File content as of revision 0:3fb5ae3480ae:

#include "mbed.h"

#include "PQ_EEPROM.h"

Serial pc(USBTX, USBRX, 115200);

I2C i2c(p28, p27);

EEPROM eeprom(i2c);

char data[128];

char *phase_names[] =  {"SAFETY", "READY", "FLIGHT", "SEP", "EMERGENCY", "RECOVERY"};

int mission_time;
float flight_time;
char phase;
char f_launched;
char f_burning;
char f_apogee;
char f_mission;
char f_relay;
char f_flight_pin;
char f_sep;
char f_buzzer;
char f_sd;
char f_gps;
char f_adxl;
char f_ina_in;
char f_ina_ex;
char f_lps;
char f_mpu;
char f_mpu_ak;
float lat;
float lon;
int sat;
int fix;
float hdop;
float alt;
float geoid;
float high_accel[3];
float voltage_in;
float current_in;
float voltage_ex;
float current_ex;
float press;
float temp;
float accel[3];
float gyro[3];
float mag[3];

int mission_hour, mission_min, mission_sec;

int main()
{
    for(int addr = 0x000000; addr < 0x07FFFF; addr += 0x80) {
        eeprom.read(addr, data, 128);
        mission_time = *(int*)&data[0];
        flight_time = *(float*)&data[4];
        phase = *(float*)&data[8];
        f_launched = *(float*)&data[9];
        f_burning = *(float*)&data[10];
        f_apogee = *(float*)&data[11];
        f_mission = *(float*)&data[12];
        f_relay = *(float*)&data[13];
        f_flight_pin = *(float*)&data[14];
        f_sep = *(float*)&data[15];
        f_buzzer = *(float*)&data[16];
        f_sd = *(float*)&data[17];
        f_gps = *(float*)&data[18];
        f_adxl = *(float*)&data[19];
        f_ina_in = *(float*)&data[20];
        f_ina_ex = *(float*)&data[21];
        f_lps = *(float*)&data[22];
        f_mpu = *(float*)&data[23];
        f_mpu_ak = *(float*)&data[24];
        lat = *(float*)&data[25];
        lon = *(float*)&data[29];
        sat = *(float*)&data[33];
        fix = *(float*)&data[37];
        hdop = *(float*)&data[41];
        alt = *(float*)&data[45];
        geoid = *(float*)&data[49];
        high_accel[0] = *(float*)&data[53];
        high_accel[1] = *(float*)&data[57];
        high_accel[2] = *(float*)&data[61];
        voltage_in = *(float*)&data[65];
        current_in = *(float*)&data[69];
        voltage_ex = *(float*)&data[73];
        current_ex = *(float*)&data[77];
        press = *(float*)&data[81];
        temp = *(float*)&data[85];
        accel[0] = *(float*)&data[89];
        accel[1] = *(float*)&data[93];
        accel[2] = *(float*)&data[97];
        gyro[0] = *(float*)&data[101];
        gyro[1] = *(float*)&data[105];
        gyro[2] = *(float*)&data[109];
        mag[0] = *(float*)&data[113];
        mag[1] = *(float*)&data[117];
        mag[2] = *(float*)&data[121];
        
        
        mission_hour = mission_time / 3600;
        mission_time %= 3600;
        mission_min = mission_time / 60;
        mission_time %= 60;
        mission_sec = mission_time;

        pc.printf(" mission time:\t%02d:%02d:%02d\r\n", mission_hour, mission_min, mission_sec);
        pc.printf(" flight time:\t%.3f[s]\r\n", flight_time);
        pc.printf(" phase:\t%s\r\n", phase_names[phase]);
        pc.printf(" flags:\tLAUNCH\tBURNING\tAPOGEE\tMISSION\tRELAY\tFLIGHT\tSEP\tBUZZER\r\n");
        pc.printf("       \t%d\t%d\t%d\t%d\t%d\t%d\t%d\t%d\r\n", f_launched, f_burning, f_apogee, f_mission, f_relay, f_flight_pin, f_sep, f_buzzer);
        pc.printf(" flags:\tSD\tGPS\tADXL\tINA_in\tINA_ex\tLPS\tMPU\tMPU_AK\r\n");
        pc.printf("       \t%d\t%d\t%d\t%d\t%d\t%d\t%d\t%d\r\n", f_sd, f_gps, f_adxl, f_ina_in, f_ina_ex, f_lps, f_mpu, f_mpu_ak);
        pc.printf("\r\n");
        pc.printf(" lat:\t\t%.6f\r\n", lat);
        pc.printf(" lon:\t\t%.6f\r\n", lon);
        pc.printf(" alt:\t\t%.1f[m]\r\n", alt);
        pc.printf("\r\n");
        pc.printf(" internal:\tvoltage\t\tcurrent\r\n");
        pc.printf("          \t%.2f[V]\t\t%.0f[mA]\r\n", voltage_in / 1000.0f, current_in);
        pc.printf(" external:\tvoltage\t\tcurrent\r\n");
        pc.printf("          \t%.2f[V]\t\t%.0f[mA]\r\n", voltage_ex / 1000.0f, current_ex);
        pc.printf("\r\n");
        pc.printf(" press:\t\t%.2f[hPa]\r\n", press);
        pc.printf(" temp:\t\t%.2f[C]\r\n", temp);
        pc.printf("\r\n");
        pc.printf(" high_accel:\tx\t\ty\t\tz\r\n");
        pc.printf("       \t\t%.2f\t\t%.2f\t\t%.2f\t[G]\r\n", high_accel[0], high_accel[1], high_accel[2]);
        pc.printf(" accel:\t\tx\t\ty\t\tz\r\n");
        pc.printf("       \t\t%.2f\t\t%.2f\t\t%.2f\t[G]\r\n", accel[0], accel[1], accel[2]);
        pc.printf(" gyro:\t\tx\t\ty\t\tz\r\n");
        pc.printf("       \t\t%.2f\t\t%.2f\t\t%.2f\t[rad/s]\r\n", gyro[0], gyro[1], gyro[2]);
    }
}