100.0f);
/* STATUSTEXT stream is like normal stream but gets messages from logbuffer instead of uORB */
configure_stream("STATUSTEXT", 20.0f);
/* COMMAND_LONG stream: use high rate to avoid commands skipping */
configure_stream("COMMAND_LONG", 100.0f);
}
/* PARAM_VALUE stream */
_parameters_manager = (MavlinkParametersManager *) MavlinkParametersManager::new_instance(this);
@@ -2078,6 +2086,11 @@ Mavlink::task_main(int argc, char *argv[])
configure_stream("MISSION_ITEM", 50.0f);
configure_stream("ACTUATOR_CONTROL_TARGET0", 30.0f);
configure_stream("MANUAL_CONTROL", 5.0f);
break;
case MAVLINK_MODE_IRIDIUM:
configure_stream("HIGH_LATENCY", 0.1f);
break;
default:
break;
@@ -2441,7 +2454,7 @@ Mavlink::start(int argc, char *argv[])
px4_task_spawn_cmd(buf,
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT,
2400,
2500,
(px4_main_t)&Mavlink::start_helper,
(char *const *)argv);
+5 -9
View File
@@ -163,7 +163,8 @@ public:
MAVLINK_MODE_ONBOARD,
MAVLINK_MODE_OSD,
MAVLINK_MODE_MAGIC,
MAVLINK_MODE_CONFIG
MAVLINK_MODE_CONFIG,
MAVLINK_MODE_IRIDIUM
};
enum BROADCAST_MODE {
@@ -191,6 +192,9 @@ public:
case MAVLINK_MODE_CONFIG:
return "Config";
case MAVLINK_MODE_IRIDIUM:
return "Iridium";
default:
return "Unknown";
}
@@ -232,14 +236,6 @@ public:
static int start_helper(int argc, char *argv[]);
/**
* Handle parameter related messages.
*/
void mavlink_pm_message_handler(const mavlink_channel_t chan, const mavlink_message_t *msg);
void get_mavlink_mode_and_state(struct vehicle_status_s *status, struct position_setpoint_triplet_s *pos_sp_triplet,
uint8_t *mavlink_state, uint8_t *mavlink_base_mode, uint32_t *mavlink_custom_mode);
/**
* Enable / disable Hardware in the Loop simulation mode.
*
+205
View File
@@ -3592,6 +3592,210 @@ protected:
}
};
class MavlinkStreamHighLatency : public MavlinkStream
{
public:
const char *get_name() const
{
return MavlinkStreamHighLatency::get_name_static();
}
static const char *get_name_static()
{
return "HIGH_LATENCY";
}
static uint16_t get_id_static()
{
return MAVLINK_MSG_ID_HIGH_LATENCY;
}
uint16_t get_id()
{
return get_id_static();
}
static MavlinkStream *new_instance(Mavlink *mavlink)
{
return new MavlinkStreamHighLatency(mavlink);
}
unsigned get_size()
{
return MAVLINK_MSG_ID_HIGH_LATENCY_LEN + MAVLINK_NUM_NON_PAYLOAD_BYTES;
}
private:
MavlinkOrbSubscription *_actuator_sub;
uint64_t _actuator_time;
MavlinkOrbSubscription *_airspeed_sub;
uint64_t _airspeed_time;
MavlinkOrbSubscription *_attitude_sp_sub;
uint64_t _attitude_sp_time;
MavlinkOrbSubscription *_attitude_sub;
uint64_t _attitude_time;
MavlinkOrbSubscription *_battery_sub;
uint64_t _battery_time;
MavlinkOrbSubscription *_fw_pos_ctrl_status_sub;
uint64_t _fw_pos_ctrl_status_time;
MavlinkOrbSubscription *_global_pos_sub;
uint64_t _global_pos_time;
MavlinkOrbSubscription *_gps_sub;
uint64_t _gps_time;
MavlinkOrbSubscription *_home_sub;
uint64_t _home_time;
MavlinkOrbSubscription *_landed_sub;
uint64_t _landed_time;
MavlinkOrbSubscription *_mission_result_sub;
uint64_t _mission_result_time;
MavlinkOrbSubscription *_sensor_sub;
uint64_t _sensor_time;
MavlinkOrbSubscription *_status_sub;
uint64_t _status_time;
MavlinkOrbSubscription *_tecs_status_sub;
uint64_t _tecs_time;
MavlinkOrbSubscription *_wind_sub;
uint64_t _wind_time;
/* do not allow top copying this class */
MavlinkStreamHighLatency(MavlinkStreamHighLatency &);
MavlinkStreamHighLatency& operator = (const MavlinkStreamHighLatency &);
protected:
explicit MavlinkStreamHighLatency(Mavlink *mavlink) : MavlinkStream(mavlink),
_actuator_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))),
_actuator_time(0),
_airspeed_sub(_mavlink->add_orb_subscription(ORB_ID(airspeed))),
_airspeed_time(0),
_attitude_sp_sub(_mavlink->add_orb_subscription(ORB_ID(fw_pos_ctrl_status))),
_attitude_sp_time(0),
_attitude_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_attitude))),
_attitude_time(0),
_battery_sub(_mavlink->add_orb_subscription(ORB_ID(battery_status))),
_battery_time(0),
_fw_pos_ctrl_status_sub(_mavlink->add_orb_subscription(ORB_ID(fw_pos_ctrl_status))),
_fw_pos_ctrl_status_time(0),
_global_pos_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_global_position))),
_global_pos_time(0),
_gps_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_gps_position))),
_gps_time(0),
_home_sub(_mavlink->add_orb_subscription(ORB_ID(home_position))),
_home_time(0),
_landed_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_land_detected))),
_landed_time(0),
_mission_result_sub(_mavlink->add_orb_subscription(ORB_ID(mission_result))),
_mission_result_time(0),
_sensor_sub(_mavlink->add_orb_subscription(ORB_ID(sensor_combined))),
_sensor_time(0),
_status_sub(_mavlink->add_orb_subscription(ORB_ID(vehicle_status))),
_status_time(0),
_tecs_status_sub(_mavlink->add_orb_subscription(ORB_ID(tecs_status))),
_tecs_time(0)
{}
void send(const hrt_abstime t)
{
struct actuator_controls_s actuator = {};
struct airspeed_s airspeed = {};
struct battery_status_s battery = {};
struct fw_pos_ctrl_status_s fw_pos_ctrl_status = {};
struct home_position_s home = {};
struct mission_result_s mission_result = {};
struct sensor_combined_s sensor = {};
struct tecs_status_s tecs_status = {};
struct vehicle_attitude_s attitude = {};
struct vehicle_attitude_setpoint_s attitude_sp = {};
struct vehicle_global_position_s global_pos = {};
struct vehicle_gps_position_s gps = {};
struct vehicle_land_detected_s land_detected = {};
struct vehicle_status_s status = {};
bool updated = _status_sub->update(&_status_time, &status);
updated |= _actuator_sub->update(&_actuator_time, &actuator);
updated |= _airspeed_sub->update(&_airspeed_time, &airspeed);
updated |= _attitude_sp_sub->update(&_attitude_sp_time, &attitude_sp);
updated |= _attitude_sub->update(&_attitude_time, &attitude);
updated |= _battery_sub->update(&_battery_time, &battery);
updated |= _fw_pos_ctrl_status_sub->update(&_fw_pos_ctrl_status_time, &fw_pos_ctrl_status);
updated |= _global_pos_sub->update(&_global_pos_time, &global_pos);
updated |= _gps_sub->update(&_gps_time, &gps);
updated |= _home_sub->update(&_home_time, &home);
updated |= _landed_sub->update(&_landed_time, &land_detected);
updated |= _mission_result_sub->update(&_mission_result_time, &mission_result);
updated |= _sensor_sub->update(&_sensor_time, &sensor);
updated |= _tecs_status_sub->update(&_tecs_time, &tecs_status);
if (updated) {
mavlink_high_latency_t msg = {};
//timespec tv;
//px4_clock_gettime(CLOCK_REALTIME, &tv);
//msg.time_usec = (uint64_t)tv.tv_sec * 1000000 + tv.tv_nsec / 1000;
msg.base_mode = 0;
msg.custom_mode = 0;
uint8_t sys_status;
get_mavlink_mode_state(&status, &sys_status, &msg.base_mode, &msg.custom_mode);
matrix::Eulerf euler = matrix::Quatf(attitude.q);
msg.roll = math::degrees(euler.phi()) * 100;
msg.pitch = math::degrees(euler.theta()) * 100;
msg.heading = math::degrees(_wrap_2pi(euler.psi())) * 100;
//msg.roll_sp = math::degrees(attitude_sp.roll_body) * 100;
//msg.pitch_sp = math::degrees(attitude_sp.pitch_body) * 100;
msg.heading_sp = math::degrees(_wrap_2pi(attitude_sp.yaw_body)) * 100;
if (status.arming_state == vehicle_status_s::ARMING_STATE_ARMED) {
msg.throttle = actuator.control[actuator_controls_s::INDEX_THROTTLE] * 100;
} else {
msg.throttle = 0;
}
msg.latitude = global_pos.lat * 1e7;
msg.longitude = global_pos.lon * 1e7;
//msg.altitude_home = (_home_time > 0) ? (global_pos.alt - home.alt) : NAN;
msg.altitude_amsl = (_global_pos_time > 0) ? global_pos.alt : NAN;
msg.altitude_sp = (_tecs_time > 0) ? (tecs_status.altitudeSp - home.alt) : NAN;
msg.airspeed = airspeed.indicated_airspeed_m_s * 100.0f;
msg.groundspeed = sqrtf(global_pos.vel_n * global_pos.vel_n + global_pos.vel_e * global_pos.vel_e) * 100.0f;
msg.climb_rate = -global_pos.vel_d;
msg.gps_nsat = gps.satellites_used;
msg.gps_fix_type = gps.fix_type;
msg.landed_state = land_detected.landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR;
msg.battery_remaining = (battery.connected) ? battery.remaining * 100.0f : -1;
msg.temperature = sensor.baro_temp_celcius;
msg.temperature_air = airspeed.air_temperature_celsius;
msg.wp_num = mission_result.seq_current;
msg.wp_distance = fw_pos_ctrl_status.wp_dist;
mavlink_msg_high_latency_send_struct(_mavlink->get_channel(), &msg);
}
}
};
const StreamListItem *streams_list[] = {
new StreamListItem(&MavlinkStreamHeartbeat::new_instance, &MavlinkStreamHeartbeat::get_name_static, &MavlinkStreamHeartbeat::get_id_static),
new StreamListItem(&MavlinkStreamStatustext::new_instance, &MavlinkStreamStatustext::get_name_static, &MavlinkStreamStatustext::get_id_static),
@@ -3638,5 +3842,6 @@ const StreamListItem *streams_list[] = {
new StreamListItem(&MavlinkStreamCollision::new_instance, &MavlinkStreamCollision::get_name_static, &MavlinkStreamCollision::get_id_static),
new StreamListItem(&MavlinkStreamWind::new_instance, &MavlinkStreamWind::get_name_static, &MavlinkStreamWind::get_id_static),
new StreamListItem(&MavlinkStreamMountOrientation::new_instance, &MavlinkStreamMountOrientation::get_name_static, &MavlinkStreamMountOrientation::get_id_static),
new StreamListItem(&MavlinkStreamHighLatency::new_instance, &MavlinkStreamHighLatency::get_name_static, &MavlinkStreamWind::get_id_static),
nullptr
};
+1
View File
@@ -121,6 +121,7 @@ PARAM_DEFINE_INT32(SYS_MC_EST_GROUP, 2);
* @value 319200 Normal Telemetry (19200 baud, 8N1)
* @value 338400 Normal Telemetry (38400 baud, 8N1)
* @value 357600 Normal Telemetry (57600 baud, 8N1)
* @value 419200 Iridium Telemetry (19200 baud, 8N1)
* @value 1921600 ESP8266 (921600 baud, 8N1)
*
* @min 0