altos: Restructure altos build to prepare for multi-arch support

Split out sources into separate directories:

	core:		architecture and product independent bits
	cc1111:		cc1111-specific code
	drivers:	architecture independent drivers
	product:	product-specific sources and Makefile fragments
	util:		scripts for building stuff

This should have no effect on the built products, but testing is encouraged

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

1 files changed, 0 insertions, 716 deletions

diff --git a/src/ao_flight_test.c b/src/ao_flight_test.c
deleted file mode 100644
index 56733c89..00000000
--- a/src/ao_flight_test.c
+++ /dev/null
@@ -1,716 +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>
-#include <getopt.h>
-#include <math.h>
-
-#define AO_HERTZ	100
-
-#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))
-
-#define AO_M_TO_HEIGHT(m)	((int16_t) (m))
-#define AO_MS_TO_SPEED(ms)	((int16_t) ((ms) * 16))
-#define AO_MSS_TO_ACCEL(mss)	((int16_t) ((mss) * 16))
-
-/*
- * 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		pres_real;	/* unclipped */
-	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
-
-#define to_fix16(x) ((int16_t) ((x) * 65536.0 + 0.5))
-#define to_fix32(x) ((int32_t) ((x) * 65536.0 + 0.5))
-#define from_fix(x)	((x) >> 16)
-
-/*
- * Above this height, the baro sensor doesn't work
- */
-#define AO_MAX_BARO_HEIGHT	12000
-#define AO_BARO_SATURATE	13000
-#define AO_MIN_BARO_VALUE	ao_altitude_to_pres(AO_BARO_SATURATE)
-
-/*
- * Above this speed, baro measurements are unreliable
- */
-#define AO_MAX_BARO_SPEED	200
-
-#define ACCEL_NOSE_UP	(ao_accel_2g >> 2)
-
-enum ao_flight_state {
-	ao_flight_startup = 0,
-	ao_flight_idle = 1,
-	ao_flight_pad = 2,
-	ao_flight_boost = 3,
-	ao_flight_fast = 4,
-	ao_flight_coast = 5,
-	ao_flight_drogue = 6,
-	ao_flight_main = 7,
-	ao_flight_landed = 8,
-	ao_flight_invalid = 9
-};
-
-extern enum ao_flight_state ao_flight_state;
-
-#define FALSE 0
-#define TRUE 1
-
-struct ao_adc ao_adc_ring[AO_ADC_RING];
-uint8_t ao_adc_head;
-int	ao_summary = 0;
-
-#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)
-#define ao_rdf_set(rdf)
-#define ao_packet_slave_start()
-#define ao_packet_slave_stop()
-
-enum ao_igniter {
-	ao_igniter_drogue = 0,
-	ao_igniter_main = 1
-};
-
-struct ao_adc ao_adc_static;
-
-int	drogue_height;
-double	drogue_time;
-int	main_height;
-double	main_time;
-
-int	tick_offset;
-
-static int32_t	ao_k_height;
-
-void
-ao_ignite(enum ao_igniter igniter)
-{
-	double time = (double) (ao_adc_static.tick + tick_offset) / 100;
-
-	if (igniter == ao_igniter_drogue) {
-		drogue_time = time;
-		drogue_height = ao_k_height >> 16;
-	} else {
-		main_time = time;
-		main_height = ao_k_height >> 16;
-	}
-}
-
-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
-
-int	ao_flight_debug;
-
-FILE *emulator_in;
-char *emulator_app;
-char *emulator_name;
-double emulator_error_max = 4;
-double emulator_height_error_max = 20;	/* noise in the baro sensor */
-
-void
-ao_dump_state(void);
-
-void
-ao_sleep(void *wchan);
-
-const char const * const ao_state_names[] = {
-	"startup", "idle", "pad", "boost", "fast",
-	"coast", "drogue", "main", "landed", "invalid"
-};
-
-struct ao_cmds {
-	void		(*func)(void);
-	const char	*help;
-};
-
-#include "ao_convert.c"
-
-struct ao_config {
-	uint16_t	main_deploy;
-	int16_t		accel_plus_g;
-	int16_t		accel_minus_g;
-	uint8_t		pad_orientation;
-};
-
-#define AO_PAD_ORIENTATION_ANTENNA_UP	0
-#define AO_PAD_ORIENTATION_ANTENNA_DOWN	1
-
-#define ao_config_get()
-
-struct ao_config ao_config;
-
-#define DATA_TO_XDATA(x) (x)
-
-#define HAS_FLIGHT 1
-#define HAS_ADC 1
-#define HAS_USB 1
-#define HAS_GPS 1
-#ifndef HAS_ACCEL
-#define HAS_ACCEL 1
-#define HAS_ACCEL_REF 0
-#endif
-
-#define GRAVITY 9.80665
-extern int16_t ao_ground_accel, ao_flight_accel;
-extern int16_t ao_accel_2g;
-
-extern uint16_t	ao_sample_tick;
-
-extern int16_t	ao_sample_height;
-extern int16_t	ao_sample_accel;
-extern int32_t	ao_accel_scale;
-extern int16_t	ao_ground_height;
-extern int16_t	ao_sample_alt;
-
-int ao_sample_prev_tick;
-uint16_t	prev_tick;
-
-#include "ao_kalman.c"
-#include "ao_sample.c"
-#include "ao_flight.c"
-
-#define to_double(f)	((f) / 65536.0)
-
-static int	ao_records_read = 0;
-static int	ao_eof_read = 0;
-static int	ao_flight_ground_accel;
-static int	ao_flight_started = 0;
-static int	ao_test_max_height;
-static double	ao_test_max_height_time;
-static int	ao_test_main_height;
-static double	ao_test_main_height_time;
-static double	ao_test_landed_time;
-static double	ao_test_landed_height;
-static double	ao_test_landed_time;
-static int	landed_set;
-static double	landed_time;
-static double	landed_height;
-
-void
-ao_test_exit(void)
-{
-	double	drogue_error;
-	double	main_error;
-	double	landed_error;
-	double	landed_time_error;
-
-	if (!ao_test_main_height_time) {
-		ao_test_main_height_time = ao_test_max_height_time;
-		ao_test_main_height = ao_test_max_height;
-	}
-	drogue_error = fabs(ao_test_max_height_time - drogue_time);
-	main_error = fabs(ao_test_main_height_time - main_time);
-	landed_error = fabs(ao_test_landed_height - landed_height);
-	landed_time_error = ao_test_landed_time - landed_time;
-	if (drogue_error > emulator_error_max || main_error > emulator_error_max ||
-	    landed_time_error > emulator_error_max || landed_error > emulator_height_error_max) {
-		printf ("%s %s\n",
-			emulator_app, emulator_name);
-		printf ("\tApogee error %g\n", drogue_error);
-		printf ("\tMain error %g\n", main_error);
-		printf ("\tLanded height error %g\n", landed_error);
-		printf ("\tLanded time error %g\n", landed_time_error);
-		printf ("\tActual: apogee: %d at %7.2f main: %d at %7.2f landed %7.2f at %7.2f\n",
-			ao_test_max_height, ao_test_max_height_time,
-			ao_test_main_height, ao_test_main_height_time,
-			ao_test_landed_height, ao_test_landed_time);
-		printf ("\tComputed: apogee: %d at %7.2f main: %d at %7.2f landed %7.2f at %7.2f\n",
-			drogue_height, drogue_time, main_height, main_time,
-			landed_height, landed_time);
-		exit (1);
-	}
-	exit(0);
-}
-
-void
-ao_insert(void)
-{
-	double	time;
-
-	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) {
-		double	height = ao_pres_to_altitude(ao_adc_static.pres_real) - ao_ground_height;
-		double  accel = ((ao_flight_ground_accel - ao_adc_static.accel) * GRAVITY * 2.0) /
-			(ao_config.accel_minus_g - ao_config.accel_plus_g);
-
-		if (!tick_offset)
-			tick_offset = -ao_adc_static.tick;
-		if ((prev_tick - ao_adc_static.tick) > 0x400)
-			tick_offset += 65536;
-		prev_tick = ao_adc_static.tick;
-		time = (double) (ao_adc_static.tick + tick_offset) / 100;
-
-		if (ao_test_max_height < height) {
-			ao_test_max_height = height;
-			ao_test_max_height_time = time;
-			ao_test_landed_height = height;
-			ao_test_landed_time = time;
-		}
-		if (height > ao_config.main_deploy) {
-			ao_test_main_height_time = time;
-			ao_test_main_height = height;
-		}
-
-		if (ao_test_landed_height > height) {
-			ao_test_landed_height = height;
-			ao_test_landed_time = time;
-		}
-
-		if (ao_flight_state == ao_flight_landed && !landed_set) {
-			landed_set = 1;
-			landed_time = time;
-			landed_height = height;
-		}
-
-		if (!ao_summary) {
-			printf("%7.2f height %8.2f accel %8.3f state %-8.8s k_height %8.2f k_speed %8.3f k_accel %8.3f avg_height %5d drogue %4d main %4d error %5d\n",
-			       time,
-			       height,
-			       accel,
-			       ao_state_names[ao_flight_state],
-			       ao_k_height / 65536.0,
-			       ao_k_speed / 65536.0 / 16.0,
-			       ao_k_accel / 65536.0 / 16.0,
-			       ao_avg_height,
-			       drogue_height,
-			       main_height,
-			       ao_error_h_sq_avg);
-			
-//			if (ao_flight_state == ao_flight_landed)
-//				ao_test_exit();
-		}
-	}
-}
-
-#define AO_MAX_CALLSIGN			8
-#define AO_MAX_VERSION			8
-#define AO_MAX_TELEMETRY		128
-
-struct ao_telemetry_generic {
-	uint16_t	serial;		/* 0 */
-	uint16_t	tick;		/* 2 */
-	uint8_t		type;		/* 4 */
-	uint8_t		payload[27];	/* 5 */
-	/* 32 */
-};
-
-#define AO_TELEMETRY_SENSOR_TELEMETRUM	0x01
-#define AO_TELEMETRY_SENSOR_TELEMINI	0x02
-#define AO_TELEMETRY_SENSOR_TELENANO	0x03
-
-struct ao_telemetry_sensor {
-	uint16_t	serial;		/*  0 */
-	uint16_t	tick;		/*  2 */
-	uint8_t		type;		/*  4 */
-
-	uint8_t         state;          /*  5 flight state */
-	int16_t		accel;		/*  6 accelerometer (TM only) */
-	int16_t		pres;		/*  8 pressure sensor */
-	int16_t		temp;		/* 10 temperature sensor */
-	int16_t		v_batt;		/* 12 battery voltage */
-	int16_t		sense_d;	/* 14 drogue continuity sense (TM/Tm) */
-	int16_t		sense_m;	/* 16 main continuity sense (TM/Tm) */
-
-	int16_t         acceleration;   /* 18 m/s² * 16 */
-	int16_t         speed;          /* 20 m/s * 16 */
-	int16_t         height;         /* 22 m */
-
-	int16_t		ground_pres;	/* 24 average pres on pad */
-	int16_t		ground_accel;	/* 26 average accel on pad */
-	int16_t		accel_plus_g;	/* 28 accel calibration at +1g */
-	int16_t		accel_minus_g;	/* 30 accel calibration at -1g */
-	/* 32 */
-};
-
-#define AO_TELEMETRY_CONFIGURATION	0x04
-
-struct ao_telemetry_configuration {
-	uint16_t	serial;				/*  0 */
-	uint16_t	tick;				/*  2 */
-	uint8_t		type;				/*  4 */
-
-	uint8_t         device;         		/*  5 device type */
-	uint16_t        flight;				/*  6 flight number */
-	uint8_t		config_major;			/*  8 Config major version */
-	uint8_t		config_minor;			/*  9 Config minor version */
-	uint16_t	apogee_delay;			/* 10 Apogee deploy delay in seconds */
-	uint16_t	main_deploy;			/* 12 Main deploy alt in meters */
-	uint16_t	flight_log_max;			/* 14 Maximum flight log size in kB */
-	char		callsign[AO_MAX_CALLSIGN];	/* 16 Radio operator identity */
-	char		version[AO_MAX_VERSION];	/* 24 Software version */
-	/* 32 */
-};
-
-#define AO_TELEMETRY_LOCATION		0x05
-
-#define AO_GPS_MODE_NOT_VALID		'N'
-#define AO_GPS_MODE_AUTONOMOUS		'A'
-#define AO_GPS_MODE_DIFFERENTIAL	'D'
-#define AO_GPS_MODE_ESTIMATED		'E'
-#define AO_GPS_MODE_MANUAL		'M'
-#define AO_GPS_MODE_SIMULATED		'S'
-
-struct ao_telemetry_location {
-	uint16_t	serial;		/*  0 */
-	uint16_t	tick;		/*  2 */
-	uint8_t		type;		/*  4 */
-
-	uint8_t         flags;		/*  5 Number of sats and other flags */
-	int16_t         altitude;	/*  6 GPS reported altitude (m) */
-	int32_t         latitude;	/*  8 latitude (degrees * 10⁷) */
-	int32_t         longitude;	/* 12 longitude (degrees * 10⁷) */
-	uint8_t         year;		/* 16 (- 2000) */
-	uint8_t         month;		/* 17 (1-12) */
-	uint8_t         day;		/* 18 (1-31) */
-	uint8_t         hour;		/* 19 (0-23) */
-	uint8_t         minute;		/* 20 (0-59) */
-	uint8_t         second;		/* 21 (0-59) */
-	uint8_t         pdop;		/* 22 (m * 5) */
-	uint8_t         hdop;		/* 23 (m * 5) */
-	uint8_t         vdop;		/* 24 (m * 5) */
-	uint8_t         mode;		/* 25 */
-	uint16_t	ground_speed;	/* 26 cm/s */
-	int16_t		climb_rate;	/* 28 cm/s */
-	uint8_t		course;		/* 30 degrees / 2 */
-	uint8_t		unused[1];	/* 31 */
-	/* 32 */
-};
-
-#define AO_TELEMETRY_SATELLITE		0x06
-
-struct ao_telemetry_satellite_info {
-	uint8_t		svid;
-	uint8_t		c_n_1;
-};
-
-struct ao_telemetry_satellite {
-	uint16_t				serial;		/*  0 */
-	uint16_t				tick;		/*  2 */
-	uint8_t					type;		/*  4 */
-	uint8_t					channels;	/*  5 number of reported sats */
-
-	struct ao_telemetry_satellite_info	sats[12];	/* 6 */
-	uint8_t					unused[2];	/* 30 */
-	/* 32 */
-};
-
-union ao_telemetry_all {
-	struct ao_telemetry_generic		generic;
-	struct ao_telemetry_sensor		sensor;
-	struct ao_telemetry_configuration	configuration;
-	struct ao_telemetry_location		location;
-	struct ao_telemetry_satellite		satellite;
-};
-
-uint16_t
-uint16(uint8_t *bytes, int off)
-{
-	off++;
-	return (uint16_t) bytes[off] | (((uint16_t) bytes[off+1]) << 8);
-}
-
-int16_t
-int16(uint8_t *bytes, int off)
-{
-	return (int16_t) uint16(bytes, off);
-}
-
-void
-ao_sleep(void *wchan)
-{
-	if (wchan == &ao_adc_head) {
-		char		type;
-		uint16_t	tick;
-		uint16_t	a, b;
-		int		ret;
-		uint8_t		bytes[1024];
-		union ao_telemetry_all	telem;
-		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) {
-					if (!ao_summary)
-						printf ("no more data, exiting simulation\n");
-					ao_test_exit();
-				}
-				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[3], NULL, 16);
-				if (type == 'P')
-					type = 'A';
-			} else if (nword >= 6 && strcmp(words[0], "Accel") == 0) {
-				ao_config.accel_plus_g = atoi(words[3]);
-				ao_config.accel_minus_g = atoi(words[5]);
-			} else if (nword >= 4 && strcmp(words[0], "Main") == 0) {
-				ao_config.main_deploy = atoi(words[2]);
-			} 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]);
-				}
-			} else if (nword == 3 && strcmp(words[0], "BARO") == 0) {
-				tick = strtol(words[1], NULL, 16);
-				a = 16384 - 328;
-				b = strtol(words[2], NULL, 10);
-				type = 'A';
-				if (!ao_flight_started) {
-					ao_flight_ground_accel = 16384 - 328;
-					ao_config.accel_plus_g = 16384 - 328;
-					ao_config.accel_minus_g = 16384 + 328;
-					ao_flight_started = 1;
-				}
-			} else if (nword == 2 && strcmp(words[0], "TELEM") == 0) {
-				char	*hex = words[1];
-				char	elt[3];
-				int	i, len;
-				uint8_t	sum;
-
-				len = strlen(hex);
-				if (len > sizeof (bytes) * 2) {
-					len = sizeof (bytes)*2;
-					hex[len] = '\0';
-				}
-				for (i = 0; i < len; i += 2) {
-					elt[0] = hex[i];
-					elt[1] = hex[i+1];
-					elt[2] = '\0';
-					bytes[i/2] = (uint8_t) strtol(elt, NULL, 16);
-				}
-				len = i/2;
-				if (bytes[0] != len - 2) {
-					printf ("bad length %d != %d\n", bytes[0], len - 2);
-					continue;
-				}
-				sum = 0x5a;
-				for (i = 1; i < len-1; i++)
-					sum += bytes[i];
-				if (sum != bytes[len-1]) {
-					printf ("bad checksum\n");
-					continue;
-				}
-				if ((bytes[len-2] & 0x80) == 0) {
-					continue;
-				}
-				if (len == 36) {
-					memcpy(&telem, bytes + 1, 32);
-					tick = telem.generic.tick;
-					switch (telem.generic.type) {
-					case AO_TELEMETRY_SENSOR_TELEMETRUM:
-					case AO_TELEMETRY_SENSOR_TELEMINI:
-					case AO_TELEMETRY_SENSOR_TELENANO:
-						if (!ao_flight_started) {
-							ao_flight_ground_accel = telem.sensor.ground_accel;
-							ao_config.accel_plus_g = telem.sensor.accel_plus_g;
-							ao_config.accel_minus_g = telem.sensor.accel_minus_g;
-							ao_flight_started = 1;
-						}
-						type = 'A';
-						a = telem.sensor.accel;
-						b = telem.sensor.pres;
-						break;
-					}
-				} else if (len == 99) {
-					ao_flight_started = 1;
-					tick = uint16(bytes, 21);
-					ao_flight_ground_accel = int16(bytes, 7);
-					ao_config.accel_plus_g = int16(bytes, 17);
-					ao_config.accel_minus_g = int16(bytes, 19);
-					type = 'A';
-					a = int16(bytes, 23);
-					b = int16(bytes, 25);
-				} else if (len == 98) {
-					ao_flight_started = 1;
-					tick = uint16(bytes, 20);
-					ao_flight_ground_accel = int16(bytes, 6);
-					ao_config.accel_plus_g = int16(bytes, 16);
-					ao_config.accel_minus_g = int16(bytes, 18);
-					type = 'A';
-					a = int16(bytes, 22);
-					b = int16(bytes, 24);
-				} else {
-					printf("unknown len %d\n", len);
-					continue;
-				}
-			}
-			if (type != 'F' && !ao_flight_started)
-				continue;
-
-			switch (type) {
-			case 'F':
-				ao_flight_ground_accel = a;
-				if (ao_config.accel_plus_g == 0) {
-					ao_config.accel_plus_g = a;
-					ao_config.accel_minus_g = a + 530;
-				}
-				if (ao_config.main_deploy == 0)
-					ao_config.main_deploy = 250;
-				ao_flight_started = 1;
-				break;
-			case 'S':
-				break;
-			case 'A':
-				ao_adc_static.tick = tick;
-				ao_adc_static.accel = a;
-				ao_adc_static.pres_real = b;
-				if (b < AO_MIN_BARO_VALUE)
-					b = AO_MIN_BARO_VALUE;
-				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)
-{
-}
-
-static const struct option options[] = {
-	{ .name = "summary", .has_arg = 0, .val = 's' },
-	{ .name = "debug", .has_arg = 0, .val = 'd' },
-	{ 0, 0, 0, 0},
-};
-
-void run_flight_fixed(char *name, FILE *f, int summary)
-{
-	emulator_name = name;
-	emulator_in = f;
-	ao_summary = summary;
-	ao_flight_init();
-	ao_flight();
-}
-
-int
-main (int argc, char **argv)
-{
-	int	summary = 0;
-	int	c;
-	int	i;
-
-#if HAS_ACCEL
-	emulator_app="full";
-#else
-	emulator_app="baro";
-#endif
-	while ((c = getopt_long(argc, argv, "sd", options, NULL)) != -1) {
-		switch (c) {
-		case 's':
-			summary = 1;
-			break;
-		case 'd':
-			ao_flight_debug = 1;
-			break;
-		}
-	}
-
-	if (optind == argc)
-		run_flight_fixed("<stdin>", stdin, summary);
-	else
-		for (i = optind; i < argc; i++) {
-			FILE	*f = fopen(argv[i], "r");
-			if (!f) {
-				perror(argv[i]);
-				continue;
-			}
-			run_flight_fixed(argv[i], f, summary);
-			fclose(f);
-		}
-}