ardupilot/libraries/AP_NavEKF/examples/AP_NavEKF/LogReader.cpp

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#include <AP_HAL.h>
#include <AP_Common.h>
#include <AP_Math.h>
#include <AP_Airspeed.h>
#include <AP_Compass.h>
#include <AP_GPS.h>
#include <AP_Compass.h>
#include <AP_Baro.h>
#include <AP_InertialSensor.h>
#include <DataFlash.h>
#include "LogReader.h"
#include <stdio.h>
#include <unistd.h>
#include <sys/types.h>
#include <sys/stat.h>
#include <fcntl.h>
extern const AP_HAL::HAL& hal;
LogReader::LogReader(AP_InertialSensor &_ins, AP_Baro_HIL &_baro, AP_Compass_HIL &_compass, GPS *&_gps) :
fd(-1),
ins(_ins),
baro(_baro),
compass(_compass),
gps(_gps)
{}
bool LogReader::open_log(const char *logfile)
{
fd = ::open(logfile, O_RDONLY);
if (fd == -1) {
return false;
}
return true;
}
struct PACKED log_Compass {
LOG_PACKET_HEADER;
uint32_t time_ms;
int16_t mag_x;
int16_t mag_y;
int16_t mag_z;
int16_t offset_x;
int16_t offset_y;
int16_t offset_z;
};
struct PACKED log_Nav_Tuning {
LOG_PACKET_HEADER;
uint32_t time_ms;
uint16_t yaw;
uint32_t wp_distance;
uint16_t target_bearing_cd;
uint16_t nav_bearing_cd;
int16_t altitude_error_cm;
int16_t airspeed_cm;
float altitude;
uint32_t groundspeed_cm;
};
struct PACKED log_Attitude {
LOG_PACKET_HEADER;
uint32_t time_ms;
int16_t roll;
int16_t pitch;
uint16_t yaw;
uint16_t error_rp;
uint16_t error_yaw;
};
bool LogReader::update(uint8_t &type)
{
uint8_t hdr[3];
if (::read(fd, hdr, 3) != 3) {
return false;
}
if (hdr[0] != HEAD_BYTE1 || hdr[1] != HEAD_BYTE2) {
return false;
}
if (hdr[2] == LOG_FORMAT_MSG) {
struct log_Format &f = formats[num_formats];
memcpy(&f, hdr, 3);
if (::read(fd, &f.type, sizeof(f)-3) != sizeof(f)-3) {
return false;
}
num_formats++;
type = f.type;
return true;
}
uint8_t i;
for (i=0; i<num_formats; i++) {
if (formats[i].type == hdr[2]) break;
}
if (i == num_formats) {
return false;
}
const struct log_Format &f = formats[i];
uint8_t data[f.length];
memcpy(data, hdr, 3);
if (::read(fd, &data[3], f.length-3) != f.length-3) {
return false;
}
switch (f.type) {
case LOG_IMU_MSG: {
struct log_IMU msg;
memcpy(&msg, data, sizeof(msg));
wait_timestamp(msg.timestamp);
ins.set_gyro(Vector3f(msg.gyro_x, msg.gyro_y, msg.gyro_z));
ins.set_accel(Vector3f(msg.accel_x, msg.accel_y, msg.accel_z));
break;
}
case LOG_GPS_MSG: {
struct log_GPS msg;
memcpy(&msg, data, sizeof(msg));
wait_timestamp(msg.apm_time);
gps->setHIL(msg.apm_time,
msg.latitude*1.0e-7f,
msg.longitude*1.0e-7f,
msg.altitude*1.0e-2f,
msg.ground_speed*1.0e-2f,
msg.ground_course*1.0e-2f,
0,
msg.status==3?msg.num_sats:0);
if (msg.status == 3 && ground_alt_cm == 0) {
ground_alt_cm = msg.altitude;
}
baro.setHIL((ground_alt_cm + msg.rel_altitude)*1.0e-2f);
break;
}
case LOG_COMPASS_MSG: {
struct log_Compass msg;
memcpy(&msg, data, sizeof(msg));
wait_timestamp(msg.time_ms);
//compass.setHIL(Vector3i(msg.mag_x - msg.offset_x, msg.mag_y - msg.offset_y, msg.mag_z - msg.offset_z));
compass.setHIL(Vector3i(msg.mag_x, msg.mag_y, msg.mag_z));
break;
}
case LOG_ATTITUDE_MSG: {
struct log_Attitude msg;
memcpy(&msg, data, sizeof(msg));
wait_timestamp(msg.time_ms);
attitude = Vector3f(msg.roll*0.01f, msg.pitch*0.01f, msg.yaw*0.01f);
break;
}
}
type = f.type;
return true;
}
void LogReader::wait_timestamp(uint32_t timestamp)
{
hal.scheduler->stop_clock(timestamp);
}
bool LogReader::wait_type(uint8_t wtype)
{
while (true) {
uint8_t type;
if (!update(type)) {
return false;
}
if (wtype == type) {
break;
}
}
return true;
}