#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)
enum ao_igniter {
ao_igniter_drogue = 0,
};
struct ao_cmds {
- uint8_t cmd;
+ char cmd;
void (*func)(void);
const char *help;
};
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
}
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)
uint16_t tick;
uint16_t a, b;
int ret;
+ char line[1024];
for (;;) {
if (ao_records_read > 20 && ao_flight_state == ao_flight_startup)
{
+ ao_adc_static.accel = ao_flight_ground_accel;
ao_insert();
return;
}
- ret = fscanf(emulator_in, "%c %hx %hx %hx\n", &type, &tick, &a, &b);
- if (ret == EOF) {
- printf ("no more data, exiting simulation\n");
- exit(0);
+ 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;
}
+ ret = sscanf(line, "%c %hx %hx %hx", &type, &tick, &a, &b);
if (ret != 4)
continue;
+ if (type != 'F' && !ao_flight_started)
+ continue;
+
switch (type) {
case 'F':
+ ao_flight_ground_accel = a;
+ ao_flight_started = 1;
break;
case 'S':
break;
{
if (ao_flight_state == ao_flight_startup)
return;
- printf ("\t%s accel %g vel %g alt %d\n",
+ printf ("\t\t\t\t\t%s accel %g vel %g alt %d main %d\n",
ao_state_names[ao_flight_state],
- (ao_flight_accel - ao_ground_accel) / COUNTS_PER_G * GRAVITY,
+ (ao_ground_accel - ao_flight_accel) / COUNTS_PER_G * GRAVITY,
(double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
- altitude_table[ao_flight_pres >> 4]);
+ 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);
}