ardupilot/libraries/SITL/SIM_GPS_SBP.cpp

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#include "SIM_GPS_SBP.h"
#if AP_SIM_GPS_SBP_ENABLED
#include <SITL/SITL.h>
using namespace SITL;
void GPS_SBP::publish(const GPS_Data *d)
{
struct sbp_heartbeat_t {
bool sys_error : 1;
bool io_error : 1;
bool nap_error : 1;
uint8_t res : 5;
uint8_t protocol_minor : 8;
uint8_t protocol_major : 8;
uint8_t res2 : 7;
bool ext_antenna : 1;
} hb; // 4 bytes
struct PACKED sbp_gps_time_t {
uint16_t wn; //< GPS week number
uint32_t tow; //< GPS Time of Week rounded to the nearest ms
int32_t ns; //< Nanosecond remainder of rounded tow
uint8_t flags; //< Status flags (reserved)
} t;
struct PACKED sbp_pos_llh_t {
uint32_t tow; //< GPS Time of Week
double lat; //< Latitude
double lon; //< Longitude
double height; //< Height
uint16_t h_accuracy; //< Horizontal position accuracy estimate
uint16_t v_accuracy; //< Vertical position accuracy estimate
uint8_t n_sats; //< Number of satellites used in solution
uint8_t flags; //< Status flags
} pos;
struct PACKED sbp_vel_ned_t {
uint32_t tow; //< GPS Time of Week
int32_t n; //< Velocity North coordinate
int32_t e; //< Velocity East coordinate
int32_t d; //< Velocity Down coordinate
uint16_t h_accuracy; //< Horizontal velocity accuracy estimate
uint16_t v_accuracy; //< Vertical velocity accuracy estimate
uint8_t n_sats; //< Number of satellites used in solution
uint8_t flags; //< Status flags (reserved)
} velned;
struct PACKED sbp_dops_t {
uint32_t tow; //< GPS Time of Week
uint16_t gdop; //< Geometric Dilution of Precision
uint16_t pdop; //< Position Dilution of Precision
uint16_t tdop; //< Time Dilution of Precision
uint16_t hdop; //< Horizontal Dilution of Precision
uint16_t vdop; //< Vertical Dilution of Precision
uint8_t flags; //< Status flags (reserved)
} dops;
static const uint16_t SBP_HEARTBEAT_MSGTYPE = 0xFFFF;
static const uint16_t SBP_GPS_TIME_MSGTYPE = 0x0100;
static const uint16_t SBP_DOPS_MSGTYPE = 0x0206;
static const uint16_t SBP_POS_LLH_MSGTYPE = 0x0201;
static const uint16_t SBP_VEL_NED_MSGTYPE = 0x0205;
const auto gps_tow = gps_time();
t.wn = gps_tow.week;
t.tow = gps_tow.ms;
t.ns = 0;
t.flags = 0;
sbp_send_message(SBP_GPS_TIME_MSGTYPE, 0x2222, sizeof(t), (uint8_t*)&t);
if (!d->have_lock) {
return;
}
pos.tow = gps_tow.ms;
pos.lon = d->longitude;
pos.lat= d->latitude;
pos.height = d->altitude;
pos.h_accuracy = d->horizontal_acc*1000;
pos.v_accuracy = d->vertical_acc*1000;
pos.n_sats = d->have_lock ? d->num_sats : 3;
// Send single point position solution
pos.flags = 0;
sbp_send_message(SBP_POS_LLH_MSGTYPE, 0x2222, sizeof(pos), (uint8_t*)&pos);
// Send "pseudo-absolute" RTK position solution
pos.flags = 1;
sbp_send_message(SBP_POS_LLH_MSGTYPE, 0x2222, sizeof(pos), (uint8_t*)&pos);
velned.tow = gps_tow.ms;
velned.n = 1e3 * d->speedN;
velned.e = 1e3 * d->speedE;
velned.d = 1e3 * d->speedD;
velned.h_accuracy = 5e3;
velned.v_accuracy = 5e3;
velned.n_sats = d->have_lock ? d->num_sats : 3;
velned.flags = 0;
sbp_send_message(SBP_VEL_NED_MSGTYPE, 0x2222, sizeof(velned), (uint8_t*)&velned);
static uint32_t do_every_count = 0;
if (do_every_count % 5 == 0) {
dops.tow = gps_tow.ms;
dops.gdop = 1;
dops.pdop = 1;
dops.tdop = 1;
dops.hdop = 100;
dops.vdop = 1;
dops.flags = 1;
sbp_send_message(SBP_DOPS_MSGTYPE, 0x2222, sizeof(dops),
(uint8_t*)&dops);
hb = {};
hb.protocol_major = 0; //Sends protocol version 0
sbp_send_message(SBP_HEARTBEAT_MSGTYPE, 0x2222, sizeof(hb),
(uint8_t*)&hb);
}
do_every_count++;
}
#endif // AP_SIM_GPS_SBP_ENABLED