Use autotools, move altos to src subdir

Signed-off-by: Keith Packard <keithp@keithp.com>

1 files changed, 288 insertions, 0 deletions

diff --git a/src/ao_flight_test.c b/src/ao_flight_test.c
new file mode 100644
index 00000000..f4731aa8
--- /dev/null
+++ b/src/ao_flight_test.c
@@ -0,0 +1,288 @@
+/*
+ * 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();
+}