X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=src%2Fcore%2Fao_telemetry.h;fp=src%2Fcore%2Fao_telemetry.h;h=0000000000000000000000000000000000000000;hp=237a35aba2a15401dc1c93695b1ae65aa1d7f47c;hb=24167015705ae831692b95735968b04a876f935e;hpb=bb9fdef607728cc326a82aa632e59724f272e53b diff --git a/src/core/ao_telemetry.h b/src/core/ao_telemetry.h deleted file mode 100644 index 237a35ab..00000000 --- a/src/core/ao_telemetry.h +++ /dev/null @@ -1,321 +0,0 @@ -/* - * Copyright © 2012 Keith Packard - * - * 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. - */ - -#ifndef _AO_TELEMETRY_H_ -#define _AO_TELEMETRY_H_ - -/* - * ao_telemetry.c - */ -#define AO_MAX_CALLSIGN 8 -#define AO_MAX_VERSION 8 -#if LEGACY_MONITOR -#define AO_MAX_TELEMETRY 128 -#else -#define AO_MAX_TELEMETRY 32 -#endif - -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; -}; - -#define AO_TELEMETRY_SATELLITE_MAX_SAT 12 - -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[AO_TELEMETRY_SATELLITE_MAX_SAT]; /* 6 */ - uint8_t unused[2]; /* 30 */ - /* 32 */ -}; - -#define AO_TELEMETRY_COMPANION 0x07 - -#define AO_COMPANION_MAX_CHANNELS 12 - -struct ao_telemetry_companion { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - uint8_t board_id; /* 5 */ - - uint8_t update_period; /* 6 */ - uint8_t channels; /* 7 */ - uint16_t companion_data[AO_COMPANION_MAX_CHANNELS]; /* 8 */ - /* 32 */ -}; - -#define AO_TELEMETRY_MEGA_SENSOR 0x08 - -struct ao_telemetry_mega_sensor { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - - uint8_t orient; /* 5 angle from vertical */ - int16_t accel; /* 6 Z axis */ - - int32_t pres; /* 8 Pa * 10 */ - int16_t temp; /* 12 °C * 100 */ - - int16_t accel_x; /* 14 */ - int16_t accel_y; /* 16 */ - int16_t accel_z; /* 18 */ - - int16_t gyro_x; /* 20 */ - int16_t gyro_y; /* 22 */ - int16_t gyro_z; /* 24 */ - - int16_t mag_x; /* 26 */ - int16_t mag_y; /* 28 */ - int16_t mag_z; /* 30 */ - /* 32 */ -}; - -#define AO_TELEMETRY_MEGA_DATA 0x09 - -struct ao_telemetry_mega_data { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - - uint8_t state; /* 5 flight state */ - - int16_t v_batt; /* 6 battery voltage */ - int16_t v_pyro; /* 8 pyro battery voltage */ - int8_t sense[6]; /* 10 continuity sense */ - - int32_t ground_pres; /* 16 average pres on pad */ - int16_t ground_accel; /* 20 average accel on pad */ - int16_t accel_plus_g; /* 22 accel calibration at +1g */ - int16_t accel_minus_g; /* 24 accel calibration at -1g */ - - int16_t acceleration; /* 26 m/s² * 16 */ - int16_t speed; /* 28 m/s * 16 */ - int16_t height; /* 30 m */ - /* 32 */ -}; - - -#define AO_TELEMETRY_METRUM_SENSOR 0x0A - -struct ao_telemetry_metrum_sensor { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - - uint8_t state; /* 5 flight state */ - int16_t accel; /* 6 Z axis */ - - int32_t pres; /* 8 Pa * 10 */ - int16_t temp; /* 12 °C * 100 */ - - int16_t acceleration; /* 14 m/s² * 16 */ - int16_t speed; /* 16 m/s * 16 */ - int16_t height; /* 18 m */ - - int16_t v_batt; /* 20 battery voltage */ - int16_t sense_a; /* 22 apogee continuity sense */ - int16_t sense_m; /* 24 main continuity sense */ - - uint8_t pad[6]; /* 26 */ - /* 32 */ -}; - -#define AO_TELEMETRY_METRUM_DATA 0x0B - -struct ao_telemetry_metrum_data { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - - int32_t ground_pres; /* 8 average pres on pad */ - int16_t ground_accel; /* 12 average accel on pad */ - int16_t accel_plus_g; /* 14 accel calibration at +1g */ - int16_t accel_minus_g; /* 16 accel calibration at -1g */ - - uint8_t pad[14]; /* 18 */ - /* 32 */ -}; - -#define AO_TELEMETRY_MINI 0x10 - -struct ao_telemetry_mini { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - - uint8_t state; /* 5 flight state */ - int16_t v_batt; /* 6 battery voltage */ - int16_t sense_a; /* 8 apogee continuity */ - int16_t sense_m; /* 10 main continuity */ - - int32_t pres; /* 12 Pa * 10 */ - int16_t temp; /* 16 °C * 100 */ - - int16_t acceleration; /* 18 m/s² * 16 */ - int16_t speed; /* 20 m/s * 16 */ - int16_t height; /* 22 m */ - - int32_t ground_pres; /* 24 average pres on pad */ - - int32_t pad28; /* 28 */ - /* 32 */ -}; - -/* #define AO_SEND_ALL_BARO */ - -#define AO_TELEMETRY_BARO 0x80 - -/* - * This packet allows the full sampling rate baro - * data to be captured over the RF link so that the - * flight software can be tested using 'real' data. - * - * Along with this telemetry packet, the flight - * code is modified to send full-rate telemetry all the time - * and never send an RDF tone; this ensure that the full radio - * link is available. - */ -struct ao_telemetry_baro { - uint16_t serial; /* 0 */ - uint16_t tick; /* 2 */ - uint8_t type; /* 4 */ - uint8_t samples; /* 5 number samples */ - - int16_t baro[12]; /* 6 samples */ - /* 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; - struct ao_telemetry_companion companion; - struct ao_telemetry_mega_sensor mega_sensor; - struct ao_telemetry_mega_data mega_data; - struct ao_telemetry_metrum_sensor metrum_sensor; - struct ao_telemetry_metrum_data metrum_data; - struct ao_telemetry_mini mini; - struct ao_telemetry_baro baro; -}; - -struct ao_telemetry_all_recv { - union ao_telemetry_all telemetry; - int8_t rssi; - uint8_t status; -}; - -#endif /* _AO_TELEMETRY_H_ */