From: Keith Packard Date: Tue, 10 Jul 2012 22:11:36 +0000 (-0700) Subject: altos: Rename *_mm.c back to *.c X-Git-Tag: 1.1~118 X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=commitdiff_plain;h=1ae3f467a1d7be2fc3b1a45ba12568a3a25a0099 altos: Rename *_mm.c back to *.c Was just a temporary hack to keep cc1111 products building during MM development. Signed-off-by: Keith Packard --- diff --git a/src/core/ao_flight.c b/src/core/ao_flight.c new file mode 100644 index 00000000..a0affc48 --- /dev/null +++ b/src/core/ao_flight.c @@ -0,0 +1,418 @@ +/* + * Copyright © 2009 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_FLIGHT_TEST +#include "ao.h" +#include +#endif + +#ifndef HAS_ACCEL +#error Please define HAS_ACCEL +#endif + +#ifndef HAS_GPS +#error Please define HAS_GPS +#endif + +#ifndef HAS_USB +#error Please define HAS_USB +#endif + +#ifndef HAS_TELEMETRY +#define HAS_TELEMETRY HAS_RADIO +#endif + +/* Main flight thread. */ + +__pdata enum ao_flight_state ao_flight_state; /* current flight state */ +__pdata uint16_t ao_boost_tick; /* time of launch detect */ + +/* + * track min/max data over a long interval to detect + * resting + */ +static __data uint16_t ao_interval_end; +static __data int16_t ao_interval_min_height; +static __data int16_t ao_interval_max_height; +static __data int16_t ao_coast_avg_accel; + +__pdata uint8_t ao_flight_force_idle; + +/* We also have a clock, which can be used to sanity check things in + * case of other failures + */ + +#define BOOST_TICKS_MAX AO_SEC_TO_TICKS(15) + +/* Landing is detected by getting constant readings from both pressure and accelerometer + * for a fairly long time (AO_INTERVAL_TICKS) + */ +#define AO_INTERVAL_TICKS AO_SEC_TO_TICKS(10) + +#define abs(a) ((a) < 0 ? -(a) : (a)) + +void +ao_flight(void) +{ + ao_sample_init(); + ao_flight_state = ao_flight_startup; + for (;;) { + + /* + * Process ADC samples, just looping + * until the sensors are calibrated. + */ + if (!ao_sample()) + continue; + + switch (ao_flight_state) { + case ao_flight_startup: + + /* Check to see what mode we should go to. + * - Invalid mode if accel cal appears to be out + * - pad mode if we're upright, + * - idle mode otherwise + */ +#if HAS_ACCEL + if (ao_config.accel_plus_g == 0 || + ao_config.accel_minus_g == 0 || + ao_ground_accel < ao_config.accel_plus_g - ACCEL_NOSE_UP || + ao_ground_accel > ao_config.accel_minus_g + ACCEL_NOSE_UP) + { + /* Detected an accel value outside -1.5g to 1.5g + * (or uncalibrated values), so we go into invalid mode + */ + ao_flight_state = ao_flight_invalid; + +#if HAS_RADIO && PACKET_HAS_SLAVE + /* Turn on packet system in invalid mode on TeleMetrum */ + ao_packet_slave_start(); +#endif + } else +#endif + if (!ao_flight_force_idle +#if HAS_ACCEL + && ao_ground_accel < ao_config.accel_plus_g + ACCEL_NOSE_UP +#endif + ) + { + /* Set pad mode - we can fly! */ + ao_flight_state = ao_flight_pad; +#if HAS_USB && HAS_RADIO + /* Disable the USB controller in flight mode + * to save power + */ + ao_usb_disable(); +#endif + +#if !HAS_ACCEL + /* Disable packet mode in pad state on TeleMini */ + ao_packet_slave_stop(); +#endif + +#if HAS_TELEMETRY + /* Turn on telemetry system */ + ao_rdf_set(1); + ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_PAD); +#endif + /* signal successful initialization by turning off the LED */ + ao_led_off(AO_LED_RED); + } else { + /* Set idle mode */ + ao_flight_state = ao_flight_idle; + +#if HAS_ACCEL && HAS_RADIO && PACKET_HAS_SLAVE + /* Turn on packet system in idle mode on TeleMetrum */ + ao_packet_slave_start(); +#endif + + /* signal successful initialization by turning off the LED */ + ao_led_off(AO_LED_RED); + } + /* wakeup threads due to state change */ + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + + break; + case ao_flight_pad: + + /* pad to boost: + * + * barometer: > 20m vertical motion + * OR + * accelerometer: > 2g AND velocity > 5m/s + * + * The accelerometer should always detect motion before + * the barometer, but we use both to make sure this + * transition is detected. If the device + * doesn't have an accelerometer, then ignore the + * speed and acceleration as they are quite noisy + * on the pad. + */ + if (ao_height > AO_M_TO_HEIGHT(20) +#if HAS_ACCEL + || (ao_accel > AO_MSS_TO_ACCEL(20) && + ao_speed > AO_MS_TO_SPEED(5)) +#endif + ) + { + ao_flight_state = ao_flight_boost; + ao_boost_tick = ao_sample_tick; + + /* start logging data */ + ao_log_start(); + +#if HAS_TELEMETRY + /* Increase telemetry rate */ + ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_FLIGHT); + + /* disable RDF beacon */ + ao_rdf_set(0); +#endif + +#if HAS_GPS + /* Record current GPS position by waking up GPS log tasks */ + ao_wakeup(&ao_gps_data); + ao_wakeup(&ao_gps_tracking_data); +#endif + + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } + break; + case ao_flight_boost: + + /* boost to fast: + * + * accelerometer: start to fall at > 1/4 G + * OR + * time: boost for more than 15 seconds + * + * Detects motor burn out by the switch from acceleration to + * deceleration, or by waiting until the maximum burn duration + * (15 seconds) has past. + */ + if ((ao_accel < AO_MSS_TO_ACCEL(-2.5) && ao_height > AO_M_TO_HEIGHT(100)) || + (int16_t) (ao_sample_tick - ao_boost_tick) > BOOST_TICKS_MAX) + { +#if HAS_ACCEL + ao_flight_state = ao_flight_fast; + ao_coast_avg_accel = ao_accel; +#else + ao_flight_state = ao_flight_coast; +#endif + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } + break; +#if HAS_ACCEL + case ao_flight_fast: + /* + * This is essentially the same as coast, + * but the barometer is being ignored as + * it may be unreliable. + */ + if (ao_speed < AO_MS_TO_SPEED(AO_MAX_BARO_SPEED)) + { + ao_flight_state = ao_flight_coast; + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } else + goto check_re_boost; + break; +#endif + case ao_flight_coast: + + /* + * By customer request - allow the user + * to lock out apogee detection for a specified + * number of seconds. + */ + if (ao_config.apogee_lockout) { + if ((ao_sample_tick - ao_boost_tick) < + AO_SEC_TO_TICKS(ao_config.apogee_lockout)) + break; + } + + /* apogee detect: coast to drogue deploy: + * + * speed: < 0 + * + * Also make sure the model altitude is tracking + * the measured altitude reasonably closely; otherwise + * we're probably transsonic. + */ + if (ao_speed < 0 +#if !HAS_ACCEL + && (ao_sample_alt >= AO_MAX_BARO_HEIGHT || ao_error_h_sq_avg < 100) +#endif + ) + { +#if HAS_IGNITE + /* ignite the drogue charge */ + ao_ignite(ao_igniter_drogue); +#endif + +#if HAS_TELEMETRY + /* slow down the telemetry system */ + ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_RECOVER); + + /* Turn the RDF beacon back on */ + ao_rdf_set(1); +#endif + + /* and enter drogue state */ + ao_flight_state = ao_flight_drogue; + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } +#if HAS_ACCEL + else { + check_re_boost: + ao_coast_avg_accel = ao_coast_avg_accel - (ao_coast_avg_accel >> 6) + (ao_accel >> 6); + if (ao_coast_avg_accel > AO_MSS_TO_ACCEL(20)) { + ao_boost_tick = ao_sample_tick; + ao_flight_state = ao_flight_boost; + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } + } +#endif + + break; + case ao_flight_drogue: + + /* drogue to main deploy: + * + * barometer: reach main deploy altitude + * + * Would like to use the accelerometer for this test, but + * the orientation of the flight computer is unknown after + * drogue deploy, so we ignore it. Could also detect + * high descent rate using the pressure sensor to + * recognize drogue deploy failure and eject the main + * at that point. Perhaps also use the drogue sense lines + * to notice continutity? + */ + if (ao_height <= ao_config.main_deploy) + { +#if HAS_IGNITE + ao_ignite(ao_igniter_main); +#endif + + /* + * Start recording min/max height + * to figure out when the rocket has landed + */ + + /* initialize interval values */ + ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS; + + ao_interval_min_height = ao_interval_max_height = ao_avg_height; + + ao_flight_state = ao_flight_main; + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } + break; + + /* fall through... */ + case ao_flight_main: + + /* main to land: + * + * barometer: altitude stable + */ + + if (ao_avg_height < ao_interval_min_height) + ao_interval_min_height = ao_avg_height; + if (ao_avg_height > ao_interval_max_height) + ao_interval_max_height = ao_avg_height; + + if ((int16_t) (ao_sample_tick - ao_interval_end) >= 0) { + if (ao_interval_max_height - ao_interval_min_height <= AO_M_TO_HEIGHT(4)) + { + ao_flight_state = ao_flight_landed; + + /* turn off the ADC capture */ + ao_timer_set_adc_interval(0); + + ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); + } + ao_interval_min_height = ao_interval_max_height = ao_avg_height; + ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS; + } + break; + case ao_flight_landed: + break; + } + } +} + +#if !HAS_RADIO +static inline int int_part(int16_t i) { return i >> 4; } +static inline int frac_part(int16_t i) { return ((i & 0xf) * 100 + 8) / 16; } + +static void +ao_flight_dump(void) +{ +#if HAS_ACCEL + int16_t accel; + + accel = ((ao_ground_accel - ao_sample_accel) * ao_accel_scale) >> 16; +#endif + + printf ("sample:\n"); + printf (" tick %d\n", ao_sample_tick); + printf (" raw pres %d\n", ao_sample_pres); +#if HAS_ACCEL + printf (" raw accel %d\n", ao_sample_accel); +#endif + printf (" ground pres %d\n", ao_ground_pres); +#if HAS_ACCEL + printf (" raw accel %d\n", ao_sample_accel); + printf (" groundaccel %d\n", ao_ground_accel); + printf (" accel_2g %d\n", ao_accel_2g); +#endif + + printf (" alt %d\n", ao_sample_alt); + printf (" height %d\n", ao_sample_height); +#if HAS_ACCEL + printf (" accel %d.%02d\n", int_part(accel), frac_part(accel)); +#endif + + + printf ("kalman:\n"); + printf (" height %d\n", ao_height); + printf (" speed %d.%02d\n", int_part(ao_speed), frac_part(ao_speed)); + printf (" accel %d.%02d\n", int_part(ao_accel), frac_part(ao_accel)); + printf (" max_height %d\n", ao_max_height); + printf (" avg_height %d\n", ao_avg_height); + printf (" error_h %d\n", ao_error_h); + printf (" error_avg %d\n", ao_error_h_sq_avg); +} + +__code struct ao_cmds ao_flight_cmds[] = { + { ao_flight_dump, "F\0Dump flight status" }, + { 0, NULL }, +}; +#endif + +static __xdata struct ao_task flight_task; + +void +ao_flight_init(void) +{ + ao_flight_state = ao_flight_startup; +#if !HAS_RADIO + ao_cmd_register(&ao_flight_cmds[0]); +#endif + ao_add_task(&flight_task, ao_flight, "flight"); +} diff --git a/src/core/ao_flight_mm.c b/src/core/ao_flight_mm.c deleted file mode 100644 index a0affc48..00000000 --- a/src/core/ao_flight_mm.c +++ /dev/null @@ -1,418 +0,0 @@ -/* - * Copyright © 2009 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_FLIGHT_TEST -#include "ao.h" -#include -#endif - -#ifndef HAS_ACCEL -#error Please define HAS_ACCEL -#endif - -#ifndef HAS_GPS -#error Please define HAS_GPS -#endif - -#ifndef HAS_USB -#error Please define HAS_USB -#endif - -#ifndef HAS_TELEMETRY -#define HAS_TELEMETRY HAS_RADIO -#endif - -/* Main flight thread. */ - -__pdata enum ao_flight_state ao_flight_state; /* current flight state */ -__pdata uint16_t ao_boost_tick; /* time of launch detect */ - -/* - * track min/max data over a long interval to detect - * resting - */ -static __data uint16_t ao_interval_end; -static __data int16_t ao_interval_min_height; -static __data int16_t ao_interval_max_height; -static __data int16_t ao_coast_avg_accel; - -__pdata uint8_t ao_flight_force_idle; - -/* We also have a clock, which can be used to sanity check things in - * case of other failures - */ - -#define BOOST_TICKS_MAX AO_SEC_TO_TICKS(15) - -/* Landing is detected by getting constant readings from both pressure and accelerometer - * for a fairly long time (AO_INTERVAL_TICKS) - */ -#define AO_INTERVAL_TICKS AO_SEC_TO_TICKS(10) - -#define abs(a) ((a) < 0 ? -(a) : (a)) - -void -ao_flight(void) -{ - ao_sample_init(); - ao_flight_state = ao_flight_startup; - for (;;) { - - /* - * Process ADC samples, just looping - * until the sensors are calibrated. - */ - if (!ao_sample()) - continue; - - switch (ao_flight_state) { - case ao_flight_startup: - - /* Check to see what mode we should go to. - * - Invalid mode if accel cal appears to be out - * - pad mode if we're upright, - * - idle mode otherwise - */ -#if HAS_ACCEL - if (ao_config.accel_plus_g == 0 || - ao_config.accel_minus_g == 0 || - ao_ground_accel < ao_config.accel_plus_g - ACCEL_NOSE_UP || - ao_ground_accel > ao_config.accel_minus_g + ACCEL_NOSE_UP) - { - /* Detected an accel value outside -1.5g to 1.5g - * (or uncalibrated values), so we go into invalid mode - */ - ao_flight_state = ao_flight_invalid; - -#if HAS_RADIO && PACKET_HAS_SLAVE - /* Turn on packet system in invalid mode on TeleMetrum */ - ao_packet_slave_start(); -#endif - } else -#endif - if (!ao_flight_force_idle -#if HAS_ACCEL - && ao_ground_accel < ao_config.accel_plus_g + ACCEL_NOSE_UP -#endif - ) - { - /* Set pad mode - we can fly! */ - ao_flight_state = ao_flight_pad; -#if HAS_USB && HAS_RADIO - /* Disable the USB controller in flight mode - * to save power - */ - ao_usb_disable(); -#endif - -#if !HAS_ACCEL - /* Disable packet mode in pad state on TeleMini */ - ao_packet_slave_stop(); -#endif - -#if HAS_TELEMETRY - /* Turn on telemetry system */ - ao_rdf_set(1); - ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_PAD); -#endif - /* signal successful initialization by turning off the LED */ - ao_led_off(AO_LED_RED); - } else { - /* Set idle mode */ - ao_flight_state = ao_flight_idle; - -#if HAS_ACCEL && HAS_RADIO && PACKET_HAS_SLAVE - /* Turn on packet system in idle mode on TeleMetrum */ - ao_packet_slave_start(); -#endif - - /* signal successful initialization by turning off the LED */ - ao_led_off(AO_LED_RED); - } - /* wakeup threads due to state change */ - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - - break; - case ao_flight_pad: - - /* pad to boost: - * - * barometer: > 20m vertical motion - * OR - * accelerometer: > 2g AND velocity > 5m/s - * - * The accelerometer should always detect motion before - * the barometer, but we use both to make sure this - * transition is detected. If the device - * doesn't have an accelerometer, then ignore the - * speed and acceleration as they are quite noisy - * on the pad. - */ - if (ao_height > AO_M_TO_HEIGHT(20) -#if HAS_ACCEL - || (ao_accel > AO_MSS_TO_ACCEL(20) && - ao_speed > AO_MS_TO_SPEED(5)) -#endif - ) - { - ao_flight_state = ao_flight_boost; - ao_boost_tick = ao_sample_tick; - - /* start logging data */ - ao_log_start(); - -#if HAS_TELEMETRY - /* Increase telemetry rate */ - ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_FLIGHT); - - /* disable RDF beacon */ - ao_rdf_set(0); -#endif - -#if HAS_GPS - /* Record current GPS position by waking up GPS log tasks */ - ao_wakeup(&ao_gps_data); - ao_wakeup(&ao_gps_tracking_data); -#endif - - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } - break; - case ao_flight_boost: - - /* boost to fast: - * - * accelerometer: start to fall at > 1/4 G - * OR - * time: boost for more than 15 seconds - * - * Detects motor burn out by the switch from acceleration to - * deceleration, or by waiting until the maximum burn duration - * (15 seconds) has past. - */ - if ((ao_accel < AO_MSS_TO_ACCEL(-2.5) && ao_height > AO_M_TO_HEIGHT(100)) || - (int16_t) (ao_sample_tick - ao_boost_tick) > BOOST_TICKS_MAX) - { -#if HAS_ACCEL - ao_flight_state = ao_flight_fast; - ao_coast_avg_accel = ao_accel; -#else - ao_flight_state = ao_flight_coast; -#endif - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } - break; -#if HAS_ACCEL - case ao_flight_fast: - /* - * This is essentially the same as coast, - * but the barometer is being ignored as - * it may be unreliable. - */ - if (ao_speed < AO_MS_TO_SPEED(AO_MAX_BARO_SPEED)) - { - ao_flight_state = ao_flight_coast; - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } else - goto check_re_boost; - break; -#endif - case ao_flight_coast: - - /* - * By customer request - allow the user - * to lock out apogee detection for a specified - * number of seconds. - */ - if (ao_config.apogee_lockout) { - if ((ao_sample_tick - ao_boost_tick) < - AO_SEC_TO_TICKS(ao_config.apogee_lockout)) - break; - } - - /* apogee detect: coast to drogue deploy: - * - * speed: < 0 - * - * Also make sure the model altitude is tracking - * the measured altitude reasonably closely; otherwise - * we're probably transsonic. - */ - if (ao_speed < 0 -#if !HAS_ACCEL - && (ao_sample_alt >= AO_MAX_BARO_HEIGHT || ao_error_h_sq_avg < 100) -#endif - ) - { -#if HAS_IGNITE - /* ignite the drogue charge */ - ao_ignite(ao_igniter_drogue); -#endif - -#if HAS_TELEMETRY - /* slow down the telemetry system */ - ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_RECOVER); - - /* Turn the RDF beacon back on */ - ao_rdf_set(1); -#endif - - /* and enter drogue state */ - ao_flight_state = ao_flight_drogue; - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } -#if HAS_ACCEL - else { - check_re_boost: - ao_coast_avg_accel = ao_coast_avg_accel - (ao_coast_avg_accel >> 6) + (ao_accel >> 6); - if (ao_coast_avg_accel > AO_MSS_TO_ACCEL(20)) { - ao_boost_tick = ao_sample_tick; - ao_flight_state = ao_flight_boost; - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } - } -#endif - - break; - case ao_flight_drogue: - - /* drogue to main deploy: - * - * barometer: reach main deploy altitude - * - * Would like to use the accelerometer for this test, but - * the orientation of the flight computer is unknown after - * drogue deploy, so we ignore it. Could also detect - * high descent rate using the pressure sensor to - * recognize drogue deploy failure and eject the main - * at that point. Perhaps also use the drogue sense lines - * to notice continutity? - */ - if (ao_height <= ao_config.main_deploy) - { -#if HAS_IGNITE - ao_ignite(ao_igniter_main); -#endif - - /* - * Start recording min/max height - * to figure out when the rocket has landed - */ - - /* initialize interval values */ - ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS; - - ao_interval_min_height = ao_interval_max_height = ao_avg_height; - - ao_flight_state = ao_flight_main; - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } - break; - - /* fall through... */ - case ao_flight_main: - - /* main to land: - * - * barometer: altitude stable - */ - - if (ao_avg_height < ao_interval_min_height) - ao_interval_min_height = ao_avg_height; - if (ao_avg_height > ao_interval_max_height) - ao_interval_max_height = ao_avg_height; - - if ((int16_t) (ao_sample_tick - ao_interval_end) >= 0) { - if (ao_interval_max_height - ao_interval_min_height <= AO_M_TO_HEIGHT(4)) - { - ao_flight_state = ao_flight_landed; - - /* turn off the ADC capture */ - ao_timer_set_adc_interval(0); - - ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); - } - ao_interval_min_height = ao_interval_max_height = ao_avg_height; - ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS; - } - break; - case ao_flight_landed: - break; - } - } -} - -#if !HAS_RADIO -static inline int int_part(int16_t i) { return i >> 4; } -static inline int frac_part(int16_t i) { return ((i & 0xf) * 100 + 8) / 16; } - -static void -ao_flight_dump(void) -{ -#if HAS_ACCEL - int16_t accel; - - accel = ((ao_ground_accel - ao_sample_accel) * ao_accel_scale) >> 16; -#endif - - printf ("sample:\n"); - printf (" tick %d\n", ao_sample_tick); - printf (" raw pres %d\n", ao_sample_pres); -#if HAS_ACCEL - printf (" raw accel %d\n", ao_sample_accel); -#endif - printf (" ground pres %d\n", ao_ground_pres); -#if HAS_ACCEL - printf (" raw accel %d\n", ao_sample_accel); - printf (" groundaccel %d\n", ao_ground_accel); - printf (" accel_2g %d\n", ao_accel_2g); -#endif - - printf (" alt %d\n", ao_sample_alt); - printf (" height %d\n", ao_sample_height); -#if HAS_ACCEL - printf (" accel %d.%02d\n", int_part(accel), frac_part(accel)); -#endif - - - printf ("kalman:\n"); - printf (" height %d\n", ao_height); - printf (" speed %d.%02d\n", int_part(ao_speed), frac_part(ao_speed)); - printf (" accel %d.%02d\n", int_part(ao_accel), frac_part(ao_accel)); - printf (" max_height %d\n", ao_max_height); - printf (" avg_height %d\n", ao_avg_height); - printf (" error_h %d\n", ao_error_h); - printf (" error_avg %d\n", ao_error_h_sq_avg); -} - -__code struct ao_cmds ao_flight_cmds[] = { - { ao_flight_dump, "F\0Dump flight status" }, - { 0, NULL }, -}; -#endif - -static __xdata struct ao_task flight_task; - -void -ao_flight_init(void) -{ - ao_flight_state = ao_flight_startup; -#if !HAS_RADIO - ao_cmd_register(&ao_flight_cmds[0]); -#endif - ao_add_task(&flight_task, ao_flight, "flight"); -} diff --git a/src/core/ao_sample.c b/src/core/ao_sample.c new file mode 100644 index 00000000..ac11eef0 --- /dev/null +++ b/src/core/ao_sample.c @@ -0,0 +1,138 @@ +/* + * Copyright © 2011 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_FLIGHT_TEST +#include "ao.h" +#include +#endif + +/* + * Current sensor values + */ + +#ifndef PRES_TYPE +#define PRES_TYPE int32_t +#define ALT_TYPE int32_t +#define ACCEL_TYPE int16_t +#endif + +__pdata uint16_t ao_sample_tick; /* time of last data */ +__pdata pres_t ao_sample_pres; +__pdata alt_t ao_sample_alt; +__pdata alt_t ao_sample_height; +#if HAS_ACCEL +__pdata accel_t ao_sample_accel; +#endif + +__data uint8_t ao_sample_data; + +/* + * Sensor calibration values + */ + +__pdata pres_t ao_ground_pres; /* startup pressure */ +__pdata alt_t ao_ground_height; /* MSL of ao_ground_pres */ + +#if HAS_ACCEL +__pdata accel_t ao_ground_accel; /* startup acceleration */ +__pdata accel_t ao_accel_2g; /* factory accel calibration */ +__pdata int32_t ao_accel_scale; /* sensor to m/s² conversion */ +#endif + +static __pdata uint8_t ao_preflight; /* in preflight mode */ + +static __pdata uint16_t nsamples; +__pdata int32_t ao_sample_pres_sum; +#if HAS_ACCEL +__pdata int32_t ao_sample_accel_sum; +#endif + +static void +ao_sample_preflight(void) +{ + /* startup state: + * + * Collect 512 samples of acceleration and pressure + * data and average them to find the resting values + */ + if (nsamples < 512) { +#if HAS_ACCEL + ao_sample_accel_sum += ao_sample_accel; +#endif + ao_sample_pres_sum += ao_sample_pres; + ++nsamples; + } else { + ao_config_get(); +#if HAS_ACCEL + ao_ground_accel = ao_sample_accel_sum >> 9; + ao_accel_2g = ao_config.accel_minus_g - ao_config.accel_plus_g; + ao_accel_scale = to_fix32(GRAVITY * 2 * 16) / ao_accel_2g; +#endif + ao_ground_pres = ao_sample_pres_sum >> 9; + ao_ground_height = pres_to_altitude(ao_ground_pres); + ao_preflight = FALSE; + } +} + + +uint8_t +ao_sample(void) +{ + ao_config_get(); + ao_wakeup(DATA_TO_XDATA(&ao_sample_data)); + ao_sleep((void *) DATA_TO_XDATA(&ao_data_head)); + while (ao_sample_data != ao_data_head) { + __xdata struct ao_data *ao_data; + + /* Capture a sample */ + ao_data = (struct ao_data *) &ao_data_ring[ao_sample_data]; + ao_sample_tick = ao_data->tick; + + ao_data_pres_cook(ao_data); + ao_sample_pres = ao_data_pres(ao_data); + ao_sample_alt = pres_to_altitude(ao_sample_pres); + ao_sample_height = ao_sample_alt - ao_ground_height; + +#if HAS_ACCEL + ao_sample_accel = ao_data_accel_cook(ao_data); + if (ao_config.pad_orientation != AO_PAD_ORIENTATION_ANTENNA_UP) + ao_sample_accel = ao_data_accel_invert(ao_sample_accel); + ao_data_set_accel(ao_data, ao_sample_accel); +#endif + + if (ao_preflight) + ao_sample_preflight(); + else + ao_kalman(); + ao_sample_data = ao_data_ring_next(ao_sample_data); + } + return !ao_preflight; +} + +void +ao_sample_init(void) +{ + nsamples = 0; + ao_sample_pres_sum = 0; + ao_sample_pres = 0; +#if HAS_ACCEL + ao_sample_accel_sum = 0; + ao_sample_accel = 0; +#endif + ao_sample_data = ao_data_head; + ao_preflight = TRUE; +} diff --git a/src/core/ao_sample_mm.c b/src/core/ao_sample_mm.c deleted file mode 100644 index ac11eef0..00000000 --- a/src/core/ao_sample_mm.c +++ /dev/null @@ -1,138 +0,0 @@ -/* - * Copyright © 2011 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_FLIGHT_TEST -#include "ao.h" -#include -#endif - -/* - * Current sensor values - */ - -#ifndef PRES_TYPE -#define PRES_TYPE int32_t -#define ALT_TYPE int32_t -#define ACCEL_TYPE int16_t -#endif - -__pdata uint16_t ao_sample_tick; /* time of last data */ -__pdata pres_t ao_sample_pres; -__pdata alt_t ao_sample_alt; -__pdata alt_t ao_sample_height; -#if HAS_ACCEL -__pdata accel_t ao_sample_accel; -#endif - -__data uint8_t ao_sample_data; - -/* - * Sensor calibration values - */ - -__pdata pres_t ao_ground_pres; /* startup pressure */ -__pdata alt_t ao_ground_height; /* MSL of ao_ground_pres */ - -#if HAS_ACCEL -__pdata accel_t ao_ground_accel; /* startup acceleration */ -__pdata accel_t ao_accel_2g; /* factory accel calibration */ -__pdata int32_t ao_accel_scale; /* sensor to m/s² conversion */ -#endif - -static __pdata uint8_t ao_preflight; /* in preflight mode */ - -static __pdata uint16_t nsamples; -__pdata int32_t ao_sample_pres_sum; -#if HAS_ACCEL -__pdata int32_t ao_sample_accel_sum; -#endif - -static void -ao_sample_preflight(void) -{ - /* startup state: - * - * Collect 512 samples of acceleration and pressure - * data and average them to find the resting values - */ - if (nsamples < 512) { -#if HAS_ACCEL - ao_sample_accel_sum += ao_sample_accel; -#endif - ao_sample_pres_sum += ao_sample_pres; - ++nsamples; - } else { - ao_config_get(); -#if HAS_ACCEL - ao_ground_accel = ao_sample_accel_sum >> 9; - ao_accel_2g = ao_config.accel_minus_g - ao_config.accel_plus_g; - ao_accel_scale = to_fix32(GRAVITY * 2 * 16) / ao_accel_2g; -#endif - ao_ground_pres = ao_sample_pres_sum >> 9; - ao_ground_height = pres_to_altitude(ao_ground_pres); - ao_preflight = FALSE; - } -} - - -uint8_t -ao_sample(void) -{ - ao_config_get(); - ao_wakeup(DATA_TO_XDATA(&ao_sample_data)); - ao_sleep((void *) DATA_TO_XDATA(&ao_data_head)); - while (ao_sample_data != ao_data_head) { - __xdata struct ao_data *ao_data; - - /* Capture a sample */ - ao_data = (struct ao_data *) &ao_data_ring[ao_sample_data]; - ao_sample_tick = ao_data->tick; - - ao_data_pres_cook(ao_data); - ao_sample_pres = ao_data_pres(ao_data); - ao_sample_alt = pres_to_altitude(ao_sample_pres); - ao_sample_height = ao_sample_alt - ao_ground_height; - -#if HAS_ACCEL - ao_sample_accel = ao_data_accel_cook(ao_data); - if (ao_config.pad_orientation != AO_PAD_ORIENTATION_ANTENNA_UP) - ao_sample_accel = ao_data_accel_invert(ao_sample_accel); - ao_data_set_accel(ao_data, ao_sample_accel); -#endif - - if (ao_preflight) - ao_sample_preflight(); - else - ao_kalman(); - ao_sample_data = ao_data_ring_next(ao_sample_data); - } - return !ao_preflight; -} - -void -ao_sample_init(void) -{ - nsamples = 0; - ao_sample_pres_sum = 0; - ao_sample_pres = 0; -#if HAS_ACCEL - ao_sample_accel_sum = 0; - ao_sample_accel = 0; -#endif - ao_sample_data = ao_data_head; - ao_preflight = TRUE; -} diff --git a/src/megametrum-v0.1/Makefile b/src/megametrum-v0.1/Makefile index 6fc9324e..13e46c97 100644 --- a/src/megametrum-v0.1/Makefile +++ b/src/megametrum-v0.1/Makefile @@ -67,9 +67,9 @@ ALTOS_SRC = \ ao_convert_pa.c \ ao_log.c \ ao_log_mega.c \ - ao_sample_mm.c \ + ao_sample.c \ ao_kalman.c \ - ao_flight_mm.c \ + ao_flight.c \ ao_telemetry.c \ ao_packet_slave.c \ ao_packet.c \ diff --git a/src/product/Makefile.telemetrum b/src/product/Makefile.telemetrum index fba2c19a..57586c95 100644 --- a/src/product/Makefile.telemetrum +++ b/src/product/Makefile.telemetrum @@ -36,8 +36,8 @@ CORE_SRC = \ ao_stdio.c \ ao_storage.c \ ao_task.c \ - ao_flight_mm.c \ - ao_sample_mm.c \ + ao_flight.c \ + ao_sample.c \ ao_kalman.c \ ao_log.c \ ao_log_big.c \ diff --git a/src/product/Makefile.telemini b/src/product/Makefile.telemini index f0ab2b14..23aed1c7 100644 --- a/src/product/Makefile.telemini +++ b/src/product/Makefile.telemini @@ -24,14 +24,14 @@ CORE_SRC = \ ao_cmd.c \ ao_config.c \ ao_convert.c \ - ao_flight_mm.c \ + ao_flight.c \ ao_kalman.c \ ao_log.c \ ao_log_tiny.c \ ao_mutex.c \ ao_panic.c \ ao_report.c \ - ao_sample_mm.c \ + ao_sample.c \ ao_stdio.c \ ao_storage.c \ ao_task.c \ diff --git a/src/product/Makefile.telenano b/src/product/Makefile.telenano index a55bcf95..ca719bbf 100644 --- a/src/product/Makefile.telenano +++ b/src/product/Makefile.telenano @@ -31,7 +31,7 @@ CORE_SRC = \ ao_mutex.c \ ao_panic.c \ ao_report.c \ - ao_sample_mm.c \ + ao_sample.c \ ao_stdio.c \ ao_storage.c \ ao_task.c \ diff --git a/src/test/Makefile b/src/test/Makefile index 4631fb78..963f4131 100644 --- a/src/test/Makefile +++ b/src/test/Makefile @@ -4,7 +4,7 @@ PROGS=ao_flight_test ao_flight_test_baro ao_flight_test_accel ao_flight_test_noi KALMAN=make-kalman -CFLAGS=-I.. -I. -I../core -I../drivers -O0 -g -Wall +CFLAGS=-I.. -I. -I../core -I../drivers -O3 -g -Wall all: $(PROGS) @@ -13,10 +13,10 @@ clean: install: -ao_flight_test: ao_flight_test.c ao_host.h ao_flight_mm.c ao_sample_mm.c ao_kalman.c altitude.h ao_kalman.h +ao_flight_test: ao_flight_test.c ao_host.h ao_flight.c ao_sample.c ao_kalman.c altitude.h ao_kalman.h cc $(CFLAGS) -o $@ $< -ao_flight_test_noisy_accel: ao_flight_test.c ao_host.h ao_flight_mm.c ao_sample_mm.c ao_kalman.c altitude.h ao_kalman.h +ao_flight_test_noisy_accel: ao_flight_test.c ao_host.h ao_flight.c ao_sample.c ao_kalman.c altitude.h ao_kalman.h cc -DNOISY_ACCEL=1 $(CFLAGS) -o $@ $< ao_flight_test_baro: ao_flight_test.c ao_host.h ao_flight.c ao_sample.c ao_kalman.c altitude.h ao_kalman.h @@ -42,3 +42,6 @@ ao_kalman.h: $(KALMAN) ao_fec_test: ao_fec_test.c ao_fec_tx.c ao_fec_rx.c cc $(CFLAGS) -DAO_FEC_DEBUG=1 -o $@ ao_fec_test.c ../core/ao_fec_tx.c ../core/ao_fec_rx.c -lm + +check: ao_fec_test ao_flight_test ao_flight_test_baro run-tests + ./ao_fec_test && ./run-tests \ No newline at end of file diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index baf2ad1d..9bb03d68 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -141,7 +141,7 @@ 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 +156,7 @@ 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 */ @@ -199,6 +200,7 @@ struct ao_config ao_config; #define DATA_TO_XDATA(x) (x) #define HAS_FLIGHT 1 +#define HAS_IGNITE 1 #define HAS_ADC 1 #define HAS_USB 1 #define HAS_GPS 1 @@ -223,8 +225,8 @@ 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_sample.c" +#include "ao_flight.c" #define to_double(f) ((f) / 65536.0) @@ -259,10 +261,11 @@ 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); @@ -477,10 +480,9 @@ 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]; @@ -676,13 +678,15 @@ 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 +698,14 @@ 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 +713,14 @@ 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 +728,8 @@ 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); }