From 52063c2679752033135fff928c7686e368d2a825 Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Sat, 18 May 2013 02:54:30 -0700 Subject: altos: ao_data_get is in ao_data.c now, not ao_adc.c Signed-off-by: Keith Packard --- src/core/ao_data.h | 4 ++++ 1 file changed, 4 insertions(+) (limited to 'src/core/ao_data.h') diff --git a/src/core/ao_data.h b/src/core/ao_data.h index 7e2f85d8..b0f086f8 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -82,6 +82,10 @@ struct ao_data { #define ao_data_ring_next(n) (((n) + 1) & (AO_DATA_RING - 1)) #define ao_data_ring_prev(n) (((n) - 1) & (AO_DATA_RING - 1)) +/* Get a copy of the last complete sample set */ +void +ao_data_get(__xdata struct ao_data *packet); + extern volatile __xdata struct ao_data ao_data_ring[AO_DATA_RING]; extern volatile __data uint8_t ao_data_head; extern volatile __data uint8_t ao_data_present; -- cgit v1.2.3 From d0b4e926ecececa7499a301b6135189be119512e Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Wed, 22 May 2013 13:03:06 -0700 Subject: Initial TeleMini bits Signed-off-by: Keith Packard --- src/cc1111/ao_adc.c | 5 ++ src/cc1111/ao_usb.c | 5 ++ src/core/ao_data.c | 2 + src/core/ao_data.h | 2 +- src/core/ao_log_mini.c | 1 - src/core/ao_telemetry.c | 40 +++++++++- src/core/ao_telemetry.h | 27 +++++++ src/drivers/ao_ms5607.c | 40 +++++----- src/drivers/ao_ms5607.h | 2 +- src/drivers/ao_ms5607_convert_8051.c | 60 +++++++++++++++ src/telemini-v2.0/Makefile | 108 +++++++++++++++++++++++++++ src/telemini-v2.0/ao_pins.h | 140 +++++++++++++++++++++++++++++++++++ src/telemini-v2.0/ao_telemini.c | 54 ++++++++++++++ src/test/Makefile | 5 +- 14 files changed, 466 insertions(+), 25 deletions(-) create mode 100644 src/drivers/ao_ms5607_convert_8051.c create mode 100644 src/telemini-v2.0/Makefile create mode 100644 src/telemini-v2.0/ao_pins.h create mode 100644 src/telemini-v2.0/ao_telemini.c (limited to 'src/core/ao_data.h') diff --git a/src/cc1111/ao_adc.c b/src/cc1111/ao_adc.c index 4a58023d..6cc08399 100644 --- a/src/cc1111/ao_adc.c +++ b/src/cc1111/ao_adc.c @@ -162,6 +162,11 @@ ao_adc_isr(void) __interrupt 1 #define GOT_ADC #endif +#ifdef FETCH_ADC + FETCH_ADC() +#define GOT_ADC +#endif + #ifndef GOT_ADC #error No known ADC configuration set #endif diff --git a/src/cc1111/ao_usb.c b/src/cc1111/ao_usb.c index a655d1be..b0ab409d 100644 --- a/src/cc1111/ao_usb.c +++ b/src/cc1111/ao_usb.c @@ -201,6 +201,11 @@ ao_usb_ep0_setup(void) ao_usb_ep0_queue_byte(0); break; case AO_USB_REQ_SET_ADDRESS: +#if USB_FORCE_FLIGHT_IDLE + /* Go to idle mode if USB is connected + */ + ao_flight_force_idle = 1; +#endif ao_usb_set_address(ao_usb_setup.value); break; case AO_USB_REQ_GET_DESCRIPTOR: diff --git a/src/core/ao_data.c b/src/core/ao_data.c index 38d2f7ff..6a3d02a1 100644 --- a/src/core/ao_data.c +++ b/src/core/ao_data.c @@ -22,6 +22,7 @@ volatile __xdata struct ao_data ao_data_ring[AO_DATA_RING]; volatile __data uint8_t ao_data_head; volatile __data uint8_t ao_data_present; +#ifndef ao_data_count void ao_data_get(__xdata struct ao_data *packet) { @@ -32,3 +33,4 @@ ao_data_get(__xdata struct ao_data *packet) #endif memcpy(packet, (void *) &ao_data_ring[i], sizeof (struct ao_data)); } +#endif diff --git a/src/core/ao_data.h b/src/core/ao_data.h index b0f086f8..080a534f 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -101,7 +101,7 @@ extern volatile __data uint8_t ao_data_count; * signaled by the timer tick */ #define AO_DATA_WAIT() do { \ - ao_sleep((void *) &ao_data_count); \ + ao_sleep(DATA_TO_XDATA ((void *) &ao_data_count)); \ } while (0) #endif /* AO_DATA_RING */ diff --git a/src/core/ao_log_mini.c b/src/core/ao_log_mini.c index 1273b0e3..46b285f3 100644 --- a/src/core/ao_log_mini.c +++ b/src/core/ao_log_mini.c @@ -79,7 +79,6 @@ void ao_log(void) { __pdata uint16_t next_sensor, next_other; - uint8_t i; ao_storage_setup(); diff --git a/src/core/ao_telemetry.c b/src/core/ao_telemetry.c index 03a8a273..9c673030 100644 --- a/src/core/ao_telemetry.c +++ b/src/core/ao_telemetry.c @@ -171,6 +171,36 @@ ao_send_mega_data(void) } #endif /* AO_SEND_MEGA */ +#ifdef AO_SEND_MINI + +static void +ao_send_mini(void) +{ + __xdata struct ao_data *packet = (__xdata struct ao_data *) &ao_data_ring[ao_data_ring_prev(ao_sample_data)]; + + telemetry.generic.tick = packet->tick; + telemetry.generic.type = AO_TELEMETRY_MINI; + + telemetry.mini.state = ao_flight_state; + + telemetry.mini.v_batt = packet->adc.v_batt; + telemetry.mini.sense_a = packet->adc.sense_a; + telemetry.mini.sense_m = packet->adc.sense_m; + + telemetry.mini.pres = ao_data_pres(packet); + telemetry.mini.temp = ao_data_temp(packet); + + telemetry.mini.acceleration = ao_accel; + telemetry.mini.speed = ao_speed; + telemetry.mini.height = ao_height; + + telemetry.mini.ground_pres = ao_ground_pres; + + ao_radio_send(&telemetry, sizeof (telemetry)); +} + +#endif + #ifdef AO_SEND_ALL_BARO static uint8_t ao_baro_sample; @@ -323,12 +353,16 @@ ao_telemetry(void) ao_send_baro(); #endif #if HAS_FLIGHT -#ifdef AO_SEND_MEGA +# ifdef AO_SEND_MEGA ao_send_mega_sensor(); ao_send_mega_data(); -#else +# else +# ifdef AO_SEND_MINI + ao_send_mini(); +# else ao_send_sensor(); -#endif +# endif +# endif #endif #if HAS_COMPANION diff --git a/src/core/ao_telemetry.h b/src/core/ao_telemetry.h index f2d201de..77601529 100644 --- a/src/core/ao_telemetry.h +++ b/src/core/ao_telemetry.h @@ -207,6 +207,32 @@ struct ao_telemetry_mega_data { }; +#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 @@ -240,6 +266,7 @@ union ao_telemetry_all { struct ao_telemetry_companion companion; struct ao_telemetry_mega_sensor mega_sensor; struct ao_telemetry_mega_data mega_data; + struct ao_telemetry_mini mini; struct ao_telemetry_baro baro; }; diff --git a/src/drivers/ao_ms5607.c b/src/drivers/ao_ms5607.c index 8f1dcbe1..5259b265 100644 --- a/src/drivers/ao_ms5607.c +++ b/src/drivers/ao_ms5607.c @@ -21,7 +21,7 @@ #if HAS_MS5607 || HAS_MS5611 -static struct ao_ms5607_prom ms5607_prom; +static __xdata struct ao_ms5607_prom ms5607_prom; static uint8_t ms5607_configured; static void @@ -40,7 +40,7 @@ ao_ms5607_reset(void) { cmd = AO_MS5607_RESET; ao_ms5607_start(); - ao_spi_send(&cmd, 1, AO_MS5607_SPI_INDEX); + ao_spi_send(DATA_TO_XDATA(&cmd), 1, AO_MS5607_SPI_INDEX); ao_delay(AO_MS_TO_TICKS(10)); ao_ms5607_stop(); } @@ -69,17 +69,17 @@ ao_ms5607_crc(uint8_t *prom) } static void -ao_ms5607_prom_read(struct ao_ms5607_prom *prom) +ao_ms5607_prom_read(__xdata struct ao_ms5607_prom *prom) { - uint8_t addr; - uint8_t crc; - uint16_t *r; + uint8_t addr; + uint8_t crc; + __xdata uint16_t *r; - r = (uint16_t *) prom; + r = (__xdata uint16_t *) prom; for (addr = 0; addr < 8; addr++) { uint8_t cmd = AO_MS5607_PROM_READ(addr); ao_ms5607_start(); - ao_spi_send(&cmd, 1, AO_MS5607_SPI_INDEX); + ao_spi_send(DATA_TO_XDATA(&cmd), 1, AO_MS5607_SPI_INDEX); ao_spi_recv(r, 2, AO_MS5607_SPI_INDEX); ao_ms5607_stop(); r++; @@ -114,25 +114,25 @@ ao_ms5607_setup(void) ao_ms5607_prom_read(&ms5607_prom); } -static volatile uint8_t ao_ms5607_done; +static __xdata volatile uint8_t ao_ms5607_done; static void ao_ms5607_isr(void) { ao_exti_disable(AO_MS5607_MISO_PORT, AO_MS5607_MISO_PIN); ao_ms5607_done = 1; - ao_wakeup((void *) &ao_ms5607_done); + ao_wakeup((__xdata void *) &ao_ms5607_done); } static uint32_t ao_ms5607_get_sample(uint8_t cmd) { - uint8_t reply[3]; - uint8_t read; + __xdata uint8_t reply[3]; + __xdata uint8_t read; ao_ms5607_done = 0; ao_ms5607_start(); - ao_spi_send(&cmd, 1, AO_MS5607_SPI_INDEX); + ao_spi_send(DATA_TO_XDATA(&cmd), 1, AO_MS5607_SPI_INDEX); ao_exti_enable(AO_MS5607_MISO_PORT, AO_MS5607_MISO_PIN); @@ -179,10 +179,14 @@ ao_ms5607_sample(struct ao_ms5607_sample *sample) sample->temp = ao_ms5607_get_sample(AO_CONVERT_D2); } +#ifdef _CC1111_H_ +#include "ao_ms5607_convert_8051.c" +#else #include "ao_ms5607_convert.c" +#endif #if HAS_TASK -struct ao_ms5607_sample ao_ms5607_current; +__xdata struct ao_ms5607_sample ao_ms5607_current; static void ao_ms5607(void) @@ -191,10 +195,10 @@ ao_ms5607(void) for (;;) { ao_ms5607_sample(&ao_ms5607_current); - ao_arch_critical( - AO_DATA_PRESENT(AO_DATA_MS5607); - AO_DATA_WAIT(); - ); + ao_arch_block_interrupts(); + AO_DATA_PRESENT(AO_DATA_MS5607); + AO_DATA_WAIT(); + ao_arch_release_interrupts(); } } diff --git a/src/drivers/ao_ms5607.h b/src/drivers/ao_ms5607.h index b2f98a59..3fd43fd4 100644 --- a/src/drivers/ao_ms5607.h +++ b/src/drivers/ao_ms5607.h @@ -56,7 +56,7 @@ struct ao_ms5607_value { int32_t temp; /* in °C * 100 */ }; -extern struct ao_ms5607_sample ao_ms5607_current; +extern __xdata struct ao_ms5607_sample ao_ms5607_current; void ao_ms5607_setup(void); diff --git a/src/drivers/ao_ms5607_convert_8051.c b/src/drivers/ao_ms5607_convert_8051.c new file mode 100644 index 00000000..f47972c9 --- /dev/null +++ b/src/drivers/ao_ms5607_convert_8051.c @@ -0,0 +1,60 @@ +/* + * 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. + */ + +#include + +void +ao_ms5607_convert(struct ao_ms5607_sample *sample, struct ao_ms5607_value *value) +{ +#if 0 + int32_t dT; + int32_t TEMP; + int64_t OFF; + int64_t SENS; + + dT = sample->temp - ((int32_t) ms5607_prom.tref << 8); + + TEMP = 2000 + (((int64_t) dT * ms5607_prom.tempsens) >> 23); + +#if HAS_MS5611 + OFF = ((int64_t) ms5607_prom.off << 16) + (((int64_t) ms5607_prom.tco * dT) >> 7); + SENS = ((int64_t) ms5607_prom.sens << 15) + (((int64_t) ms5607_prom.tcs * dT) >> 8); +#else + OFF = ((int64_t) ms5607_prom.off << 17) + (((int64_t) ms5607_prom.tco * dT) >> 6); + SENS = ((int64_t) ms5607_prom.sens << 16) + (((int64_t) ms5607_prom.tcs * dT) >> 7); +#endif + + if (TEMP < 2000) { + int32_t T2 = ((int64_t) dT * (int64_t) dT) >> 31; + int32_t TEMPM = TEMP - 2000; + int64_t OFF2 = (61 * (int64_t) TEMPM * (int64_t) TEMPM) >> 4; + int64_t SENS2 = 2 * (int64_t) TEMPM * (int64_t) TEMPM; + if (TEMP < 1500) { + int32_t TEMPP = TEMP + 1500; + int64_t TEMPP2 = TEMPP * TEMPP; + OFF2 = OFF2 + 15 * TEMPP2; + SENS2 = SENS2 + 8 * TEMPP2; + } + TEMP -= T2; + OFF -= OFF2; + SENS -= SENS2; + } + + value->pres = ((((int64_t) sample->pres * SENS) >> 21) - OFF) >> 15; + value->temp = TEMP; +#endif +} diff --git a/src/telemini-v2.0/Makefile b/src/telemini-v2.0/Makefile new file mode 100644 index 00000000..afd529f0 --- /dev/null +++ b/src/telemini-v2.0/Makefile @@ -0,0 +1,108 @@ +# +# TeleMini build file +# + +TELEMINI_VER=2.0 +TELEMINI_DEF=2_0 + +vpath %.c ..:../core:../cc1111:../drivers:../product +vpath %.h ..:../core:../cc1111:../drivers:../product +vpath ao-make-product.5c ../util + +ifndef VERSION +include ../Version +endif + +INC = \ + ao.h \ + ao_pins.h \ + ao_arch.h \ + ao_arch_funcs.h \ + cc1111.h \ + ao_product.h + +CORE_SRC = \ + ao_cmd.c \ + ao_config.c \ + ao_convert.c \ + ao_flight.c \ + ao_kalman.c \ + ao_log.c \ + ao_log_mini.c \ + ao_mutex.c \ + ao_panic.c \ + ao_report.c \ + ao_sample.c \ + ao_stdio.c \ + ao_storage.c \ + ao_task.c \ + ao_telemetry.c \ + ao_freq.c + +CC1111_SRC = \ + ao_adc.c \ + ao_dma.c \ + ao_ignite.c \ + ao_led.c \ + ao_packet.c \ + ao_packet_slave.c \ + ao_radio.c \ + ao_romconfig.c \ + ao_string.c \ + ao_spi.c \ + ao_usb.c \ + ao_convert_pa.c \ + ao_data.c \ + ao_beep.c \ + ao_timer.c \ + _bp.c + +DRIVER_SRC = \ + ao_ms5607.c \ + ao_m25.c + +PRODUCT_SRC = \ + ao_telemini.c + +SRC = \ + $(CORE_SRC) \ + $(CC1111_SRC) \ + $(DRIVER_SRC) \ + $(PRODUCT_SRC) + +PROGNAME = telemini-v$(TELEMINI_VER) +PROG = $(PROGNAME)-$(VERSION).ihx +PRODUCT=TeleMini-v$(TELEMINI_VER) +PRODUCT_DEF=-DTELEMINI_V_$(TELEMINI_DEF) +IDPRODUCT=0x000a + +include ../cc1111/Makefile.cc1111 + +NICKLE=nickle +CHECK_STACK=sh ../util/check-stack + +V=0 +# The user has explicitly enabled quiet compilation. +ifeq ($(V),0) +quiet = @printf " $1 $2 $@\n"; $($1) +endif +# Otherwise, print the full command line. +quiet ?= $($1) + +all: ../$(PROG) + +../$(PROG): $(REL) Makefile + $(call quiet,CC) $(LDFLAGS) $(CFLAGS) -o $(PROG) $(REL) && cp $(PROG) $(PMAP) .. + $(call quiet,CHECK_STACK) ../cc1111/ao_arch.h $(PMEM) || rm $@ + +ao_product.h: ao-make-product.5c ../Version + $(call quiet,NICKLE,$<) $< -m altusmetrum.org -i $(IDPRODUCT) -p $(PRODUCT) -v $(VERSION) > $@ + +distclean: clean + +clean: clean-cc1111 + +install: + +uninstall: + diff --git a/src/telemini-v2.0/ao_pins.h b/src/telemini-v2.0/ao_pins.h new file mode 100644 index 00000000..386c8dc3 --- /dev/null +++ b/src/telemini-v2.0/ao_pins.h @@ -0,0 +1,140 @@ +/* + * Copyright © 2010 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_PINS_H_ +#define _AO_PINS_H_ + +#define HAS_RADIO 1 + +#define HAS_FLIGHT 1 +#define HAS_USB 1 +#define USB_FORCE_FLIGHT_IDLE 1 +#define HAS_BEEP 1 +#define HAS_GPS 0 +#define HAS_SERIAL_1 0 +#define HAS_EEPROM 1 +#define HAS_LOG 1 +#define USE_INTERNAL_FLASH 0 +#define HAS_DBG 0 +#define PACKET_HAS_SLAVE 1 +#define USE_FAST_ASCENT_LOG 1 + +#define AO_LED_GREEN 1 +#define AO_LED_RED 2 +#define LEDS_AVAILABLE (AO_LED_RED|AO_LED_GREEN) +#define HAS_EXTERNAL_TEMP 0 +#define HAS_ACCEL 0 +#define HAS_IGNITE 1 +#define HAS_IGNITE_REPORT 1 +#define HAS_MONITOR 0 + +/* + * SPI + */ + +#define SPI_CS_PORT P1 +#define SPI_CS_SEL P1SEL +#define SPI_CS_DIR P1DIR + +/* + * Flash + */ +#define AO_M25_SPI_CS_PORT SPI_CS_PORT +#define AO_M25_SPI_CS_MASK 0x04 /* cs_flash is P1_2 */ +#define M25_MAX_CHIPS 1 + +/* + * MS5607 + */ + +#define HAS_MS5607 1 +#define HAS_MS5611 0 +#define AO_MS5607_PRIVATE_PINS 0 +#define AO_MS5607_CS_PORT P1 +#define AO_MS5607_CS_PIN 3 +#define AO_MS5607_CS P1_3 +#define AO_MS5607_CS_MASK (1 << AO_MS5607_CS_PIN) +#define AO_MS5607_MISO_PORT P0 +#define AO_MS5607_MISO_PIN 2 +#define AO_MS5607_MISO_MASK (1 << AO_MS5607_MISO_PIN) +#define AO_MS5607_SPI_INDEX 0 + +/* + * Igniters + */ +#define AO_IGNITER_PORT P2 +#define AO_IGNITER_DROGUE_PORT AO_IGNITER_PORT +#define AO_IGNITER_DROGUE P2_3 +#define AO_IGNITER_MAIN P2_4 +#define AO_IGNITER_DIR P2DIR +#define AO_IGNITER_DROGUE_BIT (1 << 3) +#define AO_IGNITER_MAIN_BIT (1 << 4) +#define AO_IGNITER_DROGUE_PIN 3 +#define AO_IGNITER_MAIN_PIN 4 + +#define AO_IGNITER_DROGUE_PORT AO_IGNITER_PORT +#define AO_IGNITER_MAIN_PORT AO_IGNITER_PORT + +/* test these values with real igniters */ +#define AO_IGNITER_OPEN 1000 +#define AO_IGNITER_CLOSED 7000 +#define AO_IGNITER_FIRE_TIME AO_MS_TO_TICKS(50) +#define AO_IGNITER_CHARGE_TIME AO_MS_TO_TICKS(2000) + +#define AO_SEND_MINI + +/* + * ADC + */ + +#define HAS_ADC 1 +#define AO_ADC_FIRST_PIN 0 + +struct ao_adc { + int16_t sense_a; /* apogee continuity sense */ + int16_t sense_m; /* main continuity sense */ + int16_t v_batt; /* battery voltage */ +}; + +#define ao_data_count ao_adc_count + +#define AO_SENSE_DROGUE(p) ((p)->adc.sense_a) +#define AO_SENSE_MAIN(p) ((p)->adc.sense_m) + +#define AO_ADC_DUMP(p) \ + printf("tick: %5u apogee: %5d main: %5d batt: %5d\n", \ + (p)->tick, (p)->adc.sense_a, (p)->adc.sense_m, (p)->adc.v_batt) + +#define FETCH_ADC() \ + a = (uint8_t __xdata *) (&ao_data_ring[ao_data_head].adc); \ + switch (sequence) { \ + case 4: \ + a += 4; \ + sequence = 0; \ + break; \ + case 1: \ + a += 2; \ + sequence = 4; \ + break; \ + case 0: \ + sequence = 1; \ + break; \ + } \ + if (sequence) \ + ; + +#endif /* _AO_PINS_H_ */ diff --git a/src/telemini-v2.0/ao_telemini.c b/src/telemini-v2.0/ao_telemini.c new file mode 100644 index 00000000..84df2b8c --- /dev/null +++ b/src/telemini-v2.0/ao_telemini.c @@ -0,0 +1,54 @@ +/* + * 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. + */ + +#include "ao.h" +#include "ao_pins.h" + +__xdata uint8_t ao_force_freq; + +void +main(void) +{ + /* + * Reduce the transient on the ignite pins at startup by + * pulling the pins low as soon as possible at power up + */ + ao_ignite_set_pins(); + + ao_clock_init(); + + /* Turn on the red LED until the system is stable */ + ao_led_init(LEDS_AVAILABLE); + ao_led_on(AO_LED_RED); + + ao_task_init(); + + ao_timer_init(); + ao_adc_init(); + ao_cmd_init(); + ao_storage_init(); + ao_ms5607_init(); + ao_flight_init(); + ao_log_init(); + ao_report_init(); + ao_telemetry_init(); + ao_radio_init(); + ao_packet_slave_init(TRUE); + ao_igniter_init(); + ao_config_init(); + ao_start_scheduler(); +} diff --git a/src/test/Makefile b/src/test/Makefile index 75b1f848..9c304318 100644 --- a/src/test/Makefile +++ b/src/test/Makefile @@ -2,7 +2,7 @@ vpath % ..:../core:../drivers:../util:../micropeak:../aes PROGS=ao_flight_test ao_flight_test_baro ao_flight_test_accel ao_flight_test_noisy_accel ao_flight_test_mm \ ao_gps_test ao_gps_test_skytraq ao_gps_test_ublox ao_convert_test ao_convert_pa_test ao_fec_test \ - ao_aprs_test ao_micropeak_test ao_fat_test ao_aes_test + ao_aprs_test ao_micropeak_test ao_fat_test ao_aes_test ao_int64_test INCS=ao_kalman.h ao_ms5607.h ao_log.h ao_data.h altitude-pa.h altitude.h @@ -73,3 +73,6 @@ ao_fat_test: ao_fat_test.c ao_fat.c ao_bufio.c ao_aes_test: ao_aes_test.c ao_aes.c ao_aes_tables.c cc $(CFLAGS) -o $@ ao_aes_test.c + +ao_int64_test: ao_int64_test.c ao_int64.c ao_int64.h + cc $(CFLAGS) -o $@ ao_int64_test.c -- cgit v1.2.3 From 39475c7b8da4f29936f73ffa2bff112f50ee9328 Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Wed, 28 Aug 2013 21:52:29 -0600 Subject: altos: TM v2 places the MMA6555 upside down compared to Tmega Means we need to invert the data coming out to make it work Signed-off-by: Keith Packard --- src/core/ao_data.h | 4 ++++ src/telemetrum-v2.0/ao_pins.h | 1 + 2 files changed, 5 insertions(+) (limited to 'src/core/ao_data.h') diff --git a/src/core/ao_data.h b/src/core/ao_data.h index b0f086f8..c873e9d3 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -272,7 +272,11 @@ typedef int16_t accel_t; /* MMA655X is hooked up so that positive values represent negative acceleration */ #define ao_data_accel(packet) ((packet)->mma655x) +#if AO_MMA655X_INVERT +#define ao_data_accel_cook(packet) (4095 - (packet)->mma655x) +#else #define ao_data_accel_cook(packet) ((packet)->mma655x) +#endif #define ao_data_set_accel(packet, accel) ((packet)->mma655x = (accel)) #define ao_data_accel_invert(accel) (4095 - (accel)) diff --git a/src/telemetrum-v2.0/ao_pins.h b/src/telemetrum-v2.0/ao_pins.h index 04cce99e..a7236b80 100644 --- a/src/telemetrum-v2.0/ao_pins.h +++ b/src/telemetrum-v2.0/ao_pins.h @@ -257,6 +257,7 @@ struct ao_adc { #define AO_MMA655X_SPI_INDEX AO_SPI_1_PB3_PB4_PB5 #define AO_MMA655X_CS_PORT (&stm_gpiob) #define AO_MMA655X_CS_PIN 9 +#define AO_MMA655X_INVERT 1 #define NUM_CMDS 16 -- cgit v1.2.3 From 08143a922fe27bc50a19924f46538f9476ab5fd1 Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Fri, 25 Oct 2013 04:05:09 -0700 Subject: altos: Add gyro-based orientation tracking This tracks the angle-from-vertical as an additional input to the pyro channels. Signed-off-by: Keith Packard --- src/core/ao_data.h | 6 +- src/core/ao_flight.c | 4 + src/core/ao_kalman.c | 3 - src/core/ao_pyro.c | 4 +- src/core/ao_quaternion.h | 116 +++++++++++++++++++ src/core/ao_sample.c | 98 +++++++++++++++- src/core/ao_sample.h | 3 +- src/core/ao_telemetry.c | 1 + src/core/ao_telemetry.h | 2 +- src/drivers/ao_mpu6000.c | 2 + src/drivers/ao_mpu6000.h | 17 ++- src/stm/Makefile.defs | 4 +- src/telemega-v0.3/Makefile | 16 +++ src/test/Makefile | 9 +- src/test/ao_flight_test.c | 259 ++---------------------------------------- src/test/ao_quaternion_test.c | 67 +++++++++++ 16 files changed, 343 insertions(+), 268 deletions(-) create mode 100644 src/core/ao_quaternion.h create mode 100644 src/test/ao_quaternion_test.c (limited to 'src/core/ao_data.h') diff --git a/src/core/ao_data.h b/src/core/ao_data.h index 339afe69..5a232885 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -18,6 +18,8 @@ #ifndef _AO_DATA_H_ #define _AO_DATA_H_ +#define GRAVITY 9.80665 + #if HAS_ADC #define AO_DATA_ADC (1 << 0) #else @@ -300,8 +302,8 @@ typedef int16_t accel_t; #define HAS_GYRO 1 -typedef int16_t gyro_t; -typedef int32_t angle_t; +typedef int16_t gyro_t; /* in raw sample units */ +typedef int16_t angle_t; /* in degrees */ /* Y axis is aligned with the direction of motion (along) */ /* X axis is aligned in the other board axis (across) */ diff --git a/src/core/ao_flight.c b/src/core/ao_flight.c index 2495a44b..240b348a 100644 --- a/src/core/ao_flight.c +++ b/src/core/ao_flight.c @@ -20,6 +20,10 @@ #include #endif +#if HAS_MPU6000 +#include +#endif + #ifndef HAS_ACCEL #error Please define HAS_ACCEL #endif diff --git a/src/core/ao_kalman.c b/src/core/ao_kalman.c index 762b2c0a..7fd4f889 100644 --- a/src/core/ao_kalman.c +++ b/src/core/ao_kalman.c @@ -292,7 +292,4 @@ ao_kalman(void) else #endif ao_avg_height = (ao_avg_height_scaled + 63) >> 7; -#ifdef AO_FLIGHT_TEST - ao_sample_prev_tick = ao_sample_tick; -#endif } diff --git a/src/core/ao_pyro.c b/src/core/ao_pyro.c index 531e1f50..24c9fe99 100644 --- a/src/core/ao_pyro.c +++ b/src/core/ao_pyro.c @@ -113,7 +113,7 @@ ao_pyro_ready(struct ao_pyro *pyro) continue; break; -#if HAS_ORIENT +#if HAS_GYRO case ao_pyro_orient_less: if (ao_orient <= pyro->orient_less) continue; @@ -310,7 +310,7 @@ const struct { { "h<", ao_pyro_height_less, offsetof(struct ao_pyro, height_less), HELP("height less (m)") }, { "h>", ao_pyro_height_greater, offsetof(struct ao_pyro, height_greater), HELP("height greater (m)") }, -#if HAS_ORIENT +#if HAS_GYRO { "o<", ao_pyro_orient_less, offsetof(struct ao_pyro, orient_less), HELP("orient less (deg)") }, { "o>", ao_pyro_orient_greater, offsetof(struct ao_pyro, orient_greater), HELP("orient greater (deg)") }, #endif diff --git a/src/core/ao_quaternion.h b/src/core/ao_quaternion.h new file mode 100644 index 00000000..f4b8aaa4 --- /dev/null +++ b/src/core/ao_quaternion.h @@ -0,0 +1,116 @@ +/* + * Copyright © 2013 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_QUATERNION_H_ +#define _AO_QUATERNION_H_ + +#include + +struct ao_quaternion { + float r; /* real bit */ + float x, y, z; /* imaginary bits */ +}; + +static inline void ao_quaternion_multiply(struct ao_quaternion *r, + struct ao_quaternion *a, + struct ao_quaternion *b) +{ + struct ao_quaternion t; +#define T(_a,_b) (((a)->_a) * ((b)->_b)) + t.r = T(r,r) - T(x,x) - T(y,y) - T(z,z); + t.x = T(r,x) + T(x,r) + T(y,z) - T(z,y); + t.y = T(r,y) - T(x,z) + T(y,r) + T(z,x); + t.z = T(r,z) + T(x,y) - T(y,x) + T(z,r); +#undef T + *r = t; +} + +static inline void ao_quaternion_conjugate(struct ao_quaternion *r, + struct ao_quaternion *a) +{ + r->r = a->r; + r->x = -a->x; + r->y = -a->y; + r->z = -a->z; +} + +static inline float ao_quaternion_normal(struct ao_quaternion *a) +{ +#define S(_a) (((a)->_a) * ((a)->_a)) + return S(r) + S(x) + S(y) + S(z); +#undef S +} + +static inline void ao_quaternion_scale(struct ao_quaternion *r, + struct ao_quaternion *a, + float b) +{ + r->r = a->r * b; + r->x = a->x * b; + r->y = a->y * b; + r->z = a->z * b; +} + +static inline void ao_quaternion_normalize(struct ao_quaternion *r, + struct ao_quaternion *a) +{ + float n = ao_quaternion_normal(a); + + if (n > 0) + ao_quaternion_scale(r, a, 1/sqrtf(n)); + else + *r = *a; +} + +static inline void ao_quaternion_rotate(struct ao_quaternion *r, + struct ao_quaternion *a, + struct ao_quaternion *b) +{ + struct ao_quaternion c; + struct ao_quaternion t; + + ao_quaternion_conjugate(&c, b); + ao_quaternion_multiply(&t, b, a); + ao_quaternion_multiply(r, &t, &c); +} + +static inline void ao_quaternion_init_vector(struct ao_quaternion *r, + float x, float y, float z) +{ + r->r = 0; + r->x = x; + r->y = y; + r->z = z; +} + +static inline void ao_quaternion_init_rotation(struct ao_quaternion *r, + float x, float y, float z, + float s, float c) +{ + r->r = c; + r->x = s * x; + r->y = s * y; + r->z = s * z; +} + +static inline void ao_quaternion_init_zero_rotation(struct ao_quaternion *r) +{ + r->r = 1; + r->x = r->y = r->z = 0; +} + +#endif /* _AO_QUATERNION_H_ */ diff --git a/src/core/ao_sample.c b/src/core/ao_sample.c index dec44f9f..676e0ffd 100644 --- a/src/core/ao_sample.c +++ b/src/core/ao_sample.c @@ -20,6 +20,10 @@ #include #endif +#if HAS_GYRO +#include +#endif + /* * Current sensor values */ @@ -44,8 +48,7 @@ __pdata accel_t ao_sample_accel_through; __pdata gyro_t ao_sample_roll; __pdata gyro_t ao_sample_pitch; __pdata gyro_t ao_sample_yaw; -__pdata angle_t ao_sample_angle; -__pdata angle_t ao_sample_roll_angle; +__pdata angle_t ao_orient; #endif __data uint8_t ao_sample_data; @@ -86,6 +89,8 @@ __pdata int32_t ao_sample_accel_through_sum; __pdata int32_t ao_sample_pitch_sum; __pdata int32_t ao_sample_yaw_sum; __pdata int32_t ao_sample_roll_sum; +static struct ao_quaternion ao_rotation; +static struct ao_quaternion ao_pad_orientation; #endif static void @@ -129,11 +134,91 @@ ao_sample_preflight_set(void) ao_sample_pitch_sum = 0; ao_sample_yaw_sum = 0; ao_sample_roll_sum = 0; - ao_sample_angle = 0; + ao_orient = 0; + + /* No rotation yet */ + ao_quaternion_init_zero_rotation(&ao_rotation); + + /* XXX Assume we're pointing straight up for now */ + ao_quaternion_init_vector(&ao_pad_orientation, + ao_ground_accel_across, + ao_ground_accel_through, + -ao_ground_accel_along); + ao_quaternion_normalize(&ao_pad_orientation, + &ao_pad_orientation); + + printf ("pad r%8.5f x%8.5f y%8.5f z%8.5f\n", + ao_pad_orientation.r, + ao_pad_orientation.x, + ao_pad_orientation.y, + ao_pad_orientation.z); #endif nsamples = 0; } +#if HAS_GYRO +static void +ao_sample_rotate(void) +{ +#ifdef AO_FLIGHT_TEST + float dt = (ao_sample_tick - ao_sample_prev_tick) / 100.0; +#else + static const float dt = 1/100.0; +#endif + float x = ao_mpu6000_gyro(ao_sample_pitch - ao_ground_pitch) * dt; + float y = ao_mpu6000_gyro(ao_sample_yaw - ao_ground_yaw) * dt; + float z = ao_mpu6000_gyro(ao_sample_roll - ao_ground_roll) * dt; + + float n_2, n; + float s, c; + + struct ao_quaternion rot; + struct ao_quaternion point; + + /* The amount of rotation is just the length of the vector. Now, + * here's the trick -- assume that the rotation amount is small. In this case, + * sin(x) ≃ x, so we can just make this the sin. + */ + + n_2 = x*x + y*y + z*z; + n = sqrtf(n_2); + s = n / 2; + if (s > 1) + s = 1; + c = sqrtf(1 - s*s); + + /* Make unit vector */ + if (n > 0) { + x /= n; + y /= n; + z /= n; + } + + /* Now compute the unified rotation quaternion */ + + ao_quaternion_init_rotation(&rot, + x, y, z, + s, c); + + /* Integrate with the previous rotation amount */ + ao_quaternion_multiply(&ao_rotation, &ao_rotation, &rot); + + /* And normalize to make sure it remains a unit vector */ + ao_quaternion_normalize(&ao_rotation, &ao_rotation); + + /* Compute pitch angle from vertical by taking the pad + * orientation vector and rotating it by the current total + * rotation value. That will be a unit vector pointing along + * the airframe axis. The Z value will be the cosine of the + * change in the angle from vertical since boost + */ + + ao_quaternion_rotate(&point, &ao_pad_orientation, &ao_rotation); + + ao_orient = acosf(point.z) * (float) (180.0/M_PI); +} +#endif + static void ao_sample_preflight(void) { @@ -232,9 +317,12 @@ ao_sample(void) ao_sample_preflight_update(); ao_kalman(); #if HAS_GYRO - /* do quaternion stuff here... */ + ao_sample_rotate(); #endif } +#ifdef AO_FLIGHT_TEST + ao_sample_prev_tick = ao_sample_tick; +#endif ao_sample_data = ao_data_ring_next(ao_sample_data); } return !ao_preflight; @@ -264,7 +352,7 @@ ao_sample_init(void) ao_sample_pitch = 0; ao_sample_yaw = 0; ao_sample_roll = 0; - ao_sample_angle = 0; + ao_orient = 0; #endif ao_sample_data = ao_data_head; ao_preflight = TRUE; diff --git a/src/core/ao_sample.h b/src/core/ao_sample.h index 5bd29536..1d1bcc7c 100644 --- a/src/core/ao_sample.h +++ b/src/core/ao_sample.h @@ -64,8 +64,6 @@ * for all further flight computations */ -#define GRAVITY 9.80665 - /* * Above this height, the baro sensor doesn't work */ @@ -118,6 +116,7 @@ extern __pdata accel_t ao_ground_accel_through; extern __pdata gyro_t ao_ground_pitch; extern __pdata gyro_t ao_ground_yaw; extern __pdata gyro_t ao_ground_roll; +extern __pdata angle_t ao_orient; #endif void ao_sample_init(void); diff --git a/src/core/ao_telemetry.c b/src/core/ao_telemetry.c index 6b47a06a..a2726016 100644 --- a/src/core/ao_telemetry.c +++ b/src/core/ao_telemetry.c @@ -115,6 +115,7 @@ ao_send_mega_sensor(void) telemetry.generic.tick = packet->tick; telemetry.generic.type = AO_TELEMETRY_MEGA_SENSOR; + telemetry.mega_sensor.orient = ao_orient; telemetry.mega_sensor.accel = ao_data_accel(packet); telemetry.mega_sensor.pres = ao_data_pres(packet); telemetry.mega_sensor.temp = ao_data_temp(packet); diff --git a/src/core/ao_telemetry.h b/src/core/ao_telemetry.h index fd6b76b3..237a35ab 100644 --- a/src/core/ao_telemetry.h +++ b/src/core/ao_telemetry.h @@ -162,7 +162,7 @@ struct ao_telemetry_mega_sensor { uint16_t tick; /* 2 */ uint8_t type; /* 4 */ - uint8_t pad5; /* 5 */ + uint8_t orient; /* 5 angle from vertical */ int16_t accel; /* 6 Z axis */ int32_t pres; /* 8 Pa * 10 */ diff --git a/src/drivers/ao_mpu6000.c b/src/drivers/ao_mpu6000.c index 73057820..5e75b78a 100644 --- a/src/drivers/ao_mpu6000.c +++ b/src/drivers/ao_mpu6000.c @@ -118,6 +118,7 @@ _ao_mpu6000_sample(struct ao_mpu6000_sample *sample) #define G 981 /* in cm/s² */ +#if 0 static int16_t /* cm/s² */ ao_mpu6000_accel(int16_t v) { @@ -129,6 +130,7 @@ ao_mpu6000_gyro(int16_t v) { return (int16_t) ((v * (int32_t) 20000) / 32767); } +#endif static uint8_t ao_mpu6000_accel_check(int16_t normal, int16_t test, char *which) diff --git a/src/drivers/ao_mpu6000.h b/src/drivers/ao_mpu6000.h index a42f69c4..2241bf80 100644 --- a/src/drivers/ao_mpu6000.h +++ b/src/drivers/ao_mpu6000.h @@ -18,6 +18,10 @@ #ifndef _AO_MPU6000_H_ #define _AO_MPU6000_H_ +#ifndef M_PI +#define M_PI 3.1415926535897832384626433 +#endif + #define MPU6000_ADDR_WRITE 0xd0 #define MPU6000_ADDR_READ 0xd1 @@ -166,9 +170,20 @@ /* Self test gyro is approximately 50°/s */ #define MPU6000_ST_GYRO(full_scale) ((int16_t) (((int32_t) 32767 * (int32_t) 50) / (full_scale))) -#define MPU6000_GYRO_FULLSCALE 2000 +#define MPU6000_GYRO_FULLSCALE ((float) 2000 * M_PI/180.0) + +static inline float +ao_mpu6000_gyro(int16_t sensor) { + return (float) sensor * ((float) (MPU6000_GYRO_FULLSCALE / 32767.0)); +} + #define MPU6000_ACCEL_FULLSCALE 16 +static inline float +ao_mpu6000_accel(int16_t sensor) { + return (float) sensor * ((float) (MPU6000_ACCEL_FULLSCALE * GRAVITY / 32767.0)); +} + struct ao_mpu6000_sample { int16_t accel_x; int16_t accel_y; diff --git a/src/stm/Makefile.defs b/src/stm/Makefile.defs index ee1cb658..0710d747 100644 --- a/src/stm/Makefile.defs +++ b/src/stm/Makefile.defs @@ -1,4 +1,4 @@ -vpath % ../stm:../product:../drivers:../core:../util:../kalman:../aes:.. +vpath % ../stm:../product:../drivers:../core:../util:../kalman:../aes:../math:.. vpath make-altitude ../util vpath make-kalman ../util vpath kalman.5c ../kalman @@ -24,7 +24,7 @@ include $(TOPDIR)/Makedefs CC=$(ARM_CC) LIBS=-lpdclib-cortex-m3 -lgcc -AO_CFLAGS=-I. -I../stm -I../core -I../drivers -I.. +AO_CFLAGS=-I. -I../stm -I../core -I../drivers -I../math -I.. STM_CFLAGS=-std=gnu99 -mlittle-endian -mcpu=cortex-m3 -mthumb -ffreestanding -nostdlib $(AO_CFLAGS) LDFLAGS=-L../stm -Wl,-Taltos.ld diff --git a/src/telemega-v0.3/Makefile b/src/telemega-v0.3/Makefile index 6e5da721..2f460105 100644 --- a/src/telemega-v0.3/Makefile +++ b/src/telemega-v0.3/Makefile @@ -27,6 +27,7 @@ INC = \ ao_sample_profile.h \ ao_mpu.h \ stm32l.h \ + math.h \ Makefile # @@ -44,6 +45,20 @@ INC = \ #STACK_GUARD=ao_mpu_stm.c #STACK_GUARD_DEF=-DHAS_STACK_GUARD=1 +MATH_SRC=\ + ef_acos.c \ + ef_sqrt.c + +# ef_rem_pio2.c \ +# kf_cos.c \ +# kf_sin.c \ +# kf_rem_pio2.c \ +# sf_copysign.c \ +# sf_cos.c \ +# sf_fabs.c \ +# sf_floor.c \ +# sf_scalbn.c + ALTOS_SRC = \ ao_boot_chain.c \ ao_interrupt.c \ @@ -93,6 +108,7 @@ ALTOS_SRC = \ ao_companion.c \ ao_pyro.c \ ao_aprs.c \ + $(MATH_SRC) \ $(PROFILE) \ $(SAMPLE_PROFILE) \ $(STACK_GUARD) diff --git a/src/test/Makefile b/src/test/Makefile index 5eee6bbb..f64a9531 100644 --- a/src/test/Makefile +++ b/src/test/Makefile @@ -1,15 +1,15 @@ -vpath % ..:../core:../drivers:../util:../micropeak:../aes +vpath % ..:../core:../drivers:../util:../micropeak:../aes:../product PROGS=ao_flight_test ao_flight_test_baro ao_flight_test_accel ao_flight_test_noisy_accel ao_flight_test_mm \ ao_gps_test ao_gps_test_skytraq ao_gps_test_ublox ao_convert_test ao_convert_pa_test ao_fec_test \ ao_aprs_test ao_micropeak_test ao_fat_test ao_aes_test ao_int64_test \ - ao_ms5607_convert_test + ao_ms5607_convert_test ao_quaternion_test INCS=ao_kalman.h ao_ms5607.h ao_log.h ao_data.h altitude-pa.h altitude.h KALMAN=make-kalman -CFLAGS=-I.. -I. -I../core -I../drivers -I../micropeak -O0 -g -Wall +CFLAGS=-I.. -I. -I../core -I../drivers -I../micropeak -I../product -O0 -g -Wall all: $(PROGS) ao_aprs_data.wav @@ -80,3 +80,6 @@ ao_int64_test: ao_int64_test.c ao_int64.c ao_int64.h ao_ms5607_convert_test: ao_ms5607_convert_test.c ao_ms5607_convert_8051.c ao_int64.c ao_int64.h cc $(CFLAGS) -o $@ ao_ms5607_convert_test.c + +ao_quaternion_test: ao_quaternion_test.c ao_quaternion.h + cc $(CFLAGS) -o $@ ao_quaternion_test.c -lm \ No newline at end of file diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index faf31aa7..e2f63e34 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -25,6 +25,8 @@ #include #include +#define GRAVITY 9.80665 + #define AO_HERTZ 100 #define HAS_ADC 1 @@ -36,6 +38,11 @@ #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 @@ -240,7 +247,6 @@ struct ao_config ao_config; #define DATA_TO_XDATA(x) (x) -#define GRAVITY 9.80665 extern int16_t ao_ground_accel, ao_flight_accel; extern int16_t ao_accel_2g; @@ -339,20 +345,6 @@ ao_test_exit(void) exit(0); } -#if HAS_MPU6000 -static double -ao_mpu6000_accel(int16_t sensor) -{ - return sensor / 32767.0 * MPU6000_ACCEL_FULLSCALE * GRAVITY; -} - -static double -ao_mpu6000_gyro(int32_t sensor) -{ - return sensor / 32767.0 * MPU6000_GYRO_FULLSCALE; -} -#endif - void ao_insert(void) { @@ -408,23 +400,23 @@ ao_insert(void) if (!ao_summary) { printf("%7.2f height %8.2f accel %8.3f " #if TELEMEGA - "roll %8.3f angle %8.3f qangle %8.3f " - "accel_x %8.3f accel_y %8.3f accel_z %8.3f gyro_x %8.3f gyro_y %8.3f gyro_z %8.3f " + "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 " */ #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_mpu6000_gyro(ao_sample_roll_angle) / 100.0, - ao_mpu6000_gyro(ao_sample_angle) / 100.0, - ao_sample_qangle, + ao_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), +*/ #endif ao_state_names[ao_flight_state], ao_k_height / 65536.0, @@ -589,207 +581,6 @@ int32(uint8_t *bytes, int off) static int log_format; -#if TELEMEGA - -static double -ao_vec_norm(double x, double y, double z) -{ - return x*x + y*y + z*z; -} - -static void -ao_vec_normalize(double *x, double *y, double *z) -{ - double scale = 1/sqrt(ao_vec_norm(*x, *y, *z)); - - *x *= scale; - *y *= scale; - *z *= scale; -} - -struct ao_quat { - double q0, q1, q2, q3; -}; - -static void -ao_quat_mul(struct ao_quat *r, struct ao_quat *a, struct ao_quat *b) -{ - r->q0 = a->q0 * b->q0 - a->q1 * b->q1 - a->q2 * b->q2 - a->q3 * b->q3; - r->q1 = a->q0 * b->q1 + a->q1 * b->q0 + a->q2 * b->q3 - a->q3 * b->q2; - r->q2 = a->q0 * b->q2 - a->q1 * b->q3 + a->q2 * b->q0 + a->q3 * b->q1; - r->q3 = a->q0 * b->q3 + a->q1 * b->q2 - a->q2 * b->q1 + a->q3 * b->q0; -} - -#if 0 -static void -ao_quat_scale(struct ao_quat *r, struct ao_quat *a, double s) -{ - r->q0 = a->q0 * s; - r->q1 = a->q1 * s; - r->q2 = a->q2 * s; - r->q3 = a->q3 * s; -} -#endif - -static void -ao_quat_conj(struct ao_quat *r, struct ao_quat *a) -{ - r->q0 = a->q0; - r->q1 = -a->q1; - r->q2 = -a->q2; - r->q3 = -a->q3; -} - -static void -ao_quat_rot(struct ao_quat *r, struct ao_quat *a, struct ao_quat *q) -{ - struct ao_quat t; - struct ao_quat c; - ao_quat_mul(&t, q, a); - ao_quat_conj(&c, q); - ao_quat_mul(r, &t, &c); -} - -static void -ao_quat_from_angle(struct ao_quat *r, - double x_rad, - double y_rad, - double z_rad) -{ - double angle = sqrt (x_rad * x_rad + y_rad * y_rad + z_rad * z_rad); - double s = sin(angle/2); - double c = cos(angle/2); - - r->q0 = c; - r->q1 = x_rad * s / angle; - r->q2 = y_rad * s / angle; - r->q3 = z_rad * s / angle; -} - -static void -ao_quat_from_vector(struct ao_quat *r, double x, double y, double z) -{ - ao_vec_normalize(&x, &y, &z); - double x_rad = atan2(z, y); - double y_rad = atan2(x, z); - double z_rad = atan2(y, x); - - ao_quat_from_angle(r, x_rad, y_rad, z_rad); -} - -static double -ao_quat_norm(struct ao_quat *a) -{ - return (a->q0 * a->q0 + - a->q1 * a->q1 + - a->q2 * a->q2 + - a->q3 * a->q3); -} - -static void -ao_quat_normalize(struct ao_quat *a) -{ - double norm = ao_quat_norm(a); - - if (norm) { - double m = 1/sqrt(norm); - - a->q0 *= m; - a->q1 *= m; - a->q2 *= m; - a->q3 *= m; - } -} - -static struct ao_quat ao_up, ao_current; -static struct ao_quat ao_orient; -static int ao_orient_tick; - -void -set_orientation(double x, double y, double z, int tick) -{ - struct ao_quat t; - - printf ("set_orientation %g %g %g\n", x, y, z); - ao_quat_from_vector(&ao_orient, x, y, z); - ao_up.q1 = ao_up.q2 = 0; - ao_up.q0 = ao_up.q3 = sqrt(2)/2; - ao_orient_tick = tick; - - ao_orient.q0 = 1; - ao_orient.q1 = 0; - ao_orient.q2 = 0; - ao_orient.q3 = 0; - - printf ("orient (%g) %g %g %g up (%g) %g %g %g\n", - ao_orient.q0, - ao_orient.q1, - ao_orient.q2, - ao_orient.q3, - ao_up.q0, - ao_up.q1, - ao_up.q2, - ao_up.q3); - - ao_quat_rot(&t, &ao_up, &ao_orient); - printf ("pad orient (%g) %g %g %g\n", - t.q0, - t.q1, - t.q2, - t.q3); - -} - -void -update_orientation (double rate_x, double rate_y, double rate_z, int tick) -{ - struct ao_quat q_dot; - double lambda; - double dt = (tick - ao_orient_tick) / 100.0; - - ao_orient_tick = tick; - -// lambda = 1 - ao_quat_norm(&ao_orient); - lambda = 0; - - q_dot.q0 = -0.5 * (ao_orient.q1 * rate_x + ao_orient.q2 * rate_y + ao_orient.q3 * rate_z) + lambda * ao_orient.q0; - q_dot.q1 = 0.5 * (ao_orient.q0 * rate_x + ao_orient.q2 * rate_z - ao_orient.q3 * rate_y) + lambda * ao_orient.q1; - q_dot.q2 = 0.5 * (ao_orient.q0 * rate_y + ao_orient.q3 * rate_x - ao_orient.q1 * rate_z) + lambda * ao_orient.q2; - q_dot.q3 = 0.5 * (ao_orient.q0 * rate_z + ao_orient.q1 * rate_y - ao_orient.q2 * rate_x) + lambda * ao_orient.q3; - -#if 0 - printf ("update_orientation %g %g %g (%g s)\n", rate_x, rate_y, rate_z, dt); - printf ("q_dot (%g) %g %g %g\n", - q_dot.q0, - q_dot.q1, - q_dot.q2, - q_dot.q3); -#endif - - ao_orient.q0 += q_dot.q0 * dt; - ao_orient.q1 += q_dot.q1 * dt; - ao_orient.q2 += q_dot.q2 * dt; - ao_orient.q3 += q_dot.q3 * dt; - - ao_quat_normalize(&ao_orient); - - ao_quat_rot(&ao_current, &ao_up, &ao_orient); - - ao_sample_qangle = 180 / M_PI * acos(ao_current.q3 * sqrt(2)); -#if 0 - printf ("orient (%g) %g %g %g current (%g) %g %g %g\n", - ao_orient.q0, - ao_orient.q1, - ao_orient.q2, - ao_orient.q3, - ao_current.q0, - ao_current.q1, - ao_current.q2, - ao_current.q3); -#endif -} -#endif - void ao_sleep(void *wchan) { @@ -872,32 +663,6 @@ ao_sleep(void *wchan) #if HAS_MMA655X ao_data_static.mma655x = int16(bytes, 26); #endif - if (ao_records_read == 0) - ao_ground_mpu6000 = ao_data_static.mpu6000; - else if (ao_records_read < 10) { -#define f(f) ao_ground_mpu6000.f = ao_ground_mpu6000.f + ((ao_data_static.mpu6000.f - ao_ground_mpu6000.f) >> 2) - f(accel_x); - f(accel_y); - f(accel_z); - f(gyro_x); - f(gyro_y); - f(gyro_z); - - double accel_x = ao_mpu6000_accel(ao_ground_mpu6000.accel_x); - double accel_y = ao_mpu6000_accel(ao_ground_mpu6000.accel_y); - double accel_z = ao_mpu6000_accel(ao_ground_mpu6000.accel_z); - - /* X and Y are in the ground plane, arbitraryily picked as MPU X and Z axes - * Z is normal to the ground, the MPU y axis - */ - set_orientation(accel_x, accel_z, accel_y, tick); - } else { - double rate_x = ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_x - ao_ground_mpu6000.gyro_x); - double rate_y = ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_y - ao_ground_mpu6000.gyro_y); - double rate_z = ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_z - ao_ground_mpu6000.gyro_z); - - update_orientation(rate_x * M_PI / 180, rate_z * M_PI / 180, rate_y * M_PI / 180, tick); - } ao_records_read++; ao_insert(); return; diff --git a/src/test/ao_quaternion_test.c b/src/test/ao_quaternion_test.c new file mode 100644 index 00000000..0e4b5b07 --- /dev/null +++ b/src/test/ao_quaternion_test.c @@ -0,0 +1,67 @@ +/* + * Copyright © 2013 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. + */ + +#define _GNU_SOURCE + +#include +#include +#include +#include +#include +#include +#include + +#include "ao_quaternion.h" + +static void +print_q(char *name, struct ao_quaternion *q) +{ + printf ("%8.8s: r%8.5f x%8.5f y%8.5f z%8.5f ", name, + q->r, q->x, q->y, q->z); +} + +int main(int argc, char **argv) +{ + struct ao_quaternion position; + struct ao_quaternion rotation; + struct ao_quaternion little_rotation; + int i; + + /* unit x vector */ + ao_quaternion_init_vector(&position, 1, 0, 0); + + /* zero rotation */ + ao_quaternion_init_zero_rotation(&rotation); + + /* π/16 rotation around Z axis */ + ao_quaternion_init_rotation(&little_rotation, 0, 0, 1, + sin((M_PI/16)/2), + cos((M_PI/16)/2)); + for (i = 0; i <= 16; i++) { + struct ao_quaternion rotated; + + ao_quaternion_rotate(&rotated, &position, &rotation); + print_q("position", &position); + print_q("rotated", &rotated); + print_q("rotation", &rotation); + printf ("\n"); + ao_quaternion_multiply(&rotation, &rotation, &little_rotation); + ao_quaternion_normalize(&rotation, &rotation); + } + return 0; +} + -- cgit v1.2.3 From bdd6244d8b4a55c9aa4fb79b0cb1a0727afbc2ac Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Tue, 12 Nov 2013 14:01:55 +0900 Subject: altos: Add orientation tracking to ao_flight_test Shows calculated offset from vertical in ao_flight_test output Signed-off-by: Keith Packard --- src/core/ao_data.h | 12 +++++ src/core/ao_quaternion.h | 9 ++++ src/test/ao_flight_test.c | 111 +++++++++++++++++++++++++++++++++++++++++++--- 3 files changed, 127 insertions(+), 5 deletions(-) (limited to 'src/core/ao_data.h') diff --git a/src/core/ao_data.h b/src/core/ao_data.h index 5a232885..e1d8a139 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -319,4 +319,16 @@ typedef int16_t angle_t; /* in degrees */ #endif +#if !HAS_MAG && HAS_HMC5883 + +#define HAS_MAG 1 + +typedef int16_t ao_mag_t; /* in raw sample units */ + +#define ao_data_mag_along(packet) ((packet)->hmc5883.x) +#define ao_data_mag_across(packet) ((packet)->hmc5883.y) +#define ao_data_mag_through(packet) ((packet)->hmc5883.z) + +#endif + #endif /* _AO_DATA_H_ */ diff --git a/src/core/ao_quaternion.h b/src/core/ao_quaternion.h index 6c885500..044f1607 100644 --- a/src/core/ao_quaternion.h +++ b/src/core/ao_quaternion.h @@ -109,6 +109,15 @@ static inline void ao_quaternion_normalize(struct ao_quaternion *r, *r = *a; } +static inline float ao_quaternion_dot(const struct ao_quaternion *a, + const struct ao_quaternion *b) +{ +#define T(_a) (((a)->_a) * ((b)->_a)) + return T(r) + T(x) + T(y) + T(z); +#undef T +} + + static inline void ao_quaternion_rotate(struct ao_quaternion *r, const struct ao_quaternion *a, const struct ao_quaternion *b) diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index 952a811a..452f5b75 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -48,6 +48,7 @@ int ao_gps_new; #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]; @@ -349,6 +350,23 @@ 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) { @@ -402,10 +420,86 @@ ao_insert(void) } if (!ao_summary) { +#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); + + 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); + + 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); + + +#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 " */ + "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, @@ -413,14 +507,17 @@ ao_insert(void) 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, @@ -430,6 +527,7 @@ ao_insert(void) drogue_height, main_height, ao_error_h_sq_avg); +#endif // if (ao_flight_state == ao_flight_landed) // ao_test_exit(); @@ -659,11 +757,14 @@ ao_sleep(void *wchan) 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_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_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 -- cgit v1.2.3