X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=src%2Ftest%2Fao_flight_test.c;h=1ee3ad2756fd9d79cf0d8ea28c656be5f3f2ba15;hp=baf2ad1dcea2f2dd3f5b4368a29fd5ffba427c0c;hb=3d5db24708b37d86eac187169e2553a408dfeb83;hpb=29edf6d901432a1afc65900ff599c963edac5a2b diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index baf2ad1d..1ee3ad27 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -20,10 +20,13 @@ #include #include #include +#include #include #include #include +#define GRAVITY 9.80665 + #define AO_HERTZ 100 #define HAS_ADC 1 @@ -35,6 +38,27 @@ #define AO_MS_TO_SPEED(ms) ((int16_t) ((ms) * 16)) #define AO_MSS_TO_ACCEL(mss) ((int16_t) ((mss) * 16)) +#define AO_GPS_NEW_DATA 1 +#define AO_GPS_NEW_TRACKING 2 + +int ao_gps_new; + +#if TELEMEGA +#define AO_ADC_NUM_SENSE 6 +#define HAS_MS5607 1 +#define HAS_MPU6000 1 +#define HAS_MMA655X 1 +#define HAS_HMC5883 1 + +struct ao_adc { + int16_t sense[AO_ADC_NUM_SENSE]; + int16_t v_batt; + int16_t v_pbatt; + int16_t accel_ref; + int16_t accel; + int16_t temp; +}; +#else /* * One set of samples read from the A/D converter */ @@ -48,13 +72,115 @@ struct ao_adc { int16_t sense_m; /* main continuity sense */ }; +#ifndef HAS_ACCEL +#define HAS_ACCEL 1 +#define HAS_ACCEL_REF 0 +#endif + +#endif + #define __pdata #define __data #define __xdata #define __code #define __reentrant +#define HAS_FLIGHT 1 +#define HAS_IGNITE 1 +#define HAS_USB 1 +#define HAS_GPS 1 + #include +#include +#include + +#if TELEMEGA +int ao_gps_count; +struct ao_telemetry_location ao_gps_first; +struct ao_telemetry_location ao_gps_prev; +struct ao_telemetry_location ao_gps_static; + +struct ao_telemetry_satellite ao_gps_tracking; + +static inline double sqr(double a) { return a * a; } + +void +cc_great_circle (double start_lat, double start_lon, + double end_lat, double end_lon, + double *dist, double *bearing) +{ + const double rad = M_PI / 180; + const double earth_radius = 6371.2 * 1000; /* in meters */ + double lat1 = rad * start_lat; + double lon1 = rad * -start_lon; + double lat2 = rad * end_lat; + double lon2 = rad * -end_lon; + +// double d_lat = lat2 - lat1; + double d_lon = lon2 - lon1; + + /* From http://en.wikipedia.org/wiki/Great-circle_distance */ + double vdn = sqrt(sqr(cos(lat2) * sin(d_lon)) + + sqr(cos(lat1) * sin(lat2) - + sin(lat1) * cos(lat2) * cos(d_lon))); + double vdd = sin(lat1) * sin(lat2) + cos(lat1) * cos(lat2) * cos(d_lon); + double d = atan2(vdn,vdd); + double course; + + if (cos(lat1) < 1e-20) { + if (lat1 > 0) + course = M_PI; + else + course = -M_PI; + } else { + if (d < 1e-10) + course = 0; + else + course = acos((sin(lat2)-sin(lat1)*cos(d)) / + (sin(d)*cos(lat1))); + if (sin(lon2-lon1) > 0) + course = 2 * M_PI-course; + } + *dist = d * earth_radius; + *bearing = course * 180/M_PI; +} + +double +ao_distance_from_pad(void) +{ + double dist, bearing; + if (!ao_gps_count) + return 0; + + cc_great_circle(ao_gps_first.latitude / 1e7, + ao_gps_first.longitude / 1e7, + ao_gps_static.latitude / 1e7, + ao_gps_static.longitude / 1e7, + &dist, &bearing); + return dist; +} + +double +ao_gps_angle(void) +{ + double dist, bearing; + double height; + double angle; + + if (ao_gps_count < 2) + return 0; + + cc_great_circle(ao_gps_prev.latitude / 1e7, + ao_gps_prev.longitude / 1e7, + ao_gps_static.latitude / 1e7, + ao_gps_static.longitude / 1e7, + &dist, &bearing); + height = ao_gps_static.altitude - ao_gps_prev.altitude; + + angle = atan2(dist, height); + return angle * 180/M_PI; +} +#endif #define to_fix16(x) ((int16_t) ((x) * 65536.0 + 0.5)) #define to_fix32(x) ((int32_t) ((x) * 65536.0 + 0.5)) @@ -63,7 +189,6 @@ struct ao_adc { /* * 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) @@ -74,19 +199,6 @@ struct ao_adc { #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 @@ -106,6 +218,7 @@ int ao_summary = 0; #define ao_rdf_set(rdf) #define ao_packet_slave_start() #define ao_packet_slave_stop() +#define flush() enum ao_igniter { ao_igniter_drogue = 0, @@ -123,6 +236,18 @@ int tick_offset; static int32_t ao_k_height; +int16_t +ao_time(void) +{ + return ao_data_static.tick; +} + +void +ao_delay(int16_t interval) +{ + return; +} + void ao_ignite(enum ao_igniter igniter) { @@ -141,7 +266,7 @@ struct ao_task { int dummy; }; -#define ao_add_task(t,f,n) +#define ao_add_task(t,f,n) ((void) (t)) #define ao_log_start() #define ao_log_stop() @@ -156,6 +281,7 @@ int ao_flight_debug; FILE *emulator_in; char *emulator_app; char *emulator_name; +char *emulator_info; double emulator_error_max = 4; double emulator_height_error_max = 20; /* noise in the baro sensor */ @@ -179,7 +305,17 @@ struct ao_cmds { #define ao_xmemset(d,v,c) memset(d,v,c) #define ao_xmemcmp(d,s,c) memcmp(d,s,c) +#define AO_NEED_ALTITUDE_TO_PRES 1 +#if TELEMEGA +#include "ao_convert_pa.c" +#include +struct ao_ms5607_prom ao_ms5607_prom; +#include "ao_ms5607_convert.c" +#define AO_PYRO_NUM 4 +#include +#else #include "ao_convert.c" +#endif struct ao_config { uint16_t main_deploy; @@ -187,6 +323,12 @@ struct ao_config { int16_t accel_minus_g; uint8_t pad_orientation; uint16_t apogee_lockout; +#if TELEMEGA + struct ao_pyro pyro[AO_PYRO_NUM]; /* minor version 12 */ + int16_t accel_zero_along; + int16_t accel_zero_across; + int16_t accel_zero_through; +#endif }; #define AO_PAD_ORIENTATION_ANTENNA_UP 0 @@ -198,33 +340,46 @@ 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; +typedef int16_t accel_t; + extern uint16_t ao_sample_tick; -extern int16_t ao_sample_height; -extern int16_t ao_sample_accel; +extern alt_t ao_sample_height; +extern accel_t ao_sample_accel; extern int32_t ao_accel_scale; -extern int16_t ao_ground_height; -extern int16_t ao_sample_alt; +extern alt_t ao_ground_height; +extern alt_t ao_sample_alt; + +double ao_sample_qangle; int ao_sample_prev_tick; uint16_t prev_tick; + #include "ao_kalman.c" -#include "ao_sample_mm.c" -#include "ao_flight_mm.c" +#include "ao_sqrt.c" +#include "ao_sample.c" +#include "ao_flight.c" +#if TELEMEGA +#define AO_PYRO_NUM 4 + +#define AO_PYRO_0 0 +#define AO_PYRO_1 1 +#define AO_PYRO_2 2 +#define AO_PYRO_3 3 + +static void +ao_pyro_pin_set(uint8_t pin, uint8_t value) +{ + printf ("set pyro %d %d\n", pin, value); +} + +#include "ao_pyro.c" +#endif #define to_double(f) ((f) / 65536.0) @@ -243,6 +398,10 @@ static int landed_set; static double landed_time; static double landed_height; +#if HAS_MPU6000 +static struct ao_mpu6000_sample ao_ground_mpu6000; +#endif + void ao_test_exit(void) { @@ -259,10 +418,11 @@ ao_test_exit(void) 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) { + if (drogue_error > emulator_error_max || main_error > emulator_error_max) { printf ("%s %s\n", emulator_app, emulator_name); + if (emulator_info) + printf ("\t%s\n", emulator_info); printf ("\tApogee error %g\n", drogue_error); printf ("\tMain error %g\n", main_error); printf ("\tLanded height error %g\n", landed_error); @@ -279,6 +439,23 @@ ao_test_exit(void) exit(0); } +#ifdef TELEMEGA +struct ao_azel { + int az; + int el; +}; + +static void +azel (struct ao_azel *r, struct ao_quaternion *q) +{ + double v; + + r->az = floor (atan2(q->y, q->x) * 180/M_PI + 0.5); + v = sqrt (q->x*q->x + q->y*q->y); + r->el = floor (atan2(q->z, v) * 180/M_PI + 0.5); +} +#endif + void ao_insert(void) { @@ -287,10 +464,22 @@ ao_insert(void) ao_data_ring[ao_data_head] = ao_data_static; ao_data_head = ao_data_ring_next(ao_data_head); if (ao_flight_state != ao_flight_startup) { - double height = ao_pres_to_altitude(ao_data_static.adc.pres_real) - ao_ground_height; - double accel = ((ao_flight_ground_accel - ao_data_static.adc.accel) * GRAVITY * 2.0) / +#if HAS_ACCEL + double accel = ((ao_flight_ground_accel - ao_data_accel_cook(&ao_data_static)) * GRAVITY * 2.0) / (ao_config.accel_minus_g - ao_config.accel_plus_g); +#else + double accel = 0.0; +#endif +#if TELEMEGA + double height; + + ao_ms5607_convert(&ao_data_static.ms5607_raw, &ao_data_static.ms5607_cooked); + height = ao_pa_to_altitude(ao_data_static.ms5607_cooked.pres) - ao_ground_height; +#else + double height = ao_pres_to_altitude(ao_data_static.adc.pres_real) - ao_ground_height; +#endif + (void) accel; if (!tick_offset) tick_offset = -ao_data_static.tick; if ((prev_tick - ao_data_static.tick) > 0x400) @@ -321,10 +510,116 @@ ao_insert(void) } 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", +#if TELEMEGA + static struct ao_quaternion ao_ground_mag; + static int ao_ground_mag_set; + + if (!ao_ground_mag_set) { + ao_quaternion_init_vector (&ao_ground_mag, + ao_data_mag_across(&ao_data_static), + ao_data_mag_through(&ao_data_static), + ao_data_mag_along(&ao_data_static)); + ao_quaternion_normalize(&ao_ground_mag, &ao_ground_mag); + ao_quaternion_rotate(&ao_ground_mag, &ao_ground_mag, &ao_rotation); + ao_ground_mag_set = 1; + } + + struct ao_quaternion ao_mag, ao_mag_rot; + + ao_quaternion_init_vector(&ao_mag, + ao_data_mag_across(&ao_data_static), + ao_data_mag_through(&ao_data_static), + ao_data_mag_along(&ao_data_static)); + + ao_quaternion_normalize(&ao_mag, &ao_mag); + ao_quaternion_rotate(&ao_mag_rot, &ao_mag, &ao_rotation); + + float ao_dot; + int ao_mag_angle; + + ao_dot = ao_quaternion_dot(&ao_mag_rot, &ao_ground_mag); + + struct ao_azel ground_azel, mag_azel, rot_azel; + + azel(&ground_azel, &ao_ground_mag); + azel(&mag_azel, &ao_mag); + azel(&rot_azel, &ao_mag_rot); + + ao_mag_angle = floor (acos(ao_dot) * 180 / M_PI + 0.5); + + (void) ao_mag_angle; + + static struct ao_quaternion ao_x = { .r = 0, .x = 1, .y = 0, .z = 0 }; + struct ao_quaternion ao_out; + + ao_quaternion_rotate(&ao_out, &ao_x, &ao_rotation); + + int out = floor (atan2(ao_out.y, ao_out.x) * 180 / M_PI); + +#if 0 + printf ("%7.2f state %-8.8s height %8.4f tilt %4d rot %4d mag_tilt %4d mag_rot %4d\n", + time, + ao_state_names[ao_flight_state], + ao_k_height / 65536.0, + ao_sample_orient, out, + mag_azel.el, + mag_azel.az); +#endif + printf ("%7.2f state %-8.8s height %8.4f tilt %4d rot %4d dist %12.2f gps_tilt %4d gps_sats %2d\n", + time, + ao_state_names[ao_flight_state], + ao_k_height / 65536.0, + ao_sample_orient, out, + ao_distance_from_pad(), + (int) floor (ao_gps_angle() + 0.5), + (ao_gps_static.flags & 0xf) * 10); + +#if 0 + printf ("\t\tstate %-8.8s ground az: %4d el %4d mag az %4d el %4d rot az %4d el %4d el_diff %4d az_diff %4d angle %4d tilt %4d ground %8.5f %8.5f %8.5f cur %8.5f %8.5f %8.5f rot %8.5f %8.5f %8.5f\n", + ao_state_names[ao_flight_state], + ground_azel.az, ground_azel.el, + mag_azel.az, mag_azel.el, + rot_azel.az, rot_azel.el, + ground_azel.el - rot_azel.el, + ground_azel.az - rot_azel.az, + ao_mag_angle, + ao_sample_orient, + ao_ground_mag.x, + ao_ground_mag.y, + ao_ground_mag.z, + ao_mag.x, + ao_mag.y, + ao_mag.z, + ao_mag_rot.x, + ao_mag_rot.y, + ao_mag_rot.z); +#endif +#endif + +#if 0 + printf("%7.2f height %8.2f accel %8.3f " +#if TELEMEGA + "angle %5d " + "accel_x %8.3f accel_y %8.3f accel_z %8.3f gyro_x %8.3f gyro_y %8.3f gyro_z %8.3f mag_x %8d mag_y %8d, mag_z %8d mag_angle %4d " +#endif + "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, +#if TELEMEGA + ao_sample_orient, + + ao_mpu6000_accel(ao_data_static.mpu6000.accel_x), + ao_mpu6000_accel(ao_data_static.mpu6000.accel_y), + ao_mpu6000_accel(ao_data_static.mpu6000.accel_z), + ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_x - ao_ground_mpu6000.gyro_x), + ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_y - ao_ground_mpu6000.gyro_y), + ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_z - ao_ground_mpu6000.gyro_z), + ao_data_static.hmc5883.x, + ao_data_static.hmc5883.y, + ao_data_static.hmc5883.z, + ao_mag_angle, +#endif ao_state_names[ao_flight_state], ao_k_height / 65536.0, ao_k_speed / 65536.0 / 16.0, @@ -333,6 +628,7 @@ ao_insert(void) drogue_height, main_height, ao_error_h_sq_avg); +#endif // if (ao_flight_state == ao_flight_landed) // ao_test_exit(); @@ -340,130 +636,10 @@ ao_insert(void) } } -#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); } @@ -473,14 +649,29 @@ int16(uint8_t *bytes, int off) return (int16_t) uint16(bytes, off); } +uint32_t +uint32(uint8_t *bytes, int off) +{ + return (uint32_t) bytes[off] | (((uint32_t) bytes[off+1]) << 8) | + (((uint32_t) bytes[off+2]) << 16) | + (((uint32_t) bytes[off+3]) << 24); +} + +int32_t +int32(uint8_t *bytes, int off) +{ + return (int32_t) uint32(bytes, off); +} + +static int log_format; + void ao_sleep(void *wchan) { if (wchan == &ao_data_head) { - char type; - uint16_t tick; - uint16_t a, b; - int ret; + char type = 0; + uint16_t tick = 0; + uint16_t a = 0, b = 0; uint8_t bytes[1024]; union ao_telemetry_all telem; char line[1024]; @@ -489,10 +680,18 @@ ao_sleep(void *wchan) char *words[64]; int nword; +#if TELEMEGA + if (ao_flight_state >= ao_flight_boost && ao_flight_state < ao_flight_landed) + ao_pyro_check(); +#endif for (;;) { if (ao_records_read > 2 && ao_flight_state == ao_flight_startup) { +#if TELEMEGA + ao_data_static.mpu6000 = ao_ground_mpu6000; +#else ao_data_static.adc.accel = ao_flight_ground_accel; +#endif ao_insert(); return; } @@ -514,16 +713,129 @@ ao_sleep(void *wchan) if (words[nword] == NULL) break; } - if (nword == 4) { +#if TELEMEGA + if (log_format == AO_LOG_FORMAT_TELEMEGA && nword == 30 && strlen(words[0]) == 1) { + int i; + struct ao_ms5607_value value; + + type = words[0][0]; + tick = strtoul(words[1], NULL, 16); +// printf ("%c %04x", type, tick); + for (i = 2; i < nword; i++) { + bytes[i - 2] = strtoul(words[i], NULL, 16); +// printf(" %02x", bytes[i-2]); + } +// printf ("\n"); + switch (type) { + case 'F': + ao_flight_ground_accel = int16(bytes, 2); + ao_flight_started = 1; + ao_ground_pres = int32(bytes, 4); + ao_ground_height = ao_pa_to_altitude(ao_ground_pres); + ao_ground_accel_along = int16(bytes, 8); + ao_ground_accel_across = int16(bytes, 10); + ao_ground_accel_through = int16(bytes, 12); + ao_ground_roll = int16(bytes, 14); + ao_ground_pitch = int16(bytes, 16); + ao_ground_yaw = int16(bytes, 18); + ao_ground_mpu6000.accel_x = ao_ground_accel_across; + ao_ground_mpu6000.accel_y = ao_ground_accel_along; + ao_ground_mpu6000.accel_z = ao_ground_accel_through; + ao_ground_mpu6000.gyro_x = ao_ground_pitch >> 9; + ao_ground_mpu6000.gyro_y = ao_ground_roll >> 9; + ao_ground_mpu6000.gyro_z = ao_ground_yaw >> 9; + break; + case 'A': + ao_data_static.tick = tick; + ao_data_static.ms5607_raw.pres = int32(bytes, 0); + ao_data_static.ms5607_raw.temp = int32(bytes, 4); + ao_ms5607_convert(&ao_data_static.ms5607_raw, &value); + ao_data_static.mpu6000.accel_x = int16(bytes, 8); + ao_data_static.mpu6000.accel_y = int16(bytes, 10); + ao_data_static.mpu6000.accel_z = int16(bytes, 12); + ao_data_static.mpu6000.gyro_x = int16(bytes, 14); + ao_data_static.mpu6000.gyro_y = int16(bytes, 16); + ao_data_static.mpu6000.gyro_z = int16(bytes, 18); + ao_data_static.hmc5883.x = int16(bytes, 20); + ao_data_static.hmc5883.y = int16(bytes, 22); + ao_data_static.hmc5883.z = int16(bytes, 24); +#if HAS_MMA655X + ao_data_static.mma655x = int16(bytes, 26); +#endif + ao_records_read++; + ao_insert(); + return; + case 'G': + ao_gps_prev = ao_gps_static; + ao_gps_static.tick = tick; + ao_gps_static.latitude = int32(bytes, 0); + ao_gps_static.longitude = int32(bytes, 4); + ao_gps_static.altitude = int32(bytes, 8); + ao_gps_static.flags = bytes[13]; + if (!ao_gps_count) + ao_gps_first = ao_gps_static; + ao_gps_count++; + break; + } + continue; + } else if (nword == 3 && strcmp(words[0], "ms5607") == 0) { + if (strcmp(words[1], "reserved:") == 0) + ao_ms5607_prom.reserved = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "sens:") == 0) + ao_ms5607_prom.sens = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "off:") == 0) + ao_ms5607_prom.off = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "tcs:") == 0) + ao_ms5607_prom.tcs = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "tco:") == 0) + ao_ms5607_prom.tco = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "tref:") == 0) + ao_ms5607_prom.tref = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "tempsens:") == 0) + ao_ms5607_prom.tempsens = strtoul(words[2], NULL, 10); + else if (strcmp(words[1], "crc:") == 0) + ao_ms5607_prom.crc = strtoul(words[2], NULL, 10); + continue; + } else if (nword >= 3 && strcmp(words[0], "Pyro") == 0) { + int p = strtoul(words[1], NULL, 10); + int i, j; + struct ao_pyro *pyro = &ao_config.pyro[p]; + + for (i = 2; i < nword; i++) { + for (j = 0; j < NUM_PYRO_VALUES; j++) + if (!strcmp (words[i], ao_pyro_values[j].name)) + break; + if (j == NUM_PYRO_VALUES) + continue; + pyro->flags |= ao_pyro_values[j].flag; + if (ao_pyro_values[j].offset != NO_VALUE && i + 1 < nword) { + int16_t val = strtoul(words[++i], NULL, 10); + *((int16_t *) ((char *) pyro + ao_pyro_values[j].offset)) = val; + } + } + } +#else + if (nword == 4 && log_format != AO_LOG_FORMAT_TELEMEGA) { 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'; + } +#endif + else if (nword == 2 && strcmp(words[0], "log-format") == 0) { + log_format = strtoul(words[1], NULL, 10); } 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]); +#ifdef TELEMEGA + } else if (nword >= 8 && strcmp(words[0], "IMU") == 0) { + ao_config.accel_zero_along = atoi(words[3]); + ao_config.accel_zero_across = atoi(words[5]); + ao_config.accel_zero_through = atoi(words[7]); + printf ("%d %d %d\n", ao_config.accel_zero_along, ao_config.accel_zero_across, ao_config.accel_zero_through); +#endif } else if (nword >= 4 && strcmp(words[0], "Main") == 0) { ao_config.main_deploy = atoi(words[2]); } else if (nword >= 3 && strcmp(words[0], "Apogee") == 0 && @@ -603,22 +915,22 @@ ao_sleep(void *wchan) } } 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); + tick = uint16(bytes+1, 21); + ao_flight_ground_accel = int16(bytes+1, 7); + ao_config.accel_plus_g = int16(bytes+1, 17); + ao_config.accel_minus_g = int16(bytes+1, 19); type = 'A'; - a = int16(bytes, 23); - b = int16(bytes, 25); + a = int16(bytes+1, 23); + b = int16(bytes+1, 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); + tick = uint16(bytes+1, 20); + ao_flight_ground_accel = int16(bytes+1, 6); + ao_config.accel_plus_g = int16(bytes+1, 16); + ao_config.accel_minus_g = int16(bytes+1, 18); type = 'A'; - a = int16(bytes, 22); - b = int16(bytes, 24); + a = int16(bytes+1, 22); + b = int16(bytes+1, 24); } else { printf("unknown len %d\n", len); continue; @@ -627,6 +939,10 @@ ao_sleep(void *wchan) if (type != 'F' && !ao_flight_started) continue; +#if TELEMEGA + (void) a; + (void) b; +#else switch (type) { case 'F': ao_flight_ground_accel = a; @@ -662,6 +978,7 @@ ao_sleep(void *wchan) case 'H': break; } +#endif } } @@ -676,13 +993,15 @@ ao_dump_state(void) static const struct option options[] = { { .name = "summary", .has_arg = 0, .val = 's' }, { .name = "debug", .has_arg = 0, .val = 'd' }, + { .name = "info", .has_arg = 1, .val = 'i' }, { 0, 0, 0, 0}, }; -void run_flight_fixed(char *name, FILE *f, int summary) +void run_flight_fixed(char *name, FILE *f, int summary, char *info) { emulator_name = name; emulator_in = f; + emulator_info = info; ao_summary = summary; ao_flight_init(); ao_flight(); @@ -694,13 +1013,14 @@ main (int argc, char **argv) int summary = 0; int c; int i; + char *info = NULL; #if HAS_ACCEL emulator_app="full"; #else emulator_app="baro"; #endif - while ((c = getopt_long(argc, argv, "sd", options, NULL)) != -1) { + while ((c = getopt_long(argc, argv, "sdi:", options, NULL)) != -1) { switch (c) { case 's': summary = 1; @@ -708,11 +1028,14 @@ main (int argc, char **argv) case 'd': ao_flight_debug = 1; break; + case 'i': + info = optarg; + break; } } if (optind == argc) - run_flight_fixed("", stdin, summary); + run_flight_fixed("", stdin, summary, info); else for (i = optind; i < argc; i++) { FILE *f = fopen(argv[i], "r"); @@ -720,7 +1043,8 @@ main (int argc, char **argv) perror(argv[i]); continue; } - run_flight_fixed(argv[i], f, summary); + run_flight_fixed(argv[i], f, summary, info); fclose(f); } + exit(0); }