Use autotools, move altos to src subdir
[fw/altos] / ao_flight_test.c
diff --git a/ao_flight_test.c b/ao_flight_test.c
deleted file mode 100644 (file)
index f4731aa..0000000
+++ /dev/null
@@ -1,288 +0,0 @@
-/*
- * 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; version 2 of the License.
- *
- * 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 <stdint.h>
-#include <stdio.h>
-#include <stdlib.h>
-#include <string.h>
-
-#define AO_ADC_RING    64
-#define ao_adc_ring_next(n)    (((n) + 1) & (AO_ADC_RING - 1))
-#define ao_adc_ring_prev(n)    (((n) - 1) & (AO_ADC_RING - 1))
-
-/*
- * One set of samples read from the A/D converter
- */
-struct ao_adc {
-       uint16_t        tick;           /* tick when the sample was read */
-       int16_t         accel;          /* accelerometer */
-       int16_t         pres;           /* pressure sensor */
-       int16_t         temp;           /* temperature sensor */
-       int16_t         v_batt;         /* battery voltage */
-       int16_t         sense_d;        /* drogue continuity sense */
-       int16_t         sense_m;        /* main continuity sense */
-};
-
-#define __pdata
-#define __data
-#define __xdata
-#define __code
-#define __reentrant
-
-enum ao_flight_state {
-       ao_flight_startup = 0,
-       ao_flight_idle = 1,
-       ao_flight_launchpad = 2,
-       ao_flight_boost = 3,
-       ao_flight_coast = 4,
-       ao_flight_apogee = 5,
-       ao_flight_drogue = 6,
-       ao_flight_main = 7,
-       ao_flight_landed = 8,
-       ao_flight_invalid = 9
-};
-
-struct ao_adc ao_adc_ring[AO_ADC_RING];
-uint8_t ao_adc_head;
-
-#define ao_led_on(l)
-#define ao_led_off(l)
-#define ao_timer_set_adc_interval(i)
-#define ao_wakeup(wchan) ao_dump_state()
-#define ao_cmd_register(c)
-#define ao_usb_disable()
-#define ao_telemetry_set_interval(x)
-
-enum ao_igniter {
-       ao_igniter_drogue = 0,
-       ao_igniter_main = 1
-};
-
-void
-ao_ignite(enum ao_igniter igniter)
-{
-       printf ("ignite %s\n", igniter == ao_igniter_drogue ? "drogue" : "main");
-}
-
-struct ao_task {
-       int dummy;
-};
-
-#define ao_add_task(t,f,n)
-
-#define ao_log_start()
-#define ao_log_stop()
-
-#define AO_MS_TO_TICKS(ms)     ((ms) / 10)
-#define AO_SEC_TO_TICKS(s)     ((s) * 100)
-
-#define AO_FLIGHT_TEST
-
-struct ao_adc ao_adc_static;
-
-FILE *emulator_in;
-
-void
-ao_dump_state(void);
-
-void
-ao_sleep(void *wchan);
-
-const char const * const ao_state_names[] = {
-       "startup", "idle", "pad", "boost", "coast",
-       "apogee", "drogue", "main", "landed", "invalid"
-};
-
-struct ao_cmds {
-       char            cmd;
-       void            (*func)(void);
-       const char      *help;
-};
-
-
-static int16_t altitude_table[2048] = {
-#include "altitude.h"
-};
-
-int16_t
-ao_pres_to_altitude(int16_t pres) __reentrant
-{
-       pres = pres >> 4;
-       if (pres < 0) pres = 0;
-       if (pres > 2047) pres = 2047;
-       return altitude_table[pres];
-}
-
-int16_t
-ao_altitude_to_pres(int16_t alt) __reentrant
-{
-       int16_t pres;
-
-       for (pres = 0; pres < 2047; pres++)
-               if (altitude_table[pres] <= alt)
-                       break;
-       return pres << 4;
-}
-
-struct ao_config {
-       uint16_t        main_deploy;
-       int16_t         accel_zero_g;
-};
-
-#define ao_config_get()
-
-struct ao_config ao_config = { 250, 16000 };
-
-#include "ao_flight.c"
-
-void
-ao_insert(void)
-{
-       ao_adc_ring[ao_adc_head] = ao_adc_static;
-       ao_adc_head = ao_adc_ring_next(ao_adc_head);
-       if (ao_flight_state != ao_flight_startup) {
-               printf("time %g accel %d pres %d\n",
-                      (double) ao_adc_static.tick / 100,
-                      ao_adc_static.accel,
-                      ao_adc_static.pres);
-       }
-}
-
-static int     ao_records_read = 0;
-static int     ao_eof_read = 0;
-static int     ao_flight_ground_accel;
-static int     ao_flight_started = 0;
-
-void
-ao_sleep(void *wchan)
-{
-       ao_dump_state();
-       if (wchan == &ao_adc_ring) {
-               char            type;
-               uint16_t        tick;
-               uint16_t        a, b;
-               int             ret;
-               char            line[1024];
-               char            *saveptr;
-               char            *l;
-               char            *words[64];
-               int             nword;
-
-               for (;;) {
-                       if (ao_records_read > 2 && ao_flight_state == ao_flight_startup)
-                       {
-                               ao_adc_static.accel = ao_flight_ground_accel;
-                               ao_insert();
-                               return;
-                       }
-
-                       if (!fgets(line, sizeof (line), emulator_in)) {
-                               if (++ao_eof_read >= 1000) {
-                                       printf ("no more data, exiting simulation\n");
-                                       exit(0);
-                               }
-                               ao_adc_static.tick += 10;
-                               ao_insert();
-                               return;
-                       }
-                       l = line;
-                       for (nword = 0; nword < 64; nword++) {
-                               words[nword] = strtok_r(l, " \t\n", &saveptr);
-                               l = NULL;
-                               if (words[nword] == NULL)
-                                       break;
-                       }
-                       if (nword == 4) {
-                               type = words[0][0];
-                               tick = strtoul(words[1], NULL, 16);
-                               a = strtoul(words[2], NULL, 16);
-                               b = strtoul(words[2], NULL, 16);
-                       } else if (nword >= 36 && strcmp(words[0], "CALL") == 0) {
-                               tick = atoi(words[10]);
-                               if (!ao_flight_started) {
-                                       type = 'F';
-                                       a = atoi(words[26]);
-                                       ao_flight_started = 1;
-                               } else {
-                                       type = 'A';
-                                       a = atoi(words[12]);
-                                       b = atoi(words[14]);
-                               }
-                       }
-                       if (type != 'F' && !ao_flight_started)
-                               continue;
-
-                       switch (type) {
-                       case 'F':
-                               ao_flight_ground_accel = a;
-                               ao_flight_started = 1;
-                               break;
-                       case 'S':
-                               break;
-                       case 'A':
-                               ao_adc_static.tick = tick;
-                               ao_adc_static.accel = a;
-                               ao_adc_static.pres = b;
-                               ao_records_read++;
-                               ao_insert();
-                               return;
-                       case 'T':
-                               ao_adc_static.tick = tick;
-                               ao_adc_static.temp = a;
-                               ao_adc_static.v_batt = b;
-                               break;
-                       case 'D':
-                       case 'G':
-                       case 'N':
-                       case 'W':
-                       case 'H':
-                               break;
-                       }
-               }
-
-       }
-}
-#define COUNTS_PER_G 264.8
-
-void
-ao_dump_state(void)
-{
-       if (ao_flight_state == ao_flight_startup)
-               return;
-       printf ("\t\t\t\t\t%s accel %g vel %g alt %d main %d\n",
-               ao_state_names[ao_flight_state],
-               (ao_ground_accel - ao_flight_accel) / COUNTS_PER_G * GRAVITY,
-               (double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
-               ao_pres_to_altitude(ao_flight_pres) - ao_pres_to_altitude(ao_ground_pres),
-               ao_pres_to_altitude(ao_main_pres) - ao_pres_to_altitude(ao_ground_pres));
-       if (ao_flight_state == ao_flight_landed)
-               exit(0);
-}
-
-int
-main (int argc, char **argv)
-{
-       emulator_in = fopen (argv[1], "r");
-       if (!emulator_in) {
-               perror(argv[1]);
-               exit(1);
-       }
-       ao_flight_init();
-       ao_flight();
-}