Fix aoview telemetry GPS parsing code to use correct columns
[fw/altos] / ao_flight_test.c
1 /*
2  * Copyright © 2009 Keith Packard <keithp@keithp.com>
3  *
4  * This program is free software; you can redistribute it and/or modify
5  * it under the terms of the GNU General Public License as published by
6  * the Free Software Foundation; version 2 of the License.
7  *
8  * This program is distributed in the hope that it will be useful, but
9  * WITHOUT ANY WARRANTY; without even the implied warranty of
10  * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
11  * General Public License for more details.
12  *
13  * You should have received a copy of the GNU General Public License along
14  * with this program; if not, write to the Free Software Foundation, Inc.,
15  * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
16  */
17
18 #define _GNU_SOURCE
19
20 #include <stdint.h>
21 #include <stdio.h>
22 #include <stdlib.h>
23 #include <string.h>
24
25 #define AO_ADC_RING     64
26 #define ao_adc_ring_next(n)     (((n) + 1) & (AO_ADC_RING - 1))
27 #define ao_adc_ring_prev(n)     (((n) - 1) & (AO_ADC_RING - 1))
28
29 /*
30  * One set of samples read from the A/D converter
31  */
32 struct ao_adc {
33         uint16_t        tick;           /* tick when the sample was read */
34         int16_t         accel;          /* accelerometer */
35         int16_t         pres;           /* pressure sensor */
36         int16_t         temp;           /* temperature sensor */
37         int16_t         v_batt;         /* battery voltage */
38         int16_t         sense_d;        /* drogue continuity sense */
39         int16_t         sense_m;        /* main continuity sense */
40 };
41
42 #define __pdata
43 #define __data
44 #define __xdata
45 #define __code
46 #define __reentrant
47
48 enum ao_flight_state {
49         ao_flight_startup = 0,
50         ao_flight_idle = 1,
51         ao_flight_launchpad = 2,
52         ao_flight_boost = 3,
53         ao_flight_coast = 4,
54         ao_flight_apogee = 5,
55         ao_flight_drogue = 6,
56         ao_flight_main = 7,
57         ao_flight_landed = 8,
58         ao_flight_invalid = 9
59 };
60
61 struct ao_adc ao_adc_ring[AO_ADC_RING];
62 uint8_t ao_adc_head;
63
64 #define ao_led_on(l)
65 #define ao_led_off(l)
66 #define ao_timer_set_adc_interval(i)
67 #define ao_wakeup(wchan) ao_dump_state()
68 #define ao_cmd_register(c)
69 #define ao_usb_disable()
70 #define ao_telemetry_set_interval(x)
71 #define ao_rdf_set(rdf)
72
73 enum ao_igniter {
74         ao_igniter_drogue = 0,
75         ao_igniter_main = 1
76 };
77
78 void
79 ao_ignite(enum ao_igniter igniter)
80 {
81         printf ("ignite %s\n", igniter == ao_igniter_drogue ? "drogue" : "main");
82 }
83
84 struct ao_task {
85         int dummy;
86 };
87
88 #define ao_add_task(t,f,n)
89
90 #define ao_log_start()
91 #define ao_log_stop()
92
93 #define AO_MS_TO_TICKS(ms)      ((ms) / 10)
94 #define AO_SEC_TO_TICKS(s)      ((s) * 100)
95
96 #define AO_FLIGHT_TEST
97
98 struct ao_adc ao_adc_static;
99
100 FILE *emulator_in;
101
102 void
103 ao_dump_state(void);
104
105 void
106 ao_sleep(void *wchan);
107
108 const char const * const ao_state_names[] = {
109         "startup", "idle", "pad", "boost", "coast",
110         "apogee", "drogue", "main", "landed", "invalid"
111 };
112
113 struct ao_cmds {
114         char            cmd;
115         void            (*func)(void);
116         const char      *help;
117 };
118
119
120 static int16_t altitude_table[2048] = {
121 #include "altitude.h"
122 };
123
124 int16_t
125 ao_pres_to_altitude(int16_t pres) __reentrant
126 {
127         pres = pres >> 4;
128         if (pres < 0) pres = 0;
129         if (pres > 2047) pres = 2047;
130         return altitude_table[pres];
131 }
132
133 int16_t
134 ao_altitude_to_pres(int16_t alt) __reentrant
135 {
136         int16_t pres;
137
138         for (pres = 0; pres < 2047; pres++)
139                 if (altitude_table[pres] <= alt)
140                         break;
141         return pres << 4;
142 }
143
144 struct ao_config {
145         uint16_t        main_deploy;
146         int16_t         accel_zero_g;
147 };
148
149 #define ao_config_get()
150
151 struct ao_config ao_config = { 250, 16000 };
152
153 #include "ao_flight.c"
154
155 void
156 ao_insert(void)
157 {
158         ao_adc_ring[ao_adc_head] = ao_adc_static;
159         ao_adc_head = ao_adc_ring_next(ao_adc_head);
160         if (ao_flight_state != ao_flight_startup) {
161                 printf("time %g accel %d pres %d\n",
162                        (double) ao_adc_static.tick / 100,
163                        ao_adc_static.accel,
164                        ao_adc_static.pres);
165         }
166 }
167
168 static int      ao_records_read = 0;
169 static int      ao_eof_read = 0;
170 static int      ao_flight_ground_accel;
171 static int      ao_flight_started = 0;
172
173 void
174 ao_sleep(void *wchan)
175 {
176         ao_dump_state();
177         if (wchan == &ao_adc_ring) {
178                 char            type;
179                 uint16_t        tick;
180                 uint16_t        a, b;
181                 int             ret;
182                 char            line[1024];
183                 char            *saveptr;
184                 char            *l;
185                 char            *words[64];
186                 int             nword;
187
188                 for (;;) {
189                         if (ao_records_read > 2 && ao_flight_state == ao_flight_startup)
190                         {
191                                 ao_adc_static.accel = ao_flight_ground_accel;
192                                 ao_insert();
193                                 return;
194                         }
195
196                         if (!fgets(line, sizeof (line), emulator_in)) {
197                                 if (++ao_eof_read >= 1000) {
198                                         printf ("no more data, exiting simulation\n");
199                                         exit(0);
200                                 }
201                                 ao_adc_static.tick += 10;
202                                 ao_insert();
203                                 return;
204                         }
205                         l = line;
206                         for (nword = 0; nword < 64; nword++) {
207                                 words[nword] = strtok_r(l, " \t\n", &saveptr);
208                                 l = NULL;
209                                 if (words[nword] == NULL)
210                                         break;
211                         }
212                         if (nword == 4) {
213                                 type = words[0][0];
214                                 tick = strtoul(words[1], NULL, 16);
215                                 a = strtoul(words[2], NULL, 16);
216                                 b = strtoul(words[2], NULL, 16);
217                         } else if (nword >= 36 && strcmp(words[0], "CALL") == 0) {
218                                 tick = atoi(words[10]);
219                                 if (!ao_flight_started) {
220                                         type = 'F';
221                                         a = atoi(words[26]);
222                                         ao_flight_started = 1;
223                                 } else {
224                                         type = 'A';
225                                         a = atoi(words[12]);
226                                         b = atoi(words[14]);
227                                 }
228                         }
229                         if (type != 'F' && !ao_flight_started)
230                                 continue;
231
232                         switch (type) {
233                         case 'F':
234                                 ao_flight_ground_accel = a;
235                                 ao_flight_started = 1;
236                                 break;
237                         case 'S':
238                                 break;
239                         case 'A':
240                                 ao_adc_static.tick = tick;
241                                 ao_adc_static.accel = a;
242                                 ao_adc_static.pres = b;
243                                 ao_records_read++;
244                                 ao_insert();
245                                 return;
246                         case 'T':
247                                 ao_adc_static.tick = tick;
248                                 ao_adc_static.temp = a;
249                                 ao_adc_static.v_batt = b;
250                                 break;
251                         case 'D':
252                         case 'G':
253                         case 'N':
254                         case 'W':
255                         case 'H':
256                                 break;
257                         }
258                 }
259
260         }
261 }
262 #define COUNTS_PER_G 264.8
263
264 void
265 ao_dump_state(void)
266 {
267         if (ao_flight_state == ao_flight_startup)
268                 return;
269         printf ("\t\t\t\t\t%s accel %g vel %g alt %d main %d\n",
270                 ao_state_names[ao_flight_state],
271                 (ao_ground_accel - ao_flight_accel) / COUNTS_PER_G * GRAVITY,
272                 (double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
273                 ao_pres_to_altitude(ao_flight_pres) - ao_pres_to_altitude(ao_ground_pres),
274                 ao_pres_to_altitude(ao_main_pres) - ao_pres_to_altitude(ao_ground_pres));
275         if (ao_flight_state == ao_flight_landed)
276                 exit(0);
277 }
278
279 int
280 main (int argc, char **argv)
281 {
282         emulator_in = fopen (argv[1], "r");
283         if (!emulator_in) {
284                 perror(argv[1]);
285                 exit(1);
286         }
287         ao_flight_init();
288         ao_flight();
289 }