#include <stdlib.h>
#include <string.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))
ao_flight_pad = 2,
ao_flight_boost = 3,
ao_flight_fast = 4,
- ao_flight_apogee = 5,
+ ao_flight_coast = 5,
ao_flight_drogue = 6,
ao_flight_main = 7,
ao_flight_landed = 8,
#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,
const char const * const ao_state_names[] = {
"startup", "idle", "pad", "boost", "fast",
- "apogee", "drogue", "main", "landed", "invalid"
+ "coast", "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;
-}
+#include "ao_convert.c"
struct ao_config {
uint16_t main_deploy;
- int16_t accel_zero_g;
+ int16_t accel_plus_g;
+ int16_t accel_minus_g;
};
#define ao_config_get()
-struct ao_config ao_config = { 250, 16000 };
+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
#include "ao_flight.c"
ao_sleep(void *wchan)
{
ao_dump_state();
- if (wchan == &ao_adc_ring) {
+ if (wchan == &ao_adc_head) {
char type;
uint16_t tick;
uint16_t a, b;
type = words[0][0];
tick = strtoul(words[1], NULL, 16);
a = strtoul(words[2], NULL, 16);
- b = strtoul(words[2], NULL, 16);
+ b = strtoul(words[3], NULL, 16);
+ } else if (nword >= 6 && strcmp(words[0], "Accel")) {
+ ao_config.accel_plus_g = atoi(words[3]);
+ ao_config.accel_minus_g = atoi(words[5]);
+ } else if (nword >= 4 && strcmp(words[0], "Main")) {
+ ao_config.main_deploy = atoi(words[2]);
} else if (nword >= 36 && strcmp(words[0], "CALL") == 0) {
tick = atoi(words[10]);
if (!ao_flight_started) {
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':
{
if (ao_flight_state == ao_flight_startup)
return;
+#if HAS_ACCEL
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));
+#else
+ printf ("\t\t\t\t\t%s alt %d main %d\n",
+ ao_state_names[ao_flight_state],
+ 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));
+#endif
if (ao_flight_state == ao_flight_landed)
exit(0);
}