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/*
* Copyright © 2009 Keith Packard <keithp@keithp.com>
*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 2 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
* General Public License for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
*/
#define _GNU_SOURCE
#include <string.h>
#include <stdio.h>
#include <stdlib.h>
#include <unistd.h>
#include <getopt.h>
#include "cc-usb.h"
#include "cc.h"
#define NUM_BLOCK 512
static const struct option options[] = {
{ 0, 0, 0, 0},
};
static void usage(char *program)
{
fprintf(stderr, "usage: %s {flight-log} ...\n", program);
exit(1);
}
static const char *state_names[] = {
"startup",
"idle",
"pad",
"boost",
"fast",
"coast",
"drogue",
"main",
"landed",
"invalid"
};
void
analyse_flight(struct cc_flightraw *f)
{
double height;
double accel;
double boost_start, boost_stop;
double min_pres;
int i;
int pres_i, accel_i;
int boost_start_set = 0;
int boost_stop_set = 0;
enum ao_flight_state state;
double state_start, state_stop;
printf ("Flight: %9d\nSerial: %9d\n",
f->flight, f->serial);
boost_start = f->accel.data[0].time;
boost_stop = f->accel.data[f->accel.num-1].time;
for (i = 0; i < f->state.num; i++) {
if (f->state.data[i].value == ao_flight_boost && !boost_start_set) {
boost_start = f->state.data[i].time;
boost_start_set = 1;
}
if (f->state.data[i].value > ao_flight_boost && !boost_stop_set) {
boost_stop = f->state.data[i].time;
boost_stop_set = 1;
}
}
pres_i = cc_timedata_min(&f->pres, f->pres.data[0].time,
f->pres.data[f->pres.num-1].time);
if (pres_i)
{
min_pres = f->pres.data[pres_i].value;
height = cc_barometer_to_altitude(min_pres) -
cc_barometer_to_altitude(f->ground_pres);
printf ("Max height: %9.2fm %9.2fft %9.2fs\n",
height, height * 100 / 2.54 / 12,
(f->pres.data[pres_i].time - boost_start) / 100.0);
}
accel_i = cc_timedata_min(&f->accel, boost_start, boost_stop);
if (accel_i)
{
accel = cc_accelerometer_to_acceleration(f->accel.data[accel_i].value,
f->ground_accel);
printf ("Max accel: %9.2fm/s² %9.2fg %9.2fs\n",
accel, accel / 9.80665,
(f->accel.data[accel_i].time - boost_start) / 100.0);
}
for (i = 0; i < f->state.num; i++) {
state = f->state.data[i].value;
state_start = f->state.data[i].time;
while (i < f->state.num - 1 && f->state.data[i+1].value == state)
i++;
if (i < f->state.num - 1)
state_stop = f->state.data[i + 1].time;
else
state_stop = f->accel.data[f->accel.num-1].time;
printf("State: %s\n", state_names[state]);
printf("\tStart: %9.2fs\n", (state_start - boost_start) / 100.0);
printf("\tDuration: %9.2fs\n", (state_stop - state_start) / 100.0);
accel_i = cc_timedata_min(&f->accel, state_start, state_stop);
if (accel_i >= 0)
{
accel = cc_accelerometer_to_acceleration(f->accel.data[accel_i].value,
f->ground_accel);
printf("\tMax accel: %9.2fm/s² %9.2fg %9.2fs\n",
accel, accel / 9.80665,
(f->accel.data[accel_i].time - boost_start) / 100.0);
}
pres_i = cc_timedata_min(&f->pres, state_start, state_stop);
if (pres_i >= 0)
{
min_pres = f->pres.data[pres_i].value;
height = cc_barometer_to_altitude(min_pres) -
cc_barometer_to_altitude(f->ground_pres);
printf ("\tMax height: %9.2fm %9.2fft %9.2fs\n",
height, height * 100 / 2.54 / 12,
(f->pres.data[pres_i].time - boost_start) / 100.0);
}
}
}
int
main (int argc, char **argv)
{
FILE *file;
int i;
int ret = 0;
struct cc_flightraw *raw;
int c;
int serial;
char *s;
while ((c = getopt_long(argc, argv, "", options, NULL)) != -1) {
switch (c) {
default:
usage(argv[0]);
break;
}
}
for (i = optind; i < argc; i++) {
file = fopen(argv[i], "r");
if (!file) {
perror(argv[i]);
ret++;
continue;
}
s = strstr(argv[i], "-serial-");
if (s)
serial = atoi(s + 8);
else
serial = 0;
raw = cc_log_read(file);
if (!raw) {
perror(argv[i]);
ret++;
continue;
}
if (!raw->serial)
raw->serial = serial;
analyse_flight(raw);
cc_flightraw_free(raw);
}
return ret;
}
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